Aircraft seating arrangement

DE502021010188D1Active Publication Date: 2026-04-23RECARO AIRCRAFT SEATING GMBH & CO KG
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Patent Information

Authority / Receiving Office
DE · DE
Patent Type
Patents
Current Assignee / Owner
RECARO AIRCRAFT SEATING GMBH & CO KG
Filing Date
2021-02-19
Publication Date
2026-04-23

AI Technical Summary

Technical Problem

Existing aircraft seating arrangements lack compactness and variability, failing to efficiently utilize space and cater to diverse passenger comfort needs across different booking classes.

Method used

An aircraft seating arrangement with multiple full-flat seats of varying comfort categories, arranged in a seat gap with differing seating and reclining directions, allowing direct access to an aisle and flexible positioning to optimize space usage and passenger comfort.

Benefits of technology

Enables a compact, variable, and comfortable seating arrangement that efficiently uses space, provides individualized comfort, and allows for flexible booking options, enhancing passenger experience across different classes.

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Description

State of the art

[0001] The invention relates to an aircraft seating arrangement according to the preamble of claim 1.

[0002] An aircraft seating arrangement has already been proposed with several aircraft seating devices arranged in one aircraft cabin section, which are at least partially different from each other and each have an aircraft seat designed as a full-flat seat.

[0003] Document US 2012 / 223 186 A1 discloses an aircraft seating arrangement with several aircraft seating units arranged in a row within an aircraft cabin section, wherein two of them are configured as lower aircraft seating units and one middle unit as an upper aircraft seating unit. The upper aircraft seating unit has a different comfort rating than the lower aircraft seating units.

[0004] The object of the invention is, in particular, to provide a generic arrangement with improved properties with regard to compactness and variability. This object is achieved according to the invention by the features of claim 1, while advantageous embodiments and further developments of the invention can be found in the dependent claims. Advantages of the invention

[0005] The invention relates to an aircraft seating arrangement for use in an aircraft cabin, wherein the aircraft cabin has at least one seat gap and at least one aircraft cabin section, and wherein the aircraft seating arrangement has several aircraft seating devices which, in the operating state of the aircraft seating arrangement, are arranged in the at least one aircraft cabin section, which are at least partially different from one another and each have an aircraft seat which is designed as a full-flat seat, wherein the aircraft seating devices in the aircraft cabin section differ in at least one comfort category, wherein the aircraft seating devices for the at least one comfort category each have a different value from one another, which is due to a different arrangement of the aircraft seats and to the at least partially different design of the aircraft seating devices.

[0006] According to the invention, at least four aircraft seat devices of different designs are arranged in a seat gap in the aircraft cabin section, wherein the at least four aircraft seat devices are arranged directly one behind the other in the seat gap in the operating state of the aircraft seat arrangement, so that all are intersected by the same longitudinal axis of the aircraft and each has direct access to the same aircraft cabin aisle.

[0007] The examples relating to aircraft seating arrangements with at least two or three seating devices are for illustrative purposes only and are not part of the claimed subject matter.

[0008] An embodiment according to the invention allows for an advantageously compact and variable arrangement of multiple aircraft seating units. The embodiment according to the invention allows for the advantageously simple combination of multiple aircraft seating units. Furthermore, the embodiment according to the invention allows for a particularly advantageous positioning of the multiple aircraft seating units relative to one another. This allows for advantageously efficient use of available space. Additionally, the aircraft seats in the reclining position can thus form an advantageously large lying surface. Furthermore, the embodiment according to the invention allows for the advantageously variable positioning of multiple aircraft seating units relative to one another, particularly when arranged side by side.Particularly advantageous is the creation of different areas that meet the individual needs of passengers, especially those traveling alone or in pairs. The design according to the invention allows for different comfort categories to be advantageously achieved for different passenger needs. Preferably, the aircraft seating arrangement is intended for use in an aircraft cabin. Preferably, the aircraft cabin is designed for all passengers during a flight, particularly regardless of the booked seating class. A seating class is, for example, configured as Economy Class, Premium Economy Class, Business Class, or First Class. Preferably, the aircraft cabin has at least one cabin section, particularly along an aircraft longitudinal axis.Preferably, the at least one aircraft cabin section is bounded along an aircraft longitudinal axis by at least one partition, in particular a partition wall or a curtain, and / or by at least one aircraft cabin module, in particular a galley module or a lavatory module. A seating class can be arranged in several aircraft cabin sections. Preferably, the aircraft cabin has a central axis. Preferably, the central axis is equidistant from opposing outer walls of the aircraft cabin. Preferably, the central axis is aligned parallel to a roll axis of the aircraft. Preferably, the central axis is aligned parallel to the aircraft cabin floor.The term "aircraft longitudinal axis" is understood to mean, in particular, an axis extending in the direction of the greatest extent of the aircraft cabin and located within the aircraft cabin. The aircraft longitudinal axis is preferably aligned parallel to the aircraft cabin's centerline. Preferably, the aircraft has a direction of flight in at least one operating state. Preferably, the direction of flight, particularly in an ideal operating state, is aligned parallel to the aircraft cabin's centerline and / or to an aircraft longitudinal axis. Preferably, the aircraft cabin has at least one aisle. Preferably, the at least one aisle extends at least substantially along an aircraft longitudinal axis. Preferably, the aircraft seating arrangements each form an aircraft seating area.The term "aircraft seating area" is understood to mean, in particular, an area available to a passenger in the aircraft cabin, especially while the passenger is sitting or lying in the aircraft seat. Preferably, the aircraft seating assemblies are designed to be mounted on the aircraft cabin floor. "Designed" is understood to mean, in particular, specifically designed and / or equipped. The fact that an object is designed for a specific function is understood to mean, in particular, that the object fulfills and / or performs this specific function in at least one application and / or operating state. Preferably, the aircraft seating assemblies each comprise an aircraft seat designed to provide a seat for a passenger in the aircraft.A "different arrangement of aircraft seats" shall be understood to mean, in particular, that the aircraft seats of the several aircraft seating configurations have different seating and / or reclining directions relative to one another, and / or that the aircraft seats of the several aircraft seating configurations have different, in particular minimum or maximum, distances to an aircraft cabin aisle. Furthermore, a "different arrangement of aircraft seats" shall be understood to mean, in particular, a different positioning of the aircraft seats within the respective aircraft seating areas.The term "different seating and / or reclining directions" shall be understood to mean, in particular, that the seating directions and / or reclining directions of the aircraft seating units have an angle greater than zero with each other, wherein the seating directions and / or reclining directions are aligned parallel to the aircraft cabin floor. Preferably, seating directions and / or reclining directions of the aircraft seating units, especially those differing in at least one comfort category, are aligned antiparallel or not parallel to each other. Preferably, the aircraft seating units of the multiple aircraft seating units are arranged consecutively along an aircraft longitudinal axis and / or side by side transversely to an aircraft longitudinal axis. Preferably, the arrangement, in particular the sequence, of the aircraft seating units of the multiple aircraft seating units may vary relative to each other.This allows for an advantageously variable aircraft seating arrangement with aircraft seating assemblies that can be combined in a variety of ways. "Differently designed" means, in particular, that the aircraft seating assemblies have similar components in the corresponding aircraft seating areas that are shaped differently, arranged differently, and / or function differently. In this context, a "component of an aircraft seating assembly" means, in particular, an aircraft seat, a console, an ottoman, an enclosure, a partition unit, a table unit, a screen, and / or a lighting device. "Similar" means, in particular, that the aircraft seating assemblies each consist of the same component.The term "differently shaped" is to be understood in particular as meaning that a shape, especially an outer contour, of identical aircraft seat components differs, particularly when viewed perpendicular to a plane parallel to the aircraft cabin floor. However, this does not include altered shapes of aircraft seat components due to environmental conditions, such as a curved contour of an aircraft cabin exterior wall.The term "at least partially differently designed" is to be understood in particular as meaning that a single aircraft seat configuration among several aircraft seat configurations, which is designed differently from at least one other aircraft seat configuration among several aircraft seat configurations, may be present multiple times in the aircraft seat configuration, thus allowing, in particular, several identically designed aircraft seat configurations to be present in the aircraft seat configuration. The term "comfort category" is to be understood in particular as a category that describes, and in particular quantifies, a property relating to the comfort of a passenger sitting and / or lying on the aircraft seat. The at least one comfort category is intended, in particular, to compare and / or differentiate the comfort between at least two of the several aircraft seat configurations.In principle, at least two aircraft seating configurations, but not all aircraft seating configurations, in the aircraft cabin section must differ in at least one comfort category. In principle, the aircraft seating configurations do not need to differ from one another in all values, particularly for multiple comfort categories. According to the invention, at least four differently designed aircraft seating configurations among the multiple aircraft seating configurations in the aircraft cabin section differ in at least one comfort category, wherein the aircraft seating configurations for the at least one comfort category each have a different value, which is due to the different arrangement of the aircraft seats and the at least partially different design of the aircraft seating configurations.A "value" is preferably understood to be a physical quantity that quantitatively describes the comfort category. In principle, it is conceivable that different booking classes and / or price categories are assigned to the various aircraft seating configurations, depending on at least one comfort category. This allows for advantageously selective booking of a desired aircraft seating configuration, thereby advantageously generating different revenues. Preferably, the aircraft seat comprises a seat base and a backrest. Preferably, the aircraft seat also includes a leg rest.A "seating direction" shall be understood to mean, in particular, a direction that is at least substantially parallel to the aircraft cabin floor, especially at a deviation of 3 degrees from the aircraft cabin floor, and at least substantially perpendicular to a theoretical, flat backrest oriented perpendicular to the aircraft cabin floor, wherein the direction corresponds to a normal on a front surface of the backrest, the front surface of the backrest forming a support surface for the back of a passenger in a normal sitting position. A "reclining direction" shall be understood to mean, in particular, a direction that is at least substantially parallel to the aircraft cabin floor, especially at a deviation of 3 degrees from the aircraft cabin floor, and, in the reclining position, runs along a common central axis of the backrest and the seat base. Preferably, the reclining direction corresponds to the sitting direction.In principle, the aircraft seat can include additional components, such as a headrest or at least one armrest. Preferably, each aircraft seat assembly has at least one console. It is particularly preferred that the at least one console be usable by two aircraft seats arranged immediately adjacent to each other. Preferably, the at least one console forms at least one footwell, at least one storage surface, and / or at least one storage compartment, wherein the at least one storage surface and / or the at least one storage compartment are specifically intended for an immediately adjacent aircraft seat assembly. Preferably, each aircraft seat assembly has at least one ottoman. In principle, the at least one ottoman can be connected to the at least one console. Preferably, the at least one ottoman is designed as a leg and / or footrest for a passenger.Preferably, the aircraft seating assemblies each have at least one housing. Preferably, the at least one housing is designed as a shell element. Preferably, the aircraft seat is adjustable between a sitting position and a reclining position, particularly electromechanically. Preferably, the aircraft seating assemblies each comprise at least one adjustment unit designed to adjust the aircraft seat between the sitting position and the reclining position. A "sitting position" is understood to mean, in particular, a position of the aircraft seat in which a passenger can sit upright on the aircraft seat. Preferably, in the sitting position, the backrest of the aircraft seat and the seat base of the aircraft seat are substantially perpendicular to each other, particularly at an angle between 90 degrees and 110 degrees. Preferably, the sitting position forms a first end position of the aircraft seat into which the aircraft seat can be adjusted to its maximum extent.Preferably, the seating position is configured as a TTL (Total Time to Load) position. A "TTL position" is understood to mean, in particular, an upright position of the aircraft seat that must be assumed for safety reasons, especially during taxiing, takeoff, and landing. A "reclined position" is understood to mean, in particular, a position of the aircraft seat designed to provide an at least substantially horizontal lying surface for a passenger, especially so that the passenger can assume a sleeping position during a flight. Preferably, in the reclined position of the aircraft seat, the passenger lies at least substantially on the aircraft seat, in particular on the seat base and the backrest. Preferably, the reclined position constitutes a second end position of the aircraft seat, into which the aircraft seat can be adjusted to its maximum extent.The term "at least substantially" shall be understood to mean, in particular, that a deviation from a predetermined value is less than 25%, preferably less than 10%, and most preferably less than 5% of the predetermined value. In principle, further positions may be provided between the sitting and reclining positions, which in particular form a combined sitting and reclining position. A "full-flat seat" shall be understood to mean, in particular, a seat that can be converted, preferably electromechanically, from the sitting position to the reclining position and, in the reclining position, forms a lying surface that is at least substantially flat. Preferably, the flat lying surface is inclined at an angle of 3 degrees to the aircraft cabin floor.Particularly preferred are at least the seat base and the backrest of the aircraft seat in the reclined position aligned at least substantially parallel to the aircraft cabin floor on which the aircraft seat is mounted. Preferably, the seat base and the backrest of the aircraft seat in the reclined position have a common contact surface that is aligned at least substantially parallel to the aircraft cabin floor.

[0009] Each of the multiple aircraft seating configurations has direct access to an aircraft cabin aisle. This design allows for advantageously simple and comfortable access to an aircraft seat, thus providing a particularly high level of comfort for the passenger. Furthermore, this design ensures a high level of passenger comfort because passengers in adjacent aircraft seating areas are not disturbed or inconvenienced by direct access to an aircraft cabin aisle. "Direct access" is understood to mean, in particular, access from an aircraft cabin aisle to an aircraft seating area, especially to a specific aircraft seat, where this access does not involve passing through an adjacent aircraft seating area.Preferably, the passenger can enter the aircraft seating area directly from the cabin aisle, particularly without having to cross another seating area. Preferably, the direct access is assigned to only one of the several aircraft seating configurations. More preferably, the direct access is only usable from one of the several aircraft seating configurations.

[0010] Furthermore, it is proposed that at least one comfort category describes a living space, in particular a floor area, bed length, bed width, footwell volume, and / or passage width in at least one area. This design allows aircraft seating configurations with advantageously variable comfort characteristics to be provided. This enables a suitably individualized level of comfort to be achieved for different passenger needs. A "living space" is understood to mean, in particular, a space, especially free space, within an aircraft seating area that can be used personally by a passenger.Particularly preferred is the at least one comfort category configured as a base surface of an aircraft seating device, as a storage surface of an aircraft seating device, in particular a console, as a table surface of an aircraft seating device, as a, in particular minimum or maximum, armroom for a passenger, in particular a limiting, maximum angle of movement starting from the seat direction in the seated position, as a, in particular maximum, support surface of an aircraft seat for a passenger, in particular in the seated or reclining position, as a, in particular maximum, bed length of an aircraft seat in the reclining position, as a, in particular maximum, bed width of the aircraft seat in the reclining position, as a, in particular maximum, footwell volume, as an aircraft seat orientation and / or as a, in particular minimum, passage width in at least one area of ​​the aircraft seating device.The footwell volume is preferably limited by a console. Preferably, the console is designed to define the footwell volume. "Aircraft seat orientation" refers in particular to the orientation of the seating direction and / or the reclining direction relative to an aircraft longitudinal axis and / or the direction of flight. Preferably, the passage width is defined as the minimum width of direct access from an aircraft cabin aisle into the aircraft seating area, directly adjacent to this cabin aisle and measured parallel to an aircraft longitudinal axis, and / or as the minimum width of direct access in an area between the cabin aisle and an area located immediately behind the seat base when viewed from the seated position. In principle, at least one comfort category can also describe a quality, noise level, and / or lighting.Quality can describe, in particular, seat upholstery, such as a foam core or a spring core, or contact material, such as fabric or leather. Noise can describe, in particular, the shielding of the aircraft seat from ambient noise from the aircraft cabin. Lighting can describe, in particular, the number of light sources and a property of the light sources.

[0011] Furthermore, the invention proposes that at least four aircraft seat assemblies of different designs are arranged directly one behind the other in a seat gap within the aircraft cabin section. This design allows for advantageously variable positioning of differently designed aircraft seat assemblies. This enables the provision of aircraft seat assemblies within a seat gap that advantageously differ in their comfort categories. This allows for advantageously individualized comfort to be achieved for different passenger needs.A "seat gap" is understood to mean, in particular, an area in the aircraft cabin in which at least one aircraft seat of several aircraft seats is arranged and which is bounded by at least one aircraft cabin aisle, wherein an axis arranged perpendicular to an aircraft longitudinal axis and parallel to the aircraft cabin floor intersects, in particular, only one aircraft seat within this area. Preferably, the seat gap extends in the direction of flight. Preferably, at least two aircraft seats are arranged one behind the other in a seat gap, all of which are intersected by the same aircraft longitudinal axis and each of which has direct access to the same aircraft cabin aisle. "One behind the other" is understood to mean, in particular, consecutively arranged along an aircraft longitudinal axis.The term "arranged directly one after the other" means, in particular, that no further object, especially no further aircraft seat, is arranged between the at least three aircraft seat assemblies of the multiple aircraft seat assemblies. Preferably, the at least three differently designed aircraft seat assemblies of the multiple aircraft seat assemblies are arranged directly one after the other in the direction of flight.

[0012] Furthermore, it is proposed that in the aircraft cabin section, one seating direction of one of the multiple aircraft seating assemblies is arranged in a seat gap at least substantially parallel to an aircraft longitudinal axis, and that another seating direction of the multiple aircraft seating assemblies is arranged at an angle of at least 18 degrees to the aircraft longitudinal axis. This design allows for an advantageously compact and variable arrangement of aircraft seating assemblies.

[0013] Furthermore, it is proposed that in the aircraft cabin section, at least one of the multiple aircraft seating configurations faces away from an immediately adjacent cabin aisle. This design allows the at least one aircraft seating configuration to be positioned particularly advantageously within the aircraft seating arrangement. Moreover, this design provides a significantly higher level of privacy for the passenger, thereby achieving a significantly higher level of comfort.

[0014] Furthermore, it is proposed that in the aircraft cabin section, at least one of the multiple aircraft seat configurations be oriented towards an immediately adjacent cabin aisle. This design allows the at least one aircraft seat configuration to be positioned particularly advantageously within the aircraft seating arrangement. Moreover, this design ensures advantageously easy access to the aircraft seat for a passenger, thereby achieving a significantly higher level of comfort.

[0015] Furthermore, it is proposed that the seating directions of at least two aircraft seating assemblies, which are spaced apart from each other, in particular by at least one further aircraft seating assembly, are arranged in a seat gap at an angle to an aircraft longitudinal axis of at least substantially the same magnitude, wherein the seating directions of the aircraft seating assemblies are mirrored with respect to an aircraft longitudinal axis. This design allows for an advantageously variable and compact aircraft seating arrangement. Furthermore, it enables several aircraft seating assemblies to be advantageously combined in a compact manner. This allows for an advantageously large number of aircraft seats to be provided in the aircraft cabin section.

[0016] Furthermore, it is proposed that one aircraft seat of an aircraft seating unit arranged in a seat gap within the aircraft cabin section be positioned facing the aisle, while another aircraft seat of an aircraft seating unit arranged in the same seat gap is positioned facing away from the aisle. This configuration allows for an advantageously variable and compact aircraft seating arrangement. Furthermore, it enables the advantageously compact combination of several aircraft seating units. This allows for the provision of an advantageously large number of aircraft seats within the aircraft cabin section. "Arranged facing the aisle" is understood to mean, in particular, that in the seated position, at least a large portion of the aircraft seat, viewed in the direction of flight, is located on a side of the aircraft seating unit facing the cabin aisle.The term "at least a large part" shall be understood to mean at least 55%, preferably at least 65%, and most preferably at least 75%. The term "arranged away from the aisle" shall be understood to mean, in particular, that in the seated position, at least a large part of the aircraft seat, viewed in the direction of flight, is arranged on a side of the aircraft seat assembly facing away from the aircraft cabin aisle. Preferably, the aircraft seat arranged facing the aisle has a smaller minimum distance to the aircraft cabin aisle than another aircraft seat arranged away from the aisle.

[0017] Furthermore, the invention proposes that the aircraft seating arrangement comprises at least one seating group of at least four aircraft seating units arranged directly one behind the other in a seat gap within the aircraft cabin section. These seating units may have different seating directions and / or their seats may be arranged facing the aisle or away from the aisle. This design allows several aircraft seating units to be advantageously combined in a compact and flexible manner. This enables a suitably large number of aircraft seats to be provided in the aircraft cabin section. Furthermore, this design allows for a repeatable sequence of the at least one seating group. Additionally, this design allows for the advantageous consideration of individual passenger needs, thereby enabling a particularly high level of comfort.A "seat grouping" is defined as an arrangement of at least four aircraft seats directly one behind the other in a seat column within the aircraft cabin section. Preferably, the at least one seat grouping forms a sequence that is repeatable, particularly periodically. Several identical seat groups can be arranged directly one behind the other, especially along an aircraft longitudinal axis.

[0018] Furthermore, it is proposed that the seating directions of the aircraft seating units arranged directly behind one another within the at least one seating group be arranged alternately at least substantially parallel and at an angle to the aircraft's longitudinal axis. This design allows for an advantageously variable and compact aircraft seating arrangement. Furthermore, it enables several aircraft seating units to be combined advantageously in a compact manner. This allows for a suitably large number of aircraft seats to be provided in the aircraft cabin section. Preferably, viewed in the direction of flight, an aircraft seating unit with a seating direction at an angle to the aircraft's longitudinal axis is arranged both in front of and behind an aircraft seating unit whose seating direction is arranged at least substantially parallel to the aircraft's longitudinal axis.Preferably, viewed in the direction of flight, an aircraft seat is arranged in front of and behind an aircraft seat whose seating direction is angled to the longitudinal axis of the aircraft, the seating direction of which is arranged at least substantially parallel to the longitudinal axis of the aircraft.

[0019] Furthermore, it is proposed that in the aircraft cabin section, within a seat gap, two aircraft seat assemblies of the multiple aircraft seat assemblies each have one aircraft seat facing the aisle, and two further aircraft seat assemblies of the multiple aircraft seat assemblies, which, viewed in a direction of flight, are arranged directly behind or in front of the two aircraft seat assemblies, each have one aircraft seat facing away from the aisle. This configuration allows for an advantageously variable and compact aircraft seat arrangement. Moreover, it enables the advantageously compact combination of multiple aircraft seat assemblies.

[0020] Furthermore, it is proposed that at least three aircraft seat assemblies of the multiple aircraft seat assemblies be arranged in a seat gap within the aircraft cabin section, wherein one seating direction of one aircraft seat assembly of the at least three aircraft seat assemblies is arranged at least substantially parallel to an aircraft longitudinal axis, and the seating directions of two further aircraft seat assemblies of the at least three aircraft seat assemblies are arranged at an angle to the aircraft longitudinal axis. This design allows for an advantageously variable and compact aircraft seat arrangement. Furthermore, it enables the advantageously compact combination of multiple aircraft seat assemblies. This allows for the provision of an advantageously large number of aircraft seats in the aircraft cabin section.Preferably, at least three of the aircraft seating devices are arranged directly one behind the other in a seat gap in the aircraft cabin section, wherein the seating directions of two of the aircraft seating devices are arranged at least substantially parallel to an aircraft longitudinal axis and a seating direction of another of the aircraft seating devices is arranged at an angle to the aircraft longitudinal axis.

[0021] Furthermore, it is proposed that aircraft seats in aircraft seating assemblies whose seating directions are angled to the aircraft's longitudinal axis have different distances to an aircraft cabin aisle. This design allows for an advantageously compact and variable arrangement of aircraft seating assemblies. "Different distances to an aircraft cabin aisle" is understood to mean, in particular, that the aircraft seats are arranged facing the aisle or away from it. Preferably, aircraft seats in aircraft seating assemblies whose seating directions are arranged at least substantially parallel to the aircraft's longitudinal axis have different distances to the aircraft cabin aisle.

[0022] Furthermore, it is proposed that in the aircraft cabin section, in at least one seat gap, four differently designed aircraft seat assemblies of the multiple aircraft seat assemblies are arranged directly one behind the other, wherein the seating directions of two aircraft seat assemblies of the four aircraft seat assemblies are arranged at least substantially parallel to an aircraft longitudinal axis, wherein one aircraft seat of one aircraft seat assembly of the two aircraft seat assemblies is arranged aisle-side and another aircraft seat of another aircraft seat assembly of the two aircraft seat assemblies is arranged away from the aisle, and the seating directions of two further aircraft seat assemblies of the four aircraft seat assemblies are arranged at an angle to the aircraft longitudinal axis.wherein one aircraft seat of one aircraft seating unit is arranged facing the aisle, and another aircraft seat of a third aircraft seating unit is arranged facing away from the aisle. This configuration allows for an advantageously compact and variable arrangement of the multiple aircraft seating units. Furthermore, this configuration allows for the advantageously simple combination of the multiple aircraft seating units. Additionally, this configuration allows for the particularly advantageous positioning of the multiple aircraft seating units relative to one another. This enables advantageously efficient use of available space. Furthermore, this configuration allows for advantageously different comfort categories to be achieved to meet different passenger needs.

[0023] Furthermore, it is proposed that in the aircraft cabin section, two aircraft seat assemblies from the multiple aircraft seat assemblies form a seat pair in two immediately adjacent seat gaps, wherein the seating directions of the two aircraft seat assemblies are arranged at least substantially parallel to an aircraft longitudinal axis and the aircraft seats of the two aircraft seat assemblies are arranged facing away from the aisle, with at least two of the seat pairs being arranged in the two immediately adjacent seat gaps. This design allows for an advantageously variable aircraft seat arrangement. This enables the adjacent aircraft seat assemblies from the multiple aircraft seat assemblies to be advantageously positioned variably relative to one another.This allows for the creation of distinct areas that cater to the individual needs of passengers, particularly those traveling alone or in pairs. A "pair of seats" is understood to mean, in particular, an arrangement of exactly two aircraft seats that are directly adjacent to one another and, in particular, are not separated by an aisle. Preferably, the two adjacent aircraft seats are mirror images of each other, especially about the central axis of the aircraft cabin. Preferably, the two aircraft seats of the multiple aircraft seats forming a pair are arranged flush with each other in the direction of flight, especially when viewed in a plane parallel to the aircraft cabin floor.Preferably, the two aircraft seating units of a multiple aircraft seating unit forming a pair of seats are arranged in a central area of ​​the aircraft cabin. A "central area" is understood to mean, in particular, an area in the middle of the aircraft cabin that is intersected by the cabin's central axis. Preferably, the central area is bounded by two cabin aisles. Particularly preferably, two seat gaps are arranged in the central area of ​​the aircraft cabin.

[0024] Furthermore, it is proposed that an arrangement of multiple aircraft seating units in at least one seating column on a first side of the cabin be configured asymmetrically to an arrangement of multiple aircraft seating units in at least one seating column on a second side of the cabin, wherein the first side of the cabin is separated from the second side by an imaginary cabin center plane oriented perpendicular to the cabin floor along the cabin center axis. This configuration allows for an advantageously variable aircraft seating arrangement. This enables the creation of different areas that meet the individual requirements of passengers. Preferably, the cabin center axis is located in the cabin center plane.Preferably, the first and second sides of the aircraft cabin each have an aisle. In principle, it is conceivable that the cabin section has at least one partition wall along the central axis separating the first and second sides.

[0025] Furthermore, it is proposed that at least one seating column should contain only aircraft seating units from the multiple aircraft seating units whose seating directions are angled to the aircraft's longitudinal axis. This design allows for a suitably compact aircraft seating arrangement.

[0026] Furthermore, it is proposed that at least one seat column should contain only aircraft seating units from among several aircraft seating units whose seating directions are arranged at least substantially parallel to the aircraft's longitudinal axis. This design allows for a suitably compact aircraft seating arrangement.

[0027] Furthermore, it is proposed that the seating directions of some of the multiple aircraft seating configurations in the aircraft cabin section be oriented at least substantially opposite to the direction of flight. This design allows for a suitably variable aircraft seating arrangement. Moreover, this design facilitates eye contact between passengers. Preferably, at least four, and in particular eight, differently configured aircraft seating configurations are arranged in the aircraft cabin section. It is conceivable that each of the differently configured aircraft seating configurations exists multiple times.

[0028] The aircraft seat arrangement according to the invention is not intended to be limited to the application and embodiment described above. In particular, the aircraft seat arrangement according to the invention may, to achieve a functionality described herein, comprise a different number of individual elements, components, and units than that specified herein. Drawings

[0029] Further advantages will become apparent from the following description of the drawings. The drawings illustrate seven exemplary embodiments of the invention. The drawings, the description, and the claims contain numerous features in combination. A person skilled in the art will expediently consider the features individually and combine them into meaningful further combinations, insofar as they fall within the scope of the claims.

[0030] They show: Fig. 1 an aircraft in a schematic representation in a first embodiment, Fig. 2 an aircraft seat arrangement according to the invention in a schematic representation in the first embodiment, Fig. 3 a section of the aircraft seat arrangement according to the invention in a schematic representation in the first embodiment, Fig. 4 the aircraft seat arrangement according to the invention in a schematic representation in the first embodiment, wherein the representation is identical to the one shown except for reference numerals. Fig. 2Fig. 5 is a schematic representation of an aircraft seat arrangement according to the invention in a second embodiment, Fig. 6 is a schematic representation of an unclaimed aircraft seat arrangement in a third embodiment, Fig. 7 is a schematic representation of an unclaimed aircraft seat arrangement in a fourth embodiment, Fig. 8 is a schematic representation of an aircraft seat arrangement according to the invention in a fifth embodiment, Fig. 9 is a schematic representation of an aircraft seat arrangement according to the invention in a sixth embodiment, and Fig. 10 is a schematic representation of an aircraft seat arrangement according to the invention in a seventh embodiment. Description of the exemplary implementations

[0031] The Figure 1 Figure 10a shows an aircraft. The aircraft 10a has an aircraft cabin 12a. The aircraft 10a has an aircraft seating arrangement 14a. Figures 2 to 4Figure 1 shows the aircraft seating arrangement 14a in a first embodiment. The aircraft seating arrangement 14a is intended for use in the partially illustrated aircraft cabin 12a of the aircraft 10a. The aircraft cabin 12a is designed to accommodate all passengers during a flight.

[0032] The aircraft cabin 12a has a cabin centerline 16a. The cabin centerline 16a is designed as a longitudinal axis of the aircraft. The cabin centerline 16a is equidistant from opposite outer walls 18a and 20a of the aircraft cabin 12a. The cabin centerline 16a is aligned parallel to a roll axis of the aircraft 10a. The cabin centerline 16a is aligned parallel to a cabin floor 22a of the aircraft cabin 12a. The aircraft 10a has a flight direction 24a in at least one operating state. In this case, the flight direction 24a is ideally aligned parallel to the cabin centerline 16a.

[0033] The aircraft cabin 12a has a cabin section 26a along the central axis 16a. Additionally, the aircraft cabin 12a may have at least one further cabin section, viewed in the direction of flight 24a, in particular in front of or behind cabin section 26a. In this case, cabin section 26a is bounded by several partitions 28a and by several schematically represented cabin modules 30a along the central axis 16a. The partitions 28a are each configured as a partition wall. The cabin modules 30a are each configured as a galley module, a lavatory module, a wardrobe, or a front-row monument.

[0034] The aircraft seating arrangement 14a comprises several aircraft seating units 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a arranged in the aircraft cabin section 26a. The aircraft seating units 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are designed to be mounted on the aircraft cabin floor 22a of the aircraft cabin 12a. In this case, the aircraft seating units 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are each configured as a business-class seating unit. The several aircraft seat devices 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are designed differently from each other.

[0035] The aircraft seating arrangement 14a comprises a first aircraft seating device 100a of several aircraft seating devices 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a. The first aircraft seating device 100a has a seating direction 110a. The seating direction 110a of the first aircraft seating device 100a is oriented in the direction of flight 24a. The seating direction 110a of the first aircraft seating device 100a corresponds to the direction of flight 24a. The seating direction 110a of the first aircraft seating device 100a is oriented at least substantially parallel to the aircraft cabin centerline 16a. The first aircraft seating device 100a has a reclining direction. In the present case, the reclining direction of the first aircraft seating device 100a corresponds to the seating direction 110a of the first aircraft seating device 100a.In principle, it is also conceivable that the reclining direction of an aircraft seat differs from the sitting direction of that aircraft seat, in particular by an angle of no more than 18 degrees. The reclining direction of the first aircraft seat 100a is aligned with the direction of flight 24a. The reclining direction of the first aircraft seat 100a corresponds to the direction of flight 24a. The reclining direction of the first aircraft seat 100a is aligned at least substantially parallel to the aircraft cabin centerline 16a.

[0036] The aircraft seating arrangement 14a comprises a second aircraft seating unit 200a of the multiple aircraft seating units 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a. The second aircraft seating unit 200a has a seating direction 210a. The seating direction 210a of the second aircraft seating unit 200a has a directional component in the direction of flight 24a. The seating direction 210a of the second aircraft seating unit 200a deviates from the direction of flight 24a. In this case, the seating direction 210a of the second aircraft seating unit 200a is angled at 30 degrees to the aircraft cabin center axis 16a. The second aircraft seating unit 200a has a reclining orientation. In the present case, the reclining direction of the second aircraft seat 200a corresponds to the sitting direction 210a of the second aircraft seat 200a. The reclining direction of the second aircraft seat 200a has a directional component in the direction of flight 24a.The reclining direction of the second aircraft seat 200a deviates from the flight direction 24a. In this case, the reclining direction of the second aircraft seat 200a is angled at 30 degrees to the aircraft cabin center axis 16a.

[0037] The aircraft seating arrangement 14a comprises a third aircraft seat 300a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a. The third aircraft seat 300a has a seating direction 310a. The seating direction 310a of the third aircraft seat 300a is oriented in the direction of flight 24a. The seating direction 310a of the third aircraft seat 300a corresponds to the direction of flight 24a. The seating direction 310a of the third aircraft seat 300a is oriented at least substantially parallel to the aircraft cabin centerline 16a. The third aircraft seat 300a has a reclining direction. In the present case, the reclining direction of the third aircraft seat 300a corresponds to the seating direction 310a of the third aircraft seat 300a. The reclining direction of the third aircraft seat 300a is aligned with the direction of flight 24a.The reclining direction of the third aircraft seat 300a corresponds to the flight direction 24a. The reclining direction of the third aircraft seat 300a is aligned at least substantially parallel to the aircraft cabin center axis 16a.

[0038] The aircraft seating arrangement 14a comprises a fourth aircraft seat 400a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a. The fourth aircraft seat 400a has a seating direction 410a. The seating direction 410a of the fourth aircraft seat 400a has a directional component in the direction of flight 24a. The seating direction 410a of the fourth aircraft seat 400a deviates from the direction of flight 24a. In this case, the seating direction 410a of the fourth aircraft seat 400a is angled at 30 degrees to the aircraft cabin center axis 16a. The fourth aircraft seat 400a has a reclining orientation. In the present case, the reclining direction of the fourth aircraft seat 400a corresponds to the sitting direction 410a of the fourth aircraft seat 400a. The reclining direction of the fourth aircraft seat 400a has a directional component in the direction of flight 24a.The reclining direction of the fourth aircraft seat 400a deviates from the flight direction 24a. In this case, the reclining direction of the fourth aircraft seat 400a is angled at 30 degrees to the aircraft cabin center axis 16a.

[0039] The first aircraft seat device 100a, the second aircraft seat device 200a, the third aircraft seat device 300a and the fourth aircraft seat device 400a are designed differently from each other.

[0040] The aircraft seating arrangement 14a comprises a fifth aircraft seating arrangement 500a of the multiple aircraft seating arrangements 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a. The fifth aircraft seating arrangement 500a is configured as a mirror image of the first aircraft seating arrangement 100a along a longitudinal axis of the aircraft, in particular along the aircraft cabin center axis 16a. The fifth aircraft seating arrangement 500a has a seating direction 510a. The seating direction 510a of the fifth aircraft seating arrangement 500a is oriented in the direction of flight 24a. The seating direction 510a of the fifth aircraft seating arrangement 500a corresponds to the direction of flight 24a. The seating direction 510a of the fifth aircraft seating arrangement 500a is oriented at least substantially parallel to the aircraft cabin center axis 16a. The fifth aircraft seat 500a has a reclining position.In the present case, the reclining direction of the fifth aircraft seat 500a corresponds to the sitting direction 510a of the fifth aircraft seat 500a. The reclining direction of the fifth aircraft seat 500a is aligned with the direction of flight 24a. The reclining direction of the fifth aircraft seat 500a corresponds to the direction of flight 24a. The reclining direction of the fifth aircraft seat 500a is aligned at least substantially parallel to the aircraft cabin centerline 16a.

[0041] The aircraft seating arrangement 14a comprises a sixth aircraft seat 600a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a. The sixth aircraft seat 600a is configured as a mirror image of the second aircraft seat 200a along a longitudinal axis of the aircraft, in particular along the central axis 16a of the aircraft cabin. The sixth aircraft seat 600a has a seating direction 610a. The seating direction 610a of the sixth aircraft seat 600a has a directional component in the direction of flight 24a.

[0042] The seating direction 610a of the sixth aircraft seat 600a deviates from the flight direction 24a. In this case, the seating direction 610a of the sixth aircraft seat 600a is angled at 30 degrees to the aircraft cabin center axis 16a. The sixth aircraft seat 600a has a reclining direction. In this case, the reclining direction of the sixth aircraft seat 600a corresponds to the seating direction 610a of the sixth aircraft seat 600a. The reclining direction of the sixth aircraft seat 600a has a directional component in the flight direction 24a. The reclining direction of the sixth aircraft seat 600a deviates from the flight direction 24a. In this case, the reclining direction of the sixth aircraft seat 600a is angled at 30 degrees to the aircraft cabin center axis 16a.

[0043] The aircraft seating arrangement 14a comprises a seventh aircraft seat 700a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a. The seventh aircraft seat 700a is configured as a mirror image of the third aircraft seat 300a along an aircraft longitudinal axis, in particular along the aircraft cabin center axis 16a. The seventh aircraft seat 700a has a seating direction 710a. The seating direction 710a of the seventh aircraft seat 700a is oriented in the direction of flight 24a. The seating direction 710a of the seventh aircraft seat 700a corresponds to the direction of flight 24a. The seating direction 710a of the seventh aircraft seat 700a is oriented at least substantially parallel to the aircraft cabin center axis 16a. The seventh aircraft seat unit 700a has a reclining position.In the present case, the reclining direction of the seventh aircraft seat 700a corresponds to the sitting direction 710a of the seventh aircraft seat 700a. The reclining direction of the seventh aircraft seat 700a is aligned with the direction of flight 24a. The reclining direction of the seventh aircraft seat 700a corresponds to the direction of flight 24a. The reclining direction of the seventh aircraft seat 700a is aligned at least substantially parallel to the aircraft cabin center axis 16a.

[0044] The aircraft seating arrangement 14a comprises an eighth aircraft seat 800a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a. The eighth aircraft seat 800a is configured as a mirror image of the fourth aircraft seat 400a along an aircraft longitudinal axis, in particular along the aircraft cabin center axis 16a. The eighth aircraft seat 800a has a seating direction 810a. The seating direction 810a of the eighth aircraft seat 800a has a directional component in the direction of flight 24a. The seating direction 810a of the eighth aircraft seat 800a differs from the direction of flight 24a. The seating direction 810a of the eighth aircraft seat 800a is, in this case, angled at 30 degrees to the aircraft cabin center axis 16a. The eighth aircraft seat 800a has a reclining orientation.In the present case, the reclining direction of the eighth aircraft seat 800a corresponds to the sitting direction 810a of the eighth aircraft seat 800a. The reclining direction of the eighth aircraft seat 800a has a directional component in the direction of flight 24a. The reclining direction of the eighth aircraft seat 800a deviates from the direction of flight 24a. In the present case, the reclining direction of the eighth aircraft seat 800a is angled at 30 degrees to the aircraft cabin center axis 16a.

[0045] The fifth aircraft seat device 500a, the sixth aircraft seat device 600a, the seventh aircraft seat device 700a and the eighth aircraft seat device 800a are designed differently from each other.

[0046] In the present case, the aircraft seating arrangement 14a comprises eight differently configured aircraft seating units 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a, each of which is present at least once in the aircraft seating arrangement 14a. The first aircraft seating unit 100a, the second aircraft seating unit 200a, the third aircraft seating unit 300a, the fourth aircraft seating unit 400a, the fifth aircraft seating unit 500a, the sixth aircraft seating unit 600a, the seventh aircraft seating unit 700a, and the eighth aircraft seating unit 800a are configured differently from one another. In the aircraft cabin section 26a, eight differently designed aircraft seat units 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are arranged in the present case.

[0047] Aircraft seating units 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a each contain one aircraft seat. The first aircraft seating unit, 100a, contains a first aircraft seat, 120a. The second aircraft seating unit, 200a, contains a second aircraft seat, 220a. The third aircraft seating unit, 300a, contains a third aircraft seat, 320a. The fourth aircraft seating unit, 400a, contains a fourth aircraft seat, 420a. The fifth aircraft seating unit, 500a, contains a fifth aircraft seat, 520a. The sixth aircraft seating unit, 600a, contains a sixth aircraft seat, 620a. The seventh aircraft seating unit, 700a, contains a seventh aircraft seat, 720a. The eighth aircraft seating unit, 800a, contains an eighth aircraft seat, 820a. Aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, 820a are each intended to provide a seat for a passenger not shown in aircraft 10a.Aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a each include a seat base. Aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a each include a backrest. Aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a each include a leg rest (not shown). Aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a each include an armrest. In the... Figure 3A seat base 140a, a backrest 150a, and an armrest 160a of the first aircraft seat 120a are provided with a reference numeral as examples. In this case, aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a are essentially identical in design. The only difference between aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a is the arrangement of the armrest. In addition, aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a may each include further, not specifically shown, add-on components, such as a headrest or at least one additional armrest. Aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a are each designed as a full-flat seat. Aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a are each adjustable between a sitting position and a reclining position. Figures 2and 3 Aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a are each shown in the seated position. Aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a each include at least one adjustment unit (not shown in detail) designed to electromechanically adjust the aircraft seat 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a between the seated and reclining positions. In principle, further positions may be provided between the seated and reclining positions, in particular those that form a combined seated and reclining position. The aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, 820a each form a lying surface that is at least essentially flat when in the reclining position.

[0048] Aircraft seating units 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a each have a console. The first aircraft seating unit, 100a, has a first console, 130a. The first console, 130a, is located away from the aisle. The second aircraft seating unit, 200a, has a second console, 230a. The second console, 230a, is located away from the aisle. The third aircraft seating unit, 300a, has a third console, 330a. The third console, 330a, is located towards the aisle. The fourth aircraft seating unit, 400a, has a fourth console, 430a. The fourth console, 430a, is located towards the aisle. The fifth aircraft seating unit, 500a, has a fifth console, 530a. The fifth console, 530a, is located away from the aisle. The sixth aircraft seat 600a has a sixth console 630a. The sixth console 630a is located away from the aisle. The seventh aircraft seat 700a has a seventh console 730a.The seventh console 730a is located on the aisle side. The eighth aircraft seat 800a has an eighth console 830a. The eighth console 830a is also located on the aisle side. Consoles 130a, 230a, 330a, 430a, 530a, 630a, 730a, and 830a can each be used by two aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a that are arranged directly adjacent to each other in a single seat column. Consoles 130a, 230a, 330a, 430a, 530a, 630a, 730a, and 830a can each be used by two aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a arranged directly behind one another. Consoles 130a, 230a, 330a, 430a, 530a, 630a, 730a, and 830a each form a storage surface. The storage area is intended for an aircraft seat 120a, 220a, 320a, 420a, 520a, 620a, 720a, 820a directly adjacent to a corresponding console 130a, 230a, 330a, 430a, 530a, 630a, 730a, 830a.In addition, consoles 130a, 230a, 330a, 430a, 530a, 630a, 730a, 830a can each provide at least one storage space, in particular for a life jacket module, for literature and / or for personal items.

[0049] The aircraft seating units 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a each comprise a table unit. In this case, the table unit is arranged on console 130a, 230a, 330a, 430a, 530a, 630a, 730a, and 830a. The table unit includes a swiveling and / or extendable table. The table can be positioned, at least partially, in an area above the seat base in at least one operating state.

[0050] Consoles 130a, 230a, 330a, 430a, 530a, 630a, 730a, and 830a each form a footwell (not shown in detail). These footwells are each associated with the aircraft seat 100a, 200a, 300a, 400a, 500a, 600a, 710a, and 810a, as viewed in the seating direction, directly in front of the aircraft seat 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a. Aircraft seating configurations 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a each feature an ottoman (not shown in detail). The ottomans are located within consoles 130a, 230a, 330a, 430a, 530a, 630a, 730a, and 830a. Each ottoman serves as a leg and / or footrest for a passenger.The ottomans are each assigned to the aircraft seating device 100a, 200a, 300a, 410a, 510a, 610a, 710a, 810a, viewed in the direction of seating 110a, 210a, 310a, 410a, 510a, 610a, 710a, 810a, as viewed directly in front of this aircraft seating device 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a.

[0051] Aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a each have an enclosure. The enclosures are each designed as a single shell element. Viewed in the direction of flight 24a, the enclosures are positioned in front of the corresponding aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a. The enclosures are designed to visually separate aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a that are arranged directly behind one another. In this case, the housings are each connected to a console 130a, 230a, 330a, 430a, 530a, 630a, 730a, 830a. In principle, housings for several of the aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a can also be formed as a single unit.

[0052] Aircraft seating units 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a each include a screen. The screens are each located on the rear side of the housing. Each screen is assigned to the aircraft seating unit 100a, 200a, 300a, 400a, 500a, 610a, 710a, 800a, as viewed in the seating direction, directly in front of that aircraft seating unit 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a.

[0053] The aircraft seating configurations 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a each feature at least one partition unit designed to visually shield the aircraft seating area from its surroundings as needed. This advantageously enhances privacy. The partition unit includes at least one adjustable partition element, which may, for example, be a sliding door.

[0054] Aircraft seating units 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a each form an aircraft seating section. Within each aircraft seating section, the corresponding aircraft seats 120a, 220a, 320a, 420a, 520a, 620a, 720a, and 820a from aircraft seating units 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a are arranged. Each aircraft seating section is intended for one passenger to occupy during a flight. The aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a have differently shaped and / or differently arranged components in the corresponding aircraft seat areas. Therefore, the first aircraft seat assembly 100a, the second aircraft seat assembly 200a, the third aircraft seat assembly 300a, and the fourth aircraft seat assembly 400a are designed differently from one another.Furthermore, the fifth aircraft seat 500a, the sixth aircraft seat 600a, the seventh aircraft seat 700a, and the eighth aircraft seat 800a are designed differently from one another. In particular, the arrangement and orientation of the aircraft seats 120a, 220a, 320a, and 420a in their respective seating areas differ between the first aircraft seat 100a, the second aircraft seat 200a, the third aircraft seat 300a, and the fourth aircraft seat 400a. Furthermore, the arrangement and orientation of the aircraft seats 520a, 620a, 720a, and 820a in their respective seating areas differ between the fifth aircraft seat 500a, the sixth aircraft seat 600a, the seventh aircraft seat 700a, and the eighth aircraft seat 800a.

[0055] In the present case, aircraft cabin 12a has two cabin aisles 32a and 34a in cabin section 26a. Aircraft cabin 12a has a first cabin aisle 32a and a second cabin aisle 34a. Alternatively, it would also be conceivable that aircraft cabin 12a has only one cabin aisle. The cabin aisles 32a and 34a each extend at least substantially along a longitudinal axis of the aircraft (not shown in detail). Each of the several aircraft seating configurations 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a has direct access to either the first cabin aisle 32a or the second cabin aisle 34a. The first aircraft seating configuration 100a has direct access to the first cabin aisle 32a. The second aircraft seating unit 200a has direct access to the first aircraft cabin aisle 32a.The third aircraft seat unit 300a has direct access to the first aircraft cabin aisle 32a. The fourth aircraft seat unit 400a has direct access to the first aircraft cabin aisle 32a. The fifth aircraft seat unit 500a has direct access to the second aircraft cabin aisle 34a. The sixth aircraft seat unit 600a has direct access to the second aircraft cabin aisle 34a. The seventh aircraft seat unit 700a has direct access to the second aircraft cabin aisle 34a. The eighth aircraft seat unit 800a has direct access to the second aircraft cabin aisle 34a. The aircraft seating areas are each accessible from either the first aircraft cabin aisle 32a or the second aircraft cabin aisle 34a.

[0056] In the present case, the aircraft seating arrangement 14a comprises four seat columns 36a, 38a, 40a, and 42a. Alternatively, it would also be conceivable that the aircraft seating arrangement 14a has only two or three seat columns. The aircraft seating arrangement 14a comprises a first outer seat column 36a and a first inner seat column 38a. The first outer seat column 36a and the first inner seat column 38a are separated from each other by the first aircraft cabin aisle 32a. The aircraft seating arrangement 14a comprises a second inner seat column 40a and a second outer seat column 42a. The second outer seat column 42a and the second inner seat column 40a are separated from each other by the second aircraft cabin aisle 34a. In the present case, the first inner seat column 38a is symmetrical to the second inner seat column 40a about the aircraft cabin center axis 16a.In the present case, the first outer seat column 36a is symmetrically arranged with respect to the second outer seat column 42a along the aircraft cabin's central axis 16a. The first inner seat column 38a and the second inner seat column 40a are arranged directly adjacent to each other. The aircraft cabin 12a has a central section 44a. The central section 44a is bounded by the two aircraft cabin aisles 32a and 34a. The first inner seat column 38a and the second inner seat column 40a are arranged in the central section 44a. The first inner seat column 38a and the second inner seat column 40a form a double seat column. The first console 130a and the fifth console 530a are arranged directly adjacent to each other in the central section 44a and, in particular, are not separated from each other by an aircraft seat.The first console 130a and the fifth console 530a are arranged directly next to each other in the central area 44a and, in particular, are not separated from each other by an aircraft seat. It would also be conceivable that only one row of seats is arranged in the central area 44a. It is also conceivable that the first inner row of seats 38a is interchangeable with the second outer row of seats 42a and / or the second inner row of seats 40a is interchangeable with the first outer row of seats 36a.

[0057] The first aircraft seat 100a and the fifth aircraft seat 500a are arranged directly next to each other. The second aircraft seat 200a and the sixth aircraft seat 600a are arranged directly next to each other. The third aircraft seat 300a and the seventh aircraft seat 700a are arranged directly next to each other. The fourth aircraft seat 400a and the eighth aircraft seat 800a are arranged directly next to each other.

[0058] In the present case, the aircraft seating arrangement 14a comprises several further first aircraft seating assemblies 100'a, which are designed at least substantially identically to the first aircraft seating assembly 100a. "At least substantially identical" in this context means, in particular, that the respective further aircraft seating assemblies are designed identically to the corresponding aircraft seating assembly located in the central area 44a of the aircraft cabin 12a, except for a possible modification of the shape of a housing, a console, and / or an aircraft seat due to a contour of an aircraft cabin outer wall 18a, 20a. The further first aircraft seating assemblies 100'a are each located in the first inner seat column 38a or in the second outer seat column 42a.In the present case, the aircraft seating arrangement 14a comprises several further second aircraft seating assemblies 200'a, which are designed at least substantially identically to the second aircraft seating assembly 200a. The further second aircraft seating assemblies 200'a are each arranged in the first inner seat column 38a or in the second outer seat column 42a. In the present case, the aircraft seating arrangement 14a comprises several further third aircraft seating assemblies 300'a, which are designed at least substantially identically to the third aircraft seating assembly 300a. The further third aircraft seating assemblies 300'a are each arranged in the first inner seat column 38a or in the second outer seat column 42a. In the present case, the aircraft seating arrangement 14a comprises several further fourth aircraft seating assemblies 400'a, which are designed at least substantially identically to the fourth aircraft seating assembly 400a.The further fourth aircraft seating assemblies 400'a are each arranged in the first inner seating column 38a or in the second outer seating column 42a. In the present case, the aircraft seating assembly 14a comprises several further fifth aircraft seating assemblies 500'a, which are designed at least substantially identically to the fifth aircraft seating assembly 500a. The further fifth aircraft seating assemblies 500'a are each arranged in the second inner seating column 40a or in the first outer seating column 36a. In the present case, the aircraft seating assembly 14a comprises several further sixth aircraft seating assemblies 600'a, which are designed at least substantially identically to the sixth aircraft seating assembly 600a. The further sixth aircraft seating assemblies 600'a are each arranged in the second inner seating column 40a or in the first outer seating column 36a.In the present case, the aircraft seating arrangement 14a comprises several further seventh aircraft seating assemblies 700'a, which are designed at least substantially identically to the seventh aircraft seating assembly 700a. The further seventh aircraft seating assemblies 700'a are each arranged in the second inner seat column 40a or in the first outer seat column 36a. In the present case, the aircraft seating arrangement 14a comprises several further eighth aircraft seating assemblies 800'a, which are designed at least substantially identically to the eighth aircraft seating assembly 800a. The further eighth aircraft seating assemblies 800'a are each arranged in the second inner seat column 40a or in the first outer seat column 36a. For the sake of clarity, the following is shown in the... Figure 2 only a selection of further aircraft seating devices 100'a, 200'a, 300'a, 400'a, 500'a, 600'a, 700'a, 800'a with a reference mark.

[0059] In aircraft cabin section 26a, the seating direction 110a of the first aircraft seat 100a of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a in the first inner seat column 38a is aligned at least substantially parallel to the aircraft cabin center axis 16a. The first aircraft seat 120a of the first aircraft seat assembly 100a of the aircraft seat assemblies 100a, 200a, 300a, 400a arranged in the first inner seat column 38a of aircraft cabin section 26a is aisle-side.

[0060] In aircraft cabin section 26a, the seating direction 210a of the second aircraft seat 200a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a is arranged in the first inner seat column 38a at an angle of at least 18 degrees to the aircraft cabin center axis 16a. In the present case, in aircraft cabin section 26a, the seating direction 210a of the second aircraft seat 200a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a is arranged in the first inner seat column 38a at an angle of 30 degrees to the aircraft cabin center axis 16a. In the aircraft cabin section 26a, in the first inner seat column 38a, the seating direction 210a of the second aircraft seat arrangement 200a of the several aircraft seat arrangements 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a is directed away from the immediately adjacent first aircraft cabin aisle 32a.The second aircraft seat 220a of the second aircraft seat assembly 200a of the aircraft seat assemblies 100a, 200a, 300a, 400a arranged in the first inner seat column 38a in the aircraft cabin section 26a is arranged on the aisle side.

[0061] In aircraft cabin section 26a, the seating direction 310a of the third aircraft seat 300a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a in the first inner seat column 38a is aligned at least substantially parallel to the aircraft cabin center axis 16a. The third aircraft seat 320a of the third aircraft seat assemblies 300a of the aircraft seat assemblies 100a, 200a, 300a, 400a arranged in the first inner seat column 38a is located away from the aisle.

[0062] In aircraft cabin section 26a, the seating direction 410a of the fourth aircraft seat 400a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a is arranged in the first inner seat column 38a at an angle of at least 18 degrees to the aircraft cabin center axis 16a. In the present case, in aircraft cabin section 26a, the seating direction 410a of the fourth aircraft seat 400a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a is arranged in the first inner seat column 38a at an angle of 30 degrees to the aircraft cabin center axis 16a. In the aircraft cabin section 26a, in the first inner seat column 38a, the seating direction 410a of the fourth aircraft seat arrangement 400a of the several aircraft seat arrangements 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a is directed towards the immediately adjacent first aircraft cabin aisle 32a.The fourth aircraft seat 420a of the fourth aircraft seat assembly 400a of the aircraft seat assemblies 100a, 200a, 300a, 400a arranged in the first inner seat column 38a is arranged facing away from the aisle.

[0063] The seating directions 210a, 410a of the second aircraft seat 200a and the fourth aircraft seat 400a are arranged in the first inner seat column 38a at an angle of at least substantially the same magnitude to an aircraft longitudinal axis, wherein the seating directions 210a, 410a of the second aircraft seat 200a and the fourth aircraft seat 400a are mirror images of this aircraft longitudinal axis. The first aircraft seat 100a and the third aircraft seat 300a are spaced apart from each other by the second aircraft seat 200a. The second aircraft seat 200a and the fourth aircraft seat 400a are spaced apart from each other by the third aircraft seat 300a.

[0064] In the aircraft cabin section 26a, in the first inner seat column 38a, the first aircraft seat 100a and the second aircraft seat 200a each have one aircraft seat 120a, 220a, which is arranged on the aisle side, and the third aircraft seat 300a and the fourth aircraft seat 400a, which are arranged directly behind or in front of the two aircraft seat assemblies 100a, 200a when viewed in the direction of flight 24a, each have one aircraft seat 320a, 420a, which is arranged away from the aisle. The aircraft seats 120a, 320a of the aircraft seat assemblies 100a, 300a, whose seating directions 110a, 310a are arranged at least substantially parallel to the aircraft cabin center axis 16a, have different distances to the first aircraft cabin aisle 32a.The aircraft seats 220a, 420a of the aircraft seating arrangements 200a, 400a, whose seating directions 210a, 410a are arranged at an angle to the aircraft cabin center axis 16a, have different distances to the first aircraft cabin aisle 32a.

[0065] In the aircraft cabin section 26a, at least three aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are arranged in the first inner seat column 38a, namely at least the first aircraft seat assembly 100a, the second aircraft seat assembly 200a and the third aircraft seat assembly 300a, wherein the seating directions 110a, 310a of the first aircraft seat assembly 100a and the third aircraft seat assembly 300a are arranged at least substantially parallel to the aircraft cabin center axis 16a and the seating direction 210a of the second aircraft seat assembly 200a is arranged at an angle to the aircraft cabin center axis 16a.In the aircraft cabin section 26a, in the first inner seat column 38a, at least three aircraft seat devices of the several aircraft seat devices 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a, namely at least the first aircraft seat device 100a, the second aircraft seat device 200a and the third aircraft seat device 300a, are arranged directly one behind the other, wherein the seating directions 110a, 310a of the first aircraft seat device 100a and the third aircraft seat device 300a are arranged at least substantially parallel to the aircraft cabin center axis 16a and the seating direction 210a of the second aircraft seat device 200a is arranged at an angle to the aircraft cabin center axis 16a.

[0066] In the aircraft cabin section 26a, at least three aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are arranged in the first inner seat column 38a, namely at least the second aircraft seat assembly 200a, the third aircraft seat assembly 300a and the fourth aircraft seat assembly 400a, wherein the seating direction 310a of the third aircraft seat assembly 300a is arranged at least substantially parallel to the aircraft cabin center axis 16a and seating directions 210a, 410a of the second aircraft seat assembly 200a and the fourth aircraft seat assembly 400a are arranged at an angle to the aircraft cabin center axis 16a.In the aircraft cabin section 26a, in the first inner seat column 38a, at least three aircraft seat devices of the several aircraft seat devices 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a, namely at least the second aircraft seat device 200a, the third aircraft seat device 300a and the fourth aircraft seat device 400a, are arranged directly one behind the other, wherein the seating direction 310a of the third aircraft seat device 300a is arranged at least substantially parallel to the aircraft cabin center axis 16a and seating directions 210a, 410a of the second aircraft seat device 200a and the fourth aircraft seat device 400a are arranged at an angle to the aircraft cabin center axis 16a.

[0067] In the aircraft cabin section 26a, at least three aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are arranged in the first inner seat column 38a, namely at least one of the further fourth aircraft seat assemblies 400'a, the first aircraft seat assembly 100a and the second aircraft seat assembly 200a, wherein the seating direction 110a of the first aircraft seat assembly 100a is arranged at least substantially parallel to the aircraft cabin center axis 16a and seating directions of the second aircraft seat assembly 200a and the further fourth aircraft seat assembly 400'a are arranged at an angle to the aircraft cabin center axis 16a.In the aircraft cabin section 26a, in the first inner seat column 38a, at least three aircraft seat devices of the several aircraft seat devices 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a, namely at least one of the further fourth aircraft seat devices 400'a, the first aircraft seat device 100a and the second aircraft seat device 200a, are arranged directly one behind the other, wherein the seating direction 110a of the first aircraft seat device 100a is arranged at least substantially parallel to the aircraft cabin center axis 16a and seating directions of the second aircraft seat device 200a and the further fourth aircraft seat device 400'a are arranged at an angle to the aircraft cabin center axis 16a.

[0068] In the aircraft cabin section 26a, at least three aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are arranged in the first inner seat column 38a, namely at least the first aircraft seat assembly 100a, one of the further fourth aircraft seat assemblies 400'a and one of the further third aircraft seat assemblies 300'a, wherein the seating directions of the first aircraft seat assembly 100a and the further third aircraft seat assembly 300'a are arranged at least substantially parallel to the aircraft cabin center axis 16a and one seating direction of the further fourth aircraft seat assembly 400'a is arranged at an angle to the aircraft cabin center axis 16a.In the aircraft cabin section 26a, in the first inner seat column 38a, at least three aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a, namely at least the first aircraft seat assembly 100a, one of the further fourth aircraft seat assemblies 400'a and one of the further third aircraft seat assemblies 300'a, are arranged directly one behind the other, wherein the seating directions of the first aircraft seat assembly 100a and the further third aircraft seat assembly 300'a are arranged at least substantially parallel to the aircraft cabin center axis 16a and one seating direction of the further fourth aircraft seat assembly 400'a is arranged at an angle to the aircraft cabin center axis 16a.

[0069] In the aircraft cabin section 26a, four differently configured aircraft seat assemblies 100a, 200a, 300a, 400a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are arranged in the first inner seat column 38a, directly one behind the other. The four differently configured aircraft seat assemblies 100a, 200a, 300a, 400a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a of the first inner seat column 38a are arranged directly following one another in the direction of flight 24a.

[0070] In aircraft cabin section 26a, the first aircraft seat 100a, the second aircraft seat 200a, and the third aircraft seat 300a are arranged directly one behind the other in the first inner seat column 38a. In aircraft cabin section 26a, the second aircraft seat 200a, the third aircraft seat 300a, and the fourth aircraft seat 400a are arranged directly one behind the other in the first inner seat column 38a. In aircraft cabin section 26a, in the first inner seat column 38a, the first aircraft seat 100a is located directly behind the second aircraft seat 200a when viewed in the direction of flight 24a. In aircraft cabin section 26a, in the first inner seat column 38a, the second aircraft seat 200a is located directly behind the third aircraft seat 300a when viewed in the direction of flight 24a.In aircraft cabin section 26a, in the first inner seat column 38a, the third aircraft seat 300a, viewed in the direction of flight 24a, is located directly behind the fourth aircraft seat 400a. In principle, the fourth aircraft seat 400a can be located in aircraft cabin section 26a, in the first inner seat column 38a, viewed in the direction of flight 24a, directly behind the first aircraft seat 100a.

[0071] In the aircraft cabin section 26a, in the first inner seat column 38a, four differently configured aircraft seat assemblies are located, namely the first aircraft seat assembly 100a, the second aircraft seat assembly 200a, the third aircraft seat assembly 300a and the fourth aircraft seat assembly 400a, of which several aircraft seat assemblies 100a, 100'a, 200a, 200'a, 300a, 300'a, 400a, 400'a, 500a, 500'a, 600a, 600'a, 700a, 700'a, 800a, 800'a are arranged directly one behind the other, with seating directions 110a, 310a of two aircraft seat assemblies of the four aircraft seat assemblies 100a, 200a, 300a, 400a, namely the first aircraft seat assembly 100a and the third aircraft seat assembly 300a are arranged at least substantially parallel to the aircraft cabin center axis 16a,wherein the first aircraft seat 120a of the first aircraft seat assembly 100a is arranged aisle-side and the third aircraft seat 320a of the third aircraft seat assembly 300a is arranged away from the aisle, and seating directions 210a, 410a of two further aircraft seat assemblies of the four aircraft seat assemblies 100a, 200a, 300a, 400a, namely the second aircraft seat assembly 200a and the fourth aircraft seat assembly 400a, are arranged at an angle to the aircraft cabin center axis 16a, wherein the second aircraft seat 220a of the second aircraft seat assembly 200a is arranged aisle-side and the fourth aircraft seat 420a of the fourth aircraft seat assembly 400a is arranged away from the aisle.

[0072] In aircraft cabin section 26a, the seating direction 510a of the fifth aircraft seat 500a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a in the second inner seat column 40a is aligned at least substantially parallel to the aircraft cabin center axis 16a. The fifth aircraft seat 520a of the fifth aircraft seat assemblies 500a, 600a, 700a, 800a arranged in the second inner seat column 40a of aircraft cabin section 26a is located on the aisle side.

[0073] In aircraft cabin section 26a, the seating direction 610a of the sixth aircraft seat 600a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a is arranged in the second inner seat column 40a at an angle of at least 18 degrees to the aircraft cabin center axis 16a. In the present case, in aircraft cabin section 26a, the seating direction 610a of the sixth aircraft seat 600a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a is arranged in the second inner seat column 40a at an angle of 30 degrees to the aircraft cabin center axis 16a. In the aircraft cabin section 26a, in the second inner seat column 40a, the seating direction 610a of the sixth aircraft seat arrangement 600a of the several aircraft seat arrangements 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a is directed away from the immediately adjacent second aircraft cabin aisle 34a.The sixth aircraft seat 620a of the sixth aircraft seat assembly 600a of the aircraft seat assemblies 500a, 600a, 700a, 800a arranged in the second inner seat column 40a of the aircraft cabin section 26a is arranged on the aisle side.

[0074] In aircraft cabin section 26a, the seating direction 710a of the seventh aircraft seat 700a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a in the second inner seat column 40a is aligned at least substantially parallel to the aircraft cabin center axis 16a. The seventh aircraft seat 720a of the seventh aircraft seat assemblies 700a of the aircraft seat assemblies 500a, 600a, 700a, 800a arranged in the second inner seat column 40a is located away from the aisle.

[0075] In aircraft cabin section 26a, in the second inner seat column 40a, the seating direction 810a of the eighth aircraft seat 800a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a is arranged at an angle of at least 18 degrees to the aircraft cabin center axis 16a. In the present case, in aircraft cabin section 26a, in the second inner seat column 40a, the seating direction 810a of the eighth aircraft seat 800a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a is arranged at an angle of 30 degrees to the aircraft cabin center axis 16a. In the aircraft cabin section 26a, in the second inner seat column 40a, the seating direction 810a of the eighth aircraft seat arrangement 800a of the several aircraft seat arrangements 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a is directed towards the immediately adjacent second aircraft cabin aisle 34a.The eighth aircraft seat 820a of the eighth aircraft seat assembly 800a of the aircraft seat assemblies 500a, 600a, 700a, 800a arranged in the second inner seat column 40a is arranged facing away from the aisle.

[0076] The seating directions 610a, 810a of the sixth aircraft seat 600a and the eighth aircraft seat 800a are arranged in the second inner seat column 40a at an angle of at least substantially the same magnitude to an aircraft longitudinal axis, wherein the seating directions 610a, 810a of the sixth aircraft seat 600a and the eighth aircraft seat 800a are mirror images of this aircraft longitudinal axis. The fifth aircraft seat 500a and the seventh aircraft seat 700a are spaced apart from each other by the sixth aircraft seat 600a. The sixth aircraft seat 600a and the eighth aircraft seat 800a are spaced apart from each other by the seventh aircraft seat 700a.

[0077] In aircraft cabin section 26a, in the second inner seat column 40a, the fifth aircraft seat 500a and the sixth aircraft seat 600a each have one aircraft seat 520a, 620a, which is arranged aisle-side, and the seventh aircraft seat 700a and the eighth aircraft seat 800a, which are arranged directly behind or in front of the two aircraft seat assemblies 500a, 600a when viewed in the direction of flight 24a, each have one aircraft seat 720a, 820a, which is arranged away from the aisle. The aircraft seats 520a, 720a of the aircraft seat assemblies 500a, 700a, whose seating directions 510a, 710a are arranged at least substantially parallel to the aircraft cabin center axis 16a, have different distances to the second aircraft cabin aisle 34a.The aircraft seats 620a, 820a of the aircraft seating arrangements 600a, 800a, whose seating directions 610a, 810a are arranged at an angle to the aircraft cabin center axis 16a, have different distances to the second aircraft cabin aisle 34a.

[0078] In the aircraft cabin section 26a, at least three aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are arranged in the second inner seat column 40a, namely at least the fifth aircraft seat assembly 500a, the sixth aircraft seat assembly 600a and the seventh aircraft seat assembly 700a, wherein the seating directions 510a, 710a of the fifth aircraft seat assembly 500a and the seventh aircraft seat assembly 700a are arranged at least substantially parallel to the aircraft cabin center axis 16a and the seating direction 610a of the sixth aircraft seat assembly 600a is arranged at an angle to the aircraft cabin center axis 16a.In the aircraft cabin section 26a, in the second inner seat column 40a, at least three aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a, namely at least the fifth aircraft seat assembly 500a, the sixth aircraft seat assembly 600a and the seventh aircraft seat assembly 700a, are arranged directly one behind the other, wherein the seating directions 510a, 710a of the fifth aircraft seat assembly 500a and the seventh aircraft seat assembly 700a are arranged at least substantially parallel to the aircraft cabin center axis 16a and the seating direction 610a of the sixth aircraft seat assembly 600a is arranged at an angle to the aircraft cabin center axis 16a.

[0079] In the aircraft cabin section 26a, at least three aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are arranged in the second inner seat column 40a, namely at least the sixth aircraft seat assembly 600a, the seventh aircraft seat assembly 700a and the eighth aircraft seat assembly 800a, wherein the seating direction 710a of the seventh aircraft seat assembly 700a is arranged at least substantially parallel to the aircraft cabin center axis 16a and seating directions 610a, 810a of the sixth aircraft seat assembly 600a and the eighth aircraft seat assembly 800a are arranged at an angle to the aircraft cabin center axis 16a.In the aircraft cabin section 26a, in the second inner seat column 40a, at least three aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a, namely at least the sixth aircraft seat assembly 600a, the seventh aircraft seat assembly 700a and the eighth aircraft seat assembly 800a, are arranged directly one behind the other, wherein the seating direction 710a of the seventh aircraft seat assembly 700a is arranged at least substantially parallel to the aircraft cabin center axis 16a and seating directions 610a, 810a of the sixth aircraft seat assembly 600a and the eighth aircraft seat assembly 800a are arranged at an angle to the aircraft cabin center axis 16a.

[0080] In the aircraft cabin section 26a, at least three aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are arranged in the second inner seat column 40a, namely at least one of the further eighth aircraft seat assemblies 800'a, the fifth aircraft seat assembly 500a and the sixth aircraft seat assembly 600a, wherein the seating direction 510a of the fifth aircraft seat assembly 500a is arranged at least substantially parallel to the aircraft cabin center axis 16a and seating directions of the sixth aircraft seat assembly 600a and the further eighth aircraft seat assembly 800'a are arranged at an angle to the aircraft cabin center axis 16a.In the aircraft cabin section 26a, in the second inner seat column 40a, at least three aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a, namely at least one of the further eighth aircraft seat assemblies 800'a, the fifth aircraft seat assembly 500a and the sixth aircraft seat assembly 600a, are arranged directly one behind the other, wherein the seating direction 510a of the fifth aircraft seat assembly 500a is arranged at least substantially parallel to the aircraft cabin center axis 16a and seating directions of the sixth aircraft seat assembly 600a and the further eighth aircraft seat assembly 800'a are arranged at an angle to the aircraft cabin center axis 16a.

[0081] In the aircraft cabin section 26a, at least three aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are arranged in the second inner seat column 40a, namely at least the fifth aircraft seat assembly 500a, one of the further eighth aircraft seat assemblies 800'a and one of the further seventh aircraft seat assemblies 700'a, wherein the seating directions of the fifth aircraft seat assembly 500a and the further seventh aircraft seat assembly 700'a are arranged at least substantially parallel to the aircraft cabin center axis 16a and one seating direction of the further eighth aircraft seat assembly 800'a is arranged at an angle to the aircraft cabin center axis 16a.In the aircraft cabin section 26a, in the second inner seat column 40a, at least three aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a, namely at least the fifth aircraft seat assembly 500a, one of the further eighth aircraft seat assemblies 800'a and one of the further seventh aircraft seat assemblies 700'a, are arranged directly one behind the other, wherein the seating directions of the fifth aircraft seat assembly 500a and the further seventh aircraft seat assembly 700'a are arranged at least substantially parallel to the aircraft cabin center axis 16a and one seating direction of the further eighth aircraft seat assembly 800'a is arranged at an angle to the aircraft cabin center axis 16a.

[0082] In aircraft cabin section 26a, four differently configured aircraft seat assemblies 500a, 600a, 700a, 800a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a are arranged in the second inner seat column 40a, directly one behind the other. The four differently configured aircraft seat assemblies 500a, 600a, 700a, 800a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a of the multiple aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a of the second inner seat column 40a are arranged directly one after the other in the direction of flight 24a.

[0083] In aircraft cabin section 26a, the fifth aircraft seat 500a, the sixth aircraft seat 600a, and the seventh aircraft seat 700a are arranged directly one behind the other in the second inner seat column 40a. In aircraft cabin section 26a, the sixth aircraft seat 600a, the seventh aircraft seat 700a, and the eighth aircraft seat 800a are arranged directly one behind the other in the second inner seat column 40a. In aircraft cabin section 26a, in the second inner seat column 40a, the fifth aircraft seat 500a is located directly behind the sixth aircraft seat 600a when viewed in the direction of flight 24a. In aircraft cabin section 26a, in the second inner seat column 40a, the sixth aircraft seat 600a is located directly behind the seventh aircraft seat 700a when viewed in the direction of flight 24a.In aircraft cabin section 26a, in the second inner seat column 40a, the seventh aircraft seat 700a, viewed in the direction of flight 24a, is located immediately behind the eighth aircraft seat 800a. In principle, the eighth aircraft seat 800a in aircraft cabin section 26a, in the second inner seat column 40a, viewed in the direction of flight 24a, can be located immediately behind the fifth aircraft seat 500a.

[0084] In the aircraft cabin section 26a, in the second inner seat column 40a, four differently configured aircraft seat assemblies are located, namely the fifth aircraft seat assembly 500a, the sixth aircraft seat assembly 600a, the seventh aircraft seat assembly 700a and the eighth aircraft seat assembly 800a, of the several aircraft seat assemblies 100a, 100'a, 200a, 200'a, 300a, 300'a, 400a, 400'a, 500a, 500'a, 600a, 600'a, 700a, 700'a, 800a, 800'a are arranged directly one behind the other, with seating directions 510a, 710a of two aircraft seat assemblies of the four aircraft seat assemblies 500a, 600a, 700a, 800a, namely the fifth aircraft seat assembly 500a and the seventh aircraft seat assembly 700a, are arranged at least substantially parallel to the aircraft cabin center axis 16a,wherein the fifth aircraft seat 520a of the fifth aircraft seat assembly 500a is arranged aisle-side and the seventh aircraft seat 720a of the seventh aircraft seat assembly 700a is arranged away from the aisle, and seating directions 610a, 810a of two further aircraft seat assemblies of the four aircraft seat assemblies 500a, 600a, 700a, 800a, namely the sixth aircraft seat assembly 600a and the eighth aircraft seat assembly 800a, are arranged at an angle to the aircraft cabin center axis 16a, wherein the sixth aircraft seat 620a of the sixth aircraft seat assembly 600a is arranged aisle-side and the eighth aircraft seat 820a of the eighth aircraft seat assembly 800a is arranged away from the aisle.

[0085] In the aircraft cabin section 26a, in the first outer seat column 36a, four differently designed aircraft seat assemblies 500'a, 600'a, 700'a, 800'a of the several further aircraft seat assemblies 100'a, 200'a, 300'a, 400'a, 500'a, 600'a, 700'a, 800'a are arranged directly one behind the other. The four differently designed aircraft seating units 500'a, 600'a, 700'a, 800'a, arranged in the first outer seat column 36a, and the several further aircraft seating units 100'a, 200'a, 300'a, 400'a, 500'a, 600'a, 700'a, 800'a, are arranged in the direction of flight 24a immediately following one another.

[0086] In the aircraft cabin section 26a, in the second outer seat column 42a, four differently designed aircraft seat units 100'a, 200'a, 300'a, 400'a of the several further aircraft seat units 100'a, 200'a, 300'a, 400'a, 500'a, 600'a, 700'a, 800'a are arranged directly one behind the other. The four aircraft seating units 100'a, 200'a, 300'a, 400'a, which are designed differently from one another and are arranged in the second outer seat column 42a, are arranged in the direction of flight 24a in a directly successive manner.

[0087] In principle, the preceding descriptions of the first inner seat column 38a also apply to the second outer seat column 42a. In principle, the preceding descriptions of the second inner seat column 40a also apply to the first outer seat column 36a.

[0088] In the aircraft cabin section 26a, two aircraft seat assemblies of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a, namely the third aircraft seat assembly 300a and the seventh aircraft seat assembly 700a, form a seat pair 46a in two immediately adjacent seat gaps, namely the first inner seat gap 38a and the second inner seat gap 40a, wherein the seating directions 310a, 710a of the two aircraft seat assemblies 300a, 700a are arranged at least substantially parallel to the aircraft cabin center axis 16a and the aircraft seats 320a, 720a of the two aircraft seat assemblies 300a, 700a are arranged facing away from the aisle, wherein in the two immediately adjacent seat gaps 38a, 40a at least two of the seat pairs 46a are arranged ( Fig. 4This allows for the advantageous creation of areas for passengers traveling in pairs within aircraft cabin section 26a. The two aircraft seat assemblies arranged directly adjacent to each other, namely the third aircraft seat assemblies 300a and the seventh aircraft seat assemblies 700a, are mirrored relative to each other about the aircraft cabin center axis 16a. The two aircraft seat assemblies 300a, 700a of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a, which form the seat pair 46a, are arranged flush with each other in the direction of flight 24a when viewed in a plane parallel to the aircraft cabin floor 22a. The two aircraft seat assemblies 300a, 700a of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a, which form the seat pair 46a, are arranged in the central area 44a of the aircraft cabin 12a.In principle, it is conceivable that the third aircraft seat assembly 300a and the seventh aircraft seat assembly 700a, which form the seat pair 46a, have a common mattress, especially in the reclining position of the third aircraft seat 320a and the seventh aircraft seat 720a.

[0089] In the first inner seat column 38a, the second aircraft seat 220a has a second axis 48a that is aligned parallel to the aircraft cabin floor 22a, that intersects a seat base of the second aircraft seat 220a of the second aircraft seat assembly 200a and that is aligned parallel to the seating direction 210a of the second aircraft seat assembly 200a, wherein the second axis 48a intersects a seat base of a further eighth aircraft seat of one of the further eighth aircraft seat assemblies 800'a in the second inner seat column 40a, wherein the further eighth aircraft seat has a further eighth axis 50a that is aligned parallel to a seating direction of this further eighth aircraft seat assembly 800'a and parallel to the second axis 48a ( Fig. 4 ).

[0090] The aircraft seating arrangement 14a comprises a first seating grouping 52a of four aircraft seating devices arranged directly one behind the other in the first inner seat column 38a in the aircraft cabin section 26a, namely the first aircraft seating device 100a, the second aircraft seating device 200a, the third aircraft seating device 300a and the fourth aircraft seating device 400a, each having different seating directions 110a, 210a, 310a, 410a and whose aircraft seats 120a, 220a, 320a, 420a are arranged facing the aisle or away from the aisle ( Fig. 3 and 4The seating directions 110a, 210a, 310a, 410a of the aircraft seating units 100a, 200a, 300a, 400a, arranged directly one behind the other, are arranged alternately within the first seating group 52a, at least substantially parallel and at an angle to the aircraft cabin center axis 16a. The first seating group 52a forms a periodically repeatable sequence. Several identical first seating groups 52a can be arranged directly one behind the other along an aircraft longitudinal axis.

[0091] Viewed in the direction of flight 24a, an aircraft seat is arranged both in front of and behind the first aircraft seat 100a, the seating direction of which 110a is arranged at least substantially parallel to the aircraft cabin center axis 16a, and the seating direction of which is angled to the aircraft cabin center axis 16a. Viewed in the direction of flight 24a, an aircraft seat is arranged both in front of and behind the second aircraft seat 200a, the seating direction of which 210a is arranged at an angle to the aircraft cabin center axis 16a, and the seating direction of which is at least substantially parallel to the aircraft cabin center axis 16a.Viewed in the direction of flight 24a, an aircraft seat is arranged both in front of and behind the third aircraft seat 300a, the seating direction of which 310a is arranged at least substantially parallel to the aircraft cabin center axis 16a, and the seating direction of which is angled to the aircraft cabin center axis 16a. Viewed in the direction of flight 24a, an aircraft seat is arranged behind the fourth aircraft seat 400a, the seating direction of which 410a is angled to the aircraft cabin center axis 16a, and the seating direction of which is at least substantially parallel to the aircraft cabin center axis 16a.In principle, viewed in the direction of flight 24a, an aircraft seat can be arranged in front of and behind the fourth aircraft seat 400a, the seating direction of which 410a is angled to the aircraft cabin center axis 16a, each of which has a seating direction that is at least substantially parallel to the aircraft cabin center axis 16a.

[0092] The aircraft seating arrangement 14a has a second seating grouping 54a of four aircraft seating devices arranged directly one behind the other in the second inner seat column 40a in the aircraft cabin section 26a, namely the fifth aircraft seating device 500a, the sixth aircraft seating device 600a, the seventh aircraft seating device 700a and the eighth aircraft seating device 800a, each having different seating directions 510a, 610a, 710a, 810a and whose aircraft seats 520a, 620a, 720a, 820a are arranged facing the aisle or away from the aisle ( Fig. 4The seating directions 510a, 610a, 710a, 810a of the aircraft seating units 500a, 600a, 700a, 800a, arranged directly one behind the other, are arranged alternately within the second seating group 54a, at least substantially parallel and at an angle to the aircraft cabin center axis 16a. The second seating group 54a forms a periodically repeatable sequence. Several identical second seating groups 54a can be arranged directly one behind the other along the aircraft cabin center axis 16a.

[0093] Viewed in the direction of flight 24a, an aircraft seat is arranged both in front of and behind the fifth aircraft seat 500a, whose seating direction 510a is arranged at least substantially parallel to the aircraft cabin center axis 16a, and whose seating direction is angled to the aircraft cabin center axis 16a. Viewed in the direction of flight 24a, an aircraft seat is arranged both in front of and behind the sixth aircraft seat 600a, whose seating direction 610a is arranged at an angle to the aircraft cabin center axis 16a, and whose seating direction is at least substantially parallel to the aircraft cabin center axis 16a.Viewed in the direction of flight 24a, an aircraft seat is arranged both in front of and behind the seventh aircraft seat 700a, whose seating direction 710a is arranged at least substantially parallel to the aircraft cabin center axis 16a, and whose seating direction is angled to the aircraft cabin center axis 16a. Viewed in the direction of flight 24a, an aircraft seat is arranged behind the eighth aircraft seat 800a, whose seating direction 810a is angled to the aircraft cabin center axis 16a, and whose seating direction is at least substantially parallel to the aircraft cabin center axis 16a.In principle, viewed in the direction of flight 24a, an aircraft seat can be arranged in front of and behind the eighth aircraft seat 800a, whose seating direction 810a is angled to the aircraft cabin center axis 16a, each of which has a seating direction that is at least substantially parallel to the aircraft cabin center axis 16a.

[0094] The first aircraft seat 100a, the second aircraft seat 200a, the third aircraft seat 300a and the fourth aircraft seat 400a in the aircraft cabin section 26a differ in at least one comfort category, wherein the aircraft seat assemblies 100a, 200a, 300a, 400a each have a different value for the at least one comfort category, which is due to a different arrangement of the aircraft seats 120a, 220a, 320a, 420a and to the at least partially different design of the aircraft seat assemblies 100a, 200a, 300a, 400a.The fifth aircraft seat 500a, the sixth aircraft seat 600a, the seventh aircraft seat 700a and the eighth aircraft seat 800a in the aircraft cabin section 26a differ in at least one comfort category, wherein the aircraft seat assemblies 500a, 600a, 700a, 800a each have a different value for the at least one comfort category, which is due to a different arrangement of the aircraft seats 520a, 620a, 720a, 820a and to the at least partially different design of the aircraft seat assemblies 500a, 600a, 700a, 800a.

[0095] In principle, at least two aircraft seating configurations (100a), 200a, 300a, 400a, 500a, 600a, 700a, and 800a) in cabin section 26a must differ in at least one comfort category. However, not all aircraft seating configurations need to differ. Specifically, aircraft seating configurations 100a, 200a, 300a, 400a, 500a, 600a, 700a, and 800a do not need to differ in all aspects, particularly across multiple comfort categories.

[0096] At least one comfort category describes a living space.

[0097] In this case, a first comfort category is defined as the maximum bed length of an aircraft seat in the reclining position. The greater the value for the maximum bed length, the greater the comfort for a passenger. The value for the maximum bed length is expressed as a single length. The second aircraft seat configuration 200a has a value for the maximum bed length of the second aircraft seat 220a that is greater than the value for the first aircraft seat configuration 100a for the maximum bed length of the first aircraft seat 120a. In this case, the value for the maximum bed length of the second aircraft seat configuration 200a is 5% greater than the value for the maximum bed length of the first aircraft seat configuration 100a. The first aircraft seat configuration 100a and the second aircraft seat configuration 200a differ in their maximum bed lengths.The fourth aircraft seat 400a has a maximum bed length value for the fourth aircraft seat 420a that is greater than the value for the third aircraft seat 300a for the maximum bed length of the third aircraft seat 320a. In this case, the maximum bed length value for the fourth aircraft seat 400a is 5% greater than the maximum bed length value for the third aircraft seat 300a. The third aircraft seat 300a and the fourth aircraft seat 400a differ in their maximum bed lengths.

[0098] In the present case, a second comfort category is defined as a minimum passage width in at least one area of ​​an aircraft seating area. The passage width is defined as the minimum width of direct access in an area between the first aircraft cabin aisle 32a or the second aircraft cabin aisle 34a and an area located, viewed in the direction of travel of the corresponding aircraft seating configuration, immediately behind the seat base of an aircraft seat of that configuration. The greater the value for the minimum passage width, the greater the comfort for a passenger. The value for the minimum passage width in at least one area of ​​an aircraft seating configuration is defined as a length.The first aircraft seating unit 100a has a minimum passage width in at least one area of ​​an aircraft seating area of ​​the first aircraft seating unit 100a that is greater than a minimum passage width in at least one area of ​​an aircraft seating area of ​​the second aircraft seating unit 200a. The third aircraft seating unit 300a has a minimum passage width in at least one area of ​​an aircraft seating area of ​​the third aircraft seating unit 300a that is greater than the minimum passage width in at least one area of ​​the aircraft seating area of ​​the first aircraft seating unit 100a.The fourth aircraft seating device 400a has a minimum passage width value in at least one area of ​​an aircraft seating area of ​​the fourth aircraft seating device 400a that is greater than the value for the minimum passage width in at least one area of ​​the aircraft seating area of ​​the third aircraft seating device 300a.

[0099] In principle, at least one further comfort category can be designed as a floor area of ​​an aircraft seating device, as a storage surface of an aircraft seating device, in particular a console, as a table surface of an aircraft seating device, as an armroom for a passenger, in particular a minimum or maximum, in particular a limiting maximum angle of movement starting from the seat direction in the seated position, as a support surface of an aircraft seat for a passenger, in particular in the seated position or in the reclining position, as a bed width of the aircraft seat in the reclining position and / or as a footwell volume.

[0100] In principle, at least one comfort category can also describe quality, noise, and / or lighting. Quality can specifically describe seat upholstery, such as a foam or spring core, or contact material, such as fabric or leather. Noise can specifically describe the aircraft seat's sound insulation from ambient cabin noise. Lighting can specifically describe the number of light sources and a characteristic of those light sources.

[0101] In the first inner seat column 38a, one of the further second aircraft seat arrangements 200'a is arranged in a first row of seats of the aircraft cabin section 26a, viewed against the direction of flight 24a ( Fig. 4Viewed in the direction of flight 24a, one of several aircraft cabin modules 30a is arranged in the central area 44a immediately behind the second aircraft seat 200'a located in the first row of aircraft cabin section 26a. This allows for greater comfort in the first row compared to the second aircraft seat 200a, as more space is available in the first row. The second aircraft seat 200'a located in the first row of aircraft cabin section 26a can, in principle, differ in at least one comfort category from at least one of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a. In the present case, the aircraft cabin module 30a located in the central area 44a can be configured as a front-row monument.In principle, the aircraft cabin module 30a can also be part of the further second aircraft seating arrangement 200'a.

[0102] In the second inner seat column 40a, one of the further sixth aircraft seat arrangements 600'a is arranged in the first seat row of the aircraft cabin section 26a, viewed against the direction of flight 24a ( Fig. 4Viewed in the direction of flight 24a, the aforementioned aircraft cabin module 30a is located in the central area 44a immediately behind the sixth aircraft seat 600'a, which is arranged in the first row of aircraft cabin section 26a. The sixth aircraft seat 600'a, located in the first row of aircraft cabin section 26a, can, in principle, differ in at least one comfort category from at least one of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a. The aircraft cabin module 30a can also, in principle, be part of the sixth aircraft seat 600'a.

[0103] In the first outer seat column 36a, one of the further fifth aircraft seat arrangements 500'a is arranged in the first seat row of the aircraft cabin section 26a, viewed against the direction of flight 24a ( Fig. 4Viewed in the direction of flight 24a, immediately behind the fifth aircraft seat 500'a located in the first row of aircraft cabin section 26a, in the first outer seat column 36a, another aircraft cabin module 30a is arranged. The fifth aircraft seat 500'a located in the first row of aircraft cabin section 26a, in the first seat column 36a, can, in principle, differ in at least one comfort category from at least one of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a. In principle, the additional aircraft cabin module 30a can also be part of the sixth aircraft seat 600'a.

[0104] In the second outer seat column 42a, one of the further first aircraft seat arrangements 100'a is arranged in the first seat row of the aircraft cabin section 26a, viewed against the direction of flight 24a ( Fig. 4Viewed in the direction of flight 24a, immediately behind the second outer seat column 42a of the first row of aircraft cabin section 26a, another aircraft cabin module 30a is arranged. The second outer seat column 42a of the first row of aircraft cabin section 26a, the second outer seat column 42a of the first row of aircraft cabin section 26a, can, in principle, differ in at least one comfort category from at least one of the several aircraft seat assemblies 100a, 200a, 300a, 400a, 500a, 600a, 700a, 800a. The other aircraft cabin module 30a can also, in principle, be part of the second first aircraft seat assembly 100'a.

[0105] Basically, the in the Figures 2 and 3The aircraft seating arrangement 14a shown is not limited to the number of aircraft seating units shown. The aircraft seating arrangement 14a can have fewer or more than the aircraft seating units 100a, 100'a, 200a, 200'a, 300a, 300'a, 400a, 400'a, 500a, 500'a, 600a, 600'a, 700a, 700'a, 800a, 800'a shown. In principle, it would also be conceivable that the number of aircraft seating units shown in the Figures 2 to 4 The aircraft seating arrangement 14a shown, in whole or in part, in particular at least one of the seat columns 36a, 38a, 40a, 42a, is arranged in the aircraft cabin 12a mirrored about an axis, wherein the axis is perpendicular to the aircraft cabin center axis 16a and parallel to the aircraft cabin floor 22a.

[0106] In the Figures 5 to 10Six further embodiments of the invention are shown. The following descriptions and drawings are essentially limited to the differences between the embodiments, whereby, with regard to identically designated components, in particular components with the same reference numerals, reference is also generally made to the drawings and / or the description of the other embodiments, in particular the Figures 1 to 4 , can be referenced. To distinguish the embodiments, the letter a is the reference numeral of the embodiment in Figures 1 to 4 recreated. In the exemplary embodiments of the Figures 5 to 10 The letter a is replaced by the letters b to g.

[0107] The Figure 5Figure 1 shows an aircraft seating arrangement 14b in a second embodiment. The aircraft seating arrangement 14b is intended for use in a partially illustrated aircraft cabin 12b. The aircraft cabin 12b has a cabin centerline 16b. The cabin centerline 16b is configured as a longitudinal axis of the aircraft. The aircraft cabin 12b has two opposing outer walls 18b, 20b. The cabin centerline 16b is aligned parallel to a cabin floor 22b of the aircraft cabin 12b. The aircraft has a flight direction 24b in at least one operating state. In this case, the flight direction 24b is ideally aligned parallel to the cabin centerline 16b. The aircraft cabin 12b has a cabin section 26b along the cabin centerline 16b.In this case, the aircraft cabin section 26b is bounded by several schematically represented aircraft cabin modules 30b along the aircraft cabin centerline 16b. The aircraft cabin 12b has a first cabin aisle 32b and a second cabin aisle 34b within the aircraft cabin section 26b. The aircraft seating arrangement 14b comprises a first outer seat column 36b. The aircraft seating arrangement 14b comprises a first inner seat column 38b. The aircraft seating arrangement 14b comprises a second inner seat column 40b. The aircraft seating arrangement 14b comprises a second outer seat column 42b. In this case, the first inner seat column 38b is symmetrical to the second inner seat column 40b about the aircraft cabin centerline 16b. In this case, the first outer seat column 36b is symmetrical to the second outer seat column 42b about the aircraft cabin centerline 16b.The first inner seat column 38b and the second inner seat column 40b are arranged directly next to each other. The aircraft cabin 12b has a central section 44b.

[0108] The aircraft seating arrangement 14b comprises several aircraft seating assemblies 100b, 200b, 300b, 500b, 600b, and 700b arranged in the aircraft cabin section 26b. The several aircraft seating assemblies 100b, 200b, 300b, 500b, 600b, and 700b are configured differently from one another. Each aircraft seating assembly 100b, 200b, 300b, 500b, 600b, and 700b has one aircraft seat. Each aircraft seating assembly 100b, 200b, 300b, 500b, 600b, and 700b has one console. The aircraft seating arrangement 14b comprises a first aircraft seating device 100b of several aircraft seating devices 100b, 200b, 300b, 500b, 600b, 700b. The first aircraft seating device 100b has a seating direction 110b. The seating direction 110b of the first aircraft seating device 100b corresponds to the flight direction 24b. The first aircraft seating device 100b has a first aircraft seat 120b. The first aircraft seating device 100b has a first console 130b.The first aircraft seating arrangement 100b has direct access to the first aircraft cabin aisle 32b. The aircraft seating arrangement 14b includes a second aircraft seating arrangement 200b, which may include several aircraft seating arrangements 100b, 200b, 300b, 500b, 600b, and 700b. The second aircraft seating arrangement 200b has a seating direction 210b. The seating direction 210b of the second aircraft seating arrangement 200b differs from the flight direction 24b. The second aircraft seating arrangement 200b includes a second aircraft seat 220b. The second aircraft seating arrangement 200b includes a second console 230b. The second aircraft seating arrangement 200b has direct access to the first aircraft cabin aisle 32b. The aircraft seating arrangement 14b comprises a third aircraft seating device 300b of the several aircraft seating devices 100b, 200b, 300b, 500b, 600b, 700b. The third aircraft seating device 300b has a seating direction 310b.The seating direction 310b of the third aircraft seating arrangement 300b corresponds to the flight direction 24b. The third aircraft seating arrangement 300b has a third aircraft seat 320b. The third aircraft seating arrangement 300b has a third console 330b. The third aircraft seating arrangement 300b has direct access to the first aircraft cabin aisle 32b. The first aircraft seating arrangement 100b, the second aircraft seating arrangement 200b, and the third aircraft seating arrangement 300b are configured differently from one another. The aircraft seating arrangement 14b includes a fifth aircraft seating arrangement 500b of the multiple aircraft seating arrangements 100b, 200b, 300b, 500b, 600b, 700b. The fifth aircraft seating arrangement 500b is configured as a mirror image of the first aircraft seating arrangement 100b about an aircraft longitudinal axis, in particular about the aircraft cabin center axis 16b. The fifth aircraft seat 500b has a seating direction 510b.The seating direction 510b of the fifth aircraft seating arrangement 500b corresponds to the flight direction 24b. The fifth aircraft seating arrangement 500b has a fifth aircraft seat 520b. The fifth aircraft seating arrangement 500b has a fifth console 530b. The fifth aircraft seating arrangement 500b has direct access to the second aircraft cabin aisle 34b. The aircraft seating arrangement 14b comprises a sixth aircraft seating arrangement 600b of the several aircraft seating arrangements 100b, 200b, 300b, 400b, 500b, 600b, 700b, 800b. The sixth aircraft seating arrangement 600b is designed as a mirror image of the second aircraft seating arrangement 200b about an aircraft longitudinal axis, in particular about the aircraft cabin center axis 16b. The sixth aircraft seating arrangement 600b has a seating direction 610b. The seating direction 610b of the sixth aircraft seating unit 600b differs from the flight direction 24b. The sixth aircraft seating unit 600b has a sixth aircraft seat 620b.The sixth aircraft seat assembly 600b has a sixth console 630b. The sixth aircraft seat assembly 600b has direct access to the second aircraft cabin aisle 34b. The aircraft seat assembly 14b includes a seventh aircraft seat assembly 700b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b. The seventh aircraft seat assembly 700b is mirrored about an aircraft longitudinal axis, in particular about the aircraft cabin center axis 16b, to the third aircraft seat assembly 300b. The seventh aircraft seat assembly 700b has a seating direction 710b. The seating direction 710b of the seventh aircraft seat assembly 700b corresponds to the flight direction 24b. The seventh aircraft seat assembly 700b has a seventh aircraft seat 720b. The seventh aircraft seat assembly 700b has a seventh console 730b. The seventh aircraft seat assembly 700b has direct access to the second aircraft cabin aisle 34b.The fifth aircraft seat 500b, the sixth aircraft seat 600b, and the seventh aircraft seat 700b are configured differently from one another. Aircraft seats 120b, 220b, 320b, 520b, 620b, and 720b are each configured as a full-flat seat. Aircraft seats 120b, 220b, 320b, 520b, 620b, and 720b are each adjustable between a sitting position and a reclining position. In the present case, aircraft seat arrangement 14b comprises six differently configured aircraft seat assemblies: 100b, 200b, 300b, 500b, 600b, and 700b, each of which is present at least once in aircraft seat arrangement 14b. The first aircraft seat device 100b, the second aircraft seat device 200b, the third aircraft seat device 300b, the fifth aircraft seat device 500b, the sixth aircraft seat device 600b and the seventh aircraft seat device 700b are designed differently from each other.In the aircraft cabin section 26b, six differently configured aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, and 700b are arranged in the present case. Each aircraft seat assembly 100b, 200b, 300b, 500b, 600b, and 700b forms an aircraft seating area. The aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, and 700b have differently shaped and / or differently arranged components in the respective aircraft seating areas. In particular, the arrangement and orientation of the aircraft seats 120b, 220b, and 320b in the respective aircraft seating areas differ between the first aircraft seat assembly 100b, the second aircraft seat assembly 200b, and the third aircraft seat assembly 300b.Furthermore, the arrangement and orientation of aircraft seats 520b, 620b, and 720b differ in particular in the respective aircraft seating areas for the fifth aircraft seat unit 500b, the sixth aircraft seat unit 600b, and the seventh aircraft seat unit 700b. The first aircraft seat unit 100b and the fifth aircraft seat unit 500b are arranged directly next to each other. The second aircraft seat unit 200b and the sixth aircraft seat unit 600b are arranged directly next to each other. The third aircraft seat unit 300b and the seventh aircraft seat unit 700b are arranged directly next to each other.

[0109] In the present case, the aircraft seating arrangement 14b comprises several further first aircraft seating assemblies 100'b, which are designed at least substantially identically to the first aircraft seating assembly 100b. The further first aircraft seating assemblies 100'b are each arranged in the first inner seat column 38b or in the second outer seat column 42b. In the present case, the aircraft seating arrangement 14b comprises several further second aircraft seating assemblies 200'b, which are designed at least substantially identically to the second aircraft seating assembly 200b. The further second aircraft seating assemblies 200'b are each arranged in the first inner seat column 38b or in the second outer seat column 42b. In the present case, the aircraft seating arrangement 14b comprises several further third aircraft seating assemblies 300'b, which are designed at least substantially identically to the third aircraft seating assembly 300b.The further third aircraft seat assemblies 300'b are each arranged in the first inner seat column 38b or in the second outer seat column 42b. In the present case, the aircraft seat assembly 14b comprises several further fifth aircraft seat assemblies 500'b, which are designed at least substantially identically to the fifth aircraft seat assembly 500b. The further fifth aircraft seat assemblies 500'b are each arranged in the second inner seat column 40b or in the first outer seat column 36b. In the present case, the aircraft seat assembly 14b comprises several further sixth aircraft seat assemblies 600'b, which are designed at least substantially identically to the sixth aircraft seat assembly 600b. The further sixth aircraft seat assemblies 600'b are each arranged in the second inner seat column 40b or in the first outer seat column 36b.In the present case, the aircraft seating arrangement 14b comprises several further seventh aircraft seating assemblies 700'b, which are designed at least substantially identically to the seventh aircraft seating assembly 700b. The further seventh aircraft seating assemblies 700'b are each arranged in the second inner seat column 40b or in the first outer seat column 36b. For the sake of clarity, the following is shown in the figure below. Figure 5 only a selection of further aircraft seating devices 100'a, 200'a, 300'a, 500'a, 600'a, 700'a are provided with a reference mark.

[0110] In aircraft cabin section 26b, the seating direction 110b of the first aircraft seat 100b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b in the first inner seat column 38b is aligned at least substantially parallel to the aircraft cabin center axis 16b. The first aircraft seat 120b of the first aircraft seat assemblies 100b of the aircraft seat assemblies 100b, 200b, 300b arranged in the first inner seat column 38b of aircraft cabin section 26b is located on the aisle side. In the aircraft cabin section 26b, the seating direction 210b of the second aircraft seating arrangement 200b of the several aircraft seating arrangements 100b, 200b, 300b is arranged in the first inner seat column 38b at an angle of at least 18 degrees to the aircraft cabin center axis 16b.In the present case, in aircraft cabin section 26b, in the first inner seat column 38b, the seating direction 210b of the second aircraft seat 200b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b is arranged at an angle of 30 degrees to the aircraft cabin center axis 16b. In aircraft cabin section 26b, in the first inner seat column 38b, the seating direction 210b of the second aircraft seat 200b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b is directed away from the immediately adjacent first aircraft cabin aisle 32b. The second aircraft seat 220b of the second aircraft seat assembly 200b of the aircraft seat assemblies 100b, 200b, 300b arranged in the first inner seat column 38b in the aircraft cabin section 26b is arranged on the aisle side.In aircraft cabin section 26b, the seating direction 310b of the third aircraft seat 300b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b in the first inner seat column 38b is aligned at least substantially parallel to the aircraft cabin center axis 16b. The third aircraft seat 320b of the third aircraft seat assemblies 300b of the aircraft seat assemblies 100b, 200b, 300b arranged in the first inner seat column 38b is located away from the aisle. The first aircraft seat 100b and the third aircraft seat assemblies 300b are separated from each other by the second aircraft seat assemblies 200b.In the aircraft cabin section 26b, in the first inner seat column 38b, the first aircraft seat assembly 100b and the second aircraft seat assembly 200b each have one aircraft seat 120b, 220b, which is arranged on the aisle side, and the third aircraft seat assembly 300b, which is arranged immediately behind or in front of the two aircraft seat assemblies 100b, 200b when viewed in the direction of flight 24b, has the aircraft seat 320b, which is arranged away from the aisle. The aircraft seats 120b, 320b of the aircraft seat assemblies 100b, 300b, whose seating directions 110b, 310b are arranged at least substantially parallel to the aircraft cabin center axis 16b, have different distances to the first aircraft cabin aisle 32b.In the aircraft cabin section 26b, three aircraft seat assemblies of the several aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b are arranged in the first inner seat column 38b, namely the first aircraft seat assembly 100b, the second aircraft seat assembly 200b and the third aircraft seat assembly 300b, wherein the seating directions 110b, 310b of the first aircraft seat assembly 100b and the third aircraft seat assembly 300b are arranged at least substantially parallel to the aircraft cabin center axis 16b and the seating direction 210b of the second aircraft seat assembly 200b is arranged at an angle to the aircraft cabin center axis 16b.In the aircraft cabin section 26b, in the first inner seat column 38b, the three aircraft seat devices of the several aircraft seat devices 100b, 200b, 300b, 500b, 600b, 700b, namely the first aircraft seat device 100b, the second aircraft seat device 200b and the third aircraft seat device 300b, are arranged directly one behind the other, wherein the seating directions 110b, 310b of the first aircraft seat device 100b and the third aircraft seat device 300b are arranged at least substantially parallel to the aircraft cabin center axis 16b and the seating direction 210b of the second aircraft seat device 200b is arranged at an angle to the aircraft cabin center axis 16b.In the aircraft cabin section 26b, three aircraft seat assemblies of the several aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b are arranged in the first inner seat column 38b, namely at least one of the further third aircraft seat assemblies 300'b, the first aircraft seat assembly 100b and the second aircraft seat assembly 200b, wherein the seating directions of the first aircraft seat assembly 100b and the further third aircraft seat assembly 300'b are arranged at least substantially parallel to the aircraft cabin center axis 16b and the seating direction 210b of the second aircraft seat assembly 200b is arranged at an angle to the aircraft cabin center axis 16b.In the aircraft cabin section 26b, in the first inner seat column 38b, the three aircraft seat devices of the several aircraft seat devices 100b, 200b, 300b, 500b, 600b, 700b, namely at least one of the further third aircraft seat devices 300'b, the first aircraft seat device 100b and the second aircraft seat device 200b, are arranged directly one behind the other, wherein the seating directions of the first aircraft seat device 100b and the further third aircraft seat device 300'b are arranged at least substantially parallel to the aircraft cabin center axis 16b and the seating direction 210b of the second aircraft seat device 200b is arranged at an angle to the aircraft cabin center axis 16b.In aircraft cabin section 26b, three differently configured aircraft seat assemblies 100b, 200b, 300b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b are arranged in the first inner seat column 38b, directly one behind the other. The three differently configured aircraft seat assemblies 100b, 200b, 300b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b of the first inner seat column 38b are arranged directly following one another in the direction of flight 24b. In the aircraft cabin section 26b, in the first inner seat column 38b, the first aircraft seat assembly 100b, the second aircraft seat assembly 200b and the third aircraft seat assembly 300b are arranged directly one behind the other.In aircraft cabin section 26b, in the first inner seat column 38b, the first aircraft seat 100b, viewed in the direction of flight 24b, is located immediately behind the second aircraft seat 200b. In aircraft cabin section 26b, in the first inner seat column 38b, the second aircraft seat 200b, viewed in the direction of flight 24b, is located immediately behind the third aircraft seat 300b. In principle, the third aircraft seat 300b can be located in aircraft cabin section 26b, in the first inner seat column 38b, viewed in the direction of flight 24b, immediately behind the first aircraft seat 100b.

[0111] In aircraft cabin section 26b, the seating direction 510b of the fifth aircraft seat 500b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b in the second inner seat column 40b is aligned at least substantially parallel to the aircraft cabin center axis 16b. The fifth aircraft seat 520b of the fifth aircraft seat assemblies 500b, 600b, 700b arranged in the second inner seat column 40b of aircraft cabin section 26b is located on the aisle side. In the aircraft cabin section 26b, in the second inner seat column 40b, the seating direction 610b of the sixth aircraft seat arrangement 600b of the several aircraft seat arrangements 100b, 200b, 300b, 500b, 600b, 700b is arranged at an angle of at least 18 degrees to the aircraft cabin center axis 16b.In the present case, in aircraft cabin section 26b, in the second inner seat column 40b, the seating direction 610b of the sixth aircraft seat 600b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b is arranged at an angle of 30 degrees to the aircraft cabin center axis 16b. In aircraft cabin section 26b, in the second inner seat column 40b, the seating direction 610b of the sixth aircraft seat 600b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b is directed away from the immediately adjacent second aircraft cabin aisle 34b. The sixth aircraft seat 620b of the sixth aircraft seat assembly 600b of the aircraft seat assemblies 500b, 600b, 700b arranged in the second inner seat column 40b in the aircraft cabin section 26b is arranged on the aisle side.In aircraft cabin section 26b, the seating direction 710b of the seventh aircraft seat 700b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b in the second inner seat column 40b is aligned at least substantially parallel to the aircraft cabin center axis 16b. The seventh aircraft seat 720b of the seventh aircraft seat assemblies 700b of the aircraft seat assemblies 500b, 600b, 700b arranged in the second inner seat column 40b is located away from the aisle. The fifth aircraft seat 500b and the seventh aircraft seat 700b are spaced apart from each other by the sixth aircraft seat 600b.In aircraft cabin section 26b, in the second inner seat column 40b, the fifth aircraft seat 500b and the sixth aircraft seat 600b each have one aircraft seat 520b, 620b, which is arranged on the aisle side, and the seventh aircraft seat 700b, which, viewed in the direction of flight 24b, is arranged immediately behind or in front of the two aircraft seat assemblies 500b, 600b, has the aircraft seat 720b, which is arranged away from the aisle. The aircraft seats 520b, 720b of the aircraft seat assemblies 500b, 700b, whose seating directions 510b, 710b are arranged at least substantially parallel to the aircraft cabin center axis 16b, have different distances to the second aircraft cabin aisle 34b.In the aircraft cabin section 26b, three aircraft seat assemblies of the several aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b are arranged in the second inner seat column 40b, namely the fifth aircraft seat assembly 500b, the sixth aircraft seat assembly 600b and the seventh aircraft seat assembly 700b, wherein the seating directions 510b, 710b of the fifth aircraft seat assembly 500b and the seventh aircraft seat assembly 700b are arranged at least substantially parallel to the aircraft cabin center axis 16b and the seating direction 610b of the sixth aircraft seat assembly 600b is arranged at an angle to the aircraft cabin center axis 16b.In the aircraft cabin section 26b, in the second inner seat column 40b, the three aircraft seat assemblies of the several aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b, namely the fifth aircraft seat assembly 500b, the sixth aircraft seat assembly 600b and the seventh aircraft seat assembly 700b, are arranged directly one behind the other, wherein the seating directions 510b, 710b of the fifth aircraft seat assembly 500b and the seventh aircraft seat assembly 700b are arranged at least substantially parallel to the aircraft cabin center axis 16b and the seating direction 610b of the sixth aircraft seat assembly 600b is arranged at an angle to the aircraft cabin center axis 16b.In the aircraft cabin section 26b, three aircraft seat assemblies of the several aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b are arranged in the second inner seat column 40b, namely one of the further seventh aircraft seat assemblies 700'b, the fifth aircraft seat assembly 500b and the sixth aircraft seat assembly 600b, wherein the seating directions of the fifth aircraft seat assembly 500b are arranged at least substantially parallel to the aircraft cabin center axis 16b and the seating direction 610b of the sixth aircraft seat assembly 600b is arranged at an angle to the aircraft cabin center axis 16b.In the aircraft cabin section 26b, in the second inner seat column 40b, the three aircraft seat assemblies of the several aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b, namely one of the further seventh aircraft seat assemblies 700'b, the fifth aircraft seat assembly 500b and the sixth aircraft seat assembly 600b, are arranged directly one behind the other, wherein the seating directions of the fifth aircraft seat assembly 500b and the further seventh aircraft seat assembly 700'b are arranged at least substantially parallel to the aircraft cabin center axis 16b and the seating direction of the sixth aircraft seat assembly 600b is arranged at an angle to the aircraft cabin center axis 16b.In aircraft cabin section 26b, three differently configured aircraft seat assemblies 500b, 600b, 700b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b are arranged in the second inner seat column 40b, directly one behind the other. The three differently configured aircraft seat assemblies 500b, 600b, 700b of the multiple aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b, arranged in the second inner seat column 40b, are arranged directly following one another in the direction of flight 24b. In the aircraft cabin section 26b, in the second inner seat column 40b, the fifth aircraft seat 500b, the sixth aircraft seat 600b and the seventh aircraft seat 700b are arranged directly one behind the other.In aircraft cabin section 26b, in the second inner seat column 40b, the fifth aircraft seat 500b, viewed in the direction of flight 24b, is located immediately behind the sixth aircraft seat 600b. In aircraft cabin section 26b, in the second inner seat column 40b, the sixth aircraft seat 600b, viewed in the direction of flight 24b, is located immediately behind the seventh aircraft seat 700b. In principle, the seventh aircraft seat 700b can be located in aircraft cabin section 26b, in the second inner seat column 40b, viewed in the direction of flight 24b, immediately behind the fifth aircraft seat 500b.

[0112] In aircraft cabin section 26b, three differently designed aircraft seat assemblies 500'b, 600'b, 700'b are arranged directly one behind the other in the first outer seat column 36b, along with several other aircraft seat assemblies 100'b, 200'b, 300'b, 500'b, 600'b, 700'b. The three differently designed aircraft seat assemblies 500'b, 600'b, 700'b, arranged in the first outer seat column 36b, along with several other aircraft seat assemblies 100'b, 200'b, 300'b, 500'b, 600'b, 700'b, are arranged directly one after the other in the direction of flight 24b.In the present case, in the second outer seat column 42b viewed in the direction of flight 24b, a further third aircraft seat 300'b is arranged in front of a further second aircraft seat 200'b, wherein in the second outer seat column 42b viewed in the direction of flight 24b, three additional further second aircraft seat 200'b are arranged behind the further second aircraft seat 200'b.

[0113] In aircraft cabin section 26b, three differently configured aircraft seat assemblies 100'b, 200'b, 300'b are arranged directly one behind the other in the second outer seat column 42b, along with several other aircraft seat assemblies 100'b, 200'b, 300'b, 500'b, 600'b, 700'b. The three differently configured aircraft seat assemblies 100'b, 200'b, 300'b, arranged in the second outer seat column 42b, along with several other aircraft seat assemblies 100'b, 200'b, 300'b, 500'b, 600'b, 700'b, are arranged directly one after the other in the direction of flight 24b.In the present case, in the first outer seat column 36b viewed in the direction of flight 24b, a further seventh aircraft seat 700'b is arranged in front of a further sixth aircraft seat 600'b, wherein in the first outer seat column 36b viewed in the direction of flight 24b, three additional further sixth aircraft seat 600'b are arranged behind the further sixth aircraft seat 600'b.

[0114] In principle, the preceding descriptions of the first inner seat column 38b also apply to the second outer seat column 42b. In principle, the preceding descriptions of the second inner seat column 40b also apply to the first outer seat column 36b.

[0115] In the aircraft cabin section 26b, two aircraft seat assemblies of the several aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b, namely the third aircraft seat assembly 300b and the seventh aircraft seat assembly 700b, form a seat pair 46b in two immediately adjacent seat gaps, namely the first inner seat gap 38b and the second inner seat gap 40b, wherein the seating directions 310b, 710b of the two aircraft seat assemblies 300b, 700b are arranged at least substantially parallel to the aircraft cabin center axis 16b and the aircraft seats 320b, 720b of the two aircraft seat assemblies 300b, 700b are arranged facing away from the aisle, wherein at least two of the seat pairs 46b are located in the two immediately adjacent seat gaps 38b, 40b are arranged.

[0116] The aircraft seating arrangement 14b comprises a first seating group 52b of three aircraft seating units arranged directly one behind the other in the first inner seat column 38b of the aircraft cabin section 26b, namely the first aircraft seating unit 100b, the second aircraft seating unit 200b, and the third aircraft seating unit 300b, each having different seating directions 110b, 210b, 310b, and whose aircraft seats 120b, 220b, 320b are arranged facing the aisle or away from the aisle. The seating directions 110b, 210b, 310b of the directly consecutive aircraft seating units 100b, 200b, 300b are arranged alternately within the first seating group 52b at least substantially parallel and at an angle to the aircraft cabin center axis 16b. The first seating group 52b forms a periodically repeatable sequence.Several identical first seating groups 52b can be arranged directly one behind the other along an aircraft longitudinal axis. Viewed in the direction of flight 24b, behind the first aircraft seating unit 100b, whose seating direction 110b is arranged at least substantially parallel to the aircraft cabin center axis 16b, an aircraft seating unit is arranged whose seating direction is arranged at least substantially parallel to the aircraft cabin center axis 16b. Viewed in the direction of flight 24b, in front of the first aircraft seating unit 100b, whose seating direction 110b is arranged at least substantially parallel to the aircraft cabin center axis 16b, an aircraft seating unit is arranged whose seating direction is angled to the aircraft cabin center axis 16a.Viewed in the direction of flight 24b, an aircraft seat is arranged both in front of and behind the second aircraft seat 200b, the seating direction of which 210b is angled to the aircraft cabin center axis 16b, and the seating direction of which is at least substantially parallel to the aircraft cabin center axis 16b. Viewed in the direction of flight 24b, an aircraft seat is arranged behind the third aircraft seat 300b, the seating direction of which 310b is at least substantially parallel to the aircraft cabin center axis 16b, and the seating direction of which is angled to the aircraft cabin center axis 16b.Viewed in the direction of flight 24b, an aircraft seat is arranged in front of the third aircraft seat 300b, the seating direction of which 310b is arranged at least substantially parallel to the aircraft cabin center axis 16b, the seating direction of which is arranged at least substantially parallel to the aircraft cabin center axis 16b.

[0117] The aircraft seating arrangement 14b comprises a second seating group 54b consisting of three aircraft seating units arranged directly one behind the other in the second inner seat column 40b of the aircraft cabin section 26b, namely the fifth aircraft seating unit 500b, the sixth aircraft seating unit 600b, and the seventh aircraft seating unit 700b, each with different seating directions 510b, 610b, and 710b, and whose aircraft seats 520b, 620b, 720b are arranged facing the aisle or away from the aisle. Within the second seating group 54b, the seating directions 510b, 610b, 710b of the directly consecutive aircraft seating units 500b, 600b, 700b are arranged alternately at least substantially parallel and at an angle to the aircraft cabin center axis 16b. The second seating group 54b forms a periodically repeatable sequence.Several identical second seating groups 54b can be arranged directly one behind the other along the aircraft cabin centerline 16b. Viewed in the direction of flight 24b, behind the fifth aircraft seating unit 500b, whose seating direction 510b is at least substantially parallel to the aircraft cabin centerline 16b, an aircraft seating unit is arranged whose seating direction is at least substantially parallel to the aircraft cabin centerline 16b. Viewed in the direction of flight 24b, in front of the fifth aircraft seating unit 500b, whose seating direction 510b is at least substantially parallel to the aircraft cabin centerline 16b, an aircraft seating unit is arranged whose seating direction is angled to the aircraft cabin centerline 16b.Viewed in the direction of flight 24b, an aircraft seat is arranged both in front of and behind the sixth aircraft seat 600b, the seating direction of which 610b is angled to the aircraft cabin center axis 16b, and the seating direction of which is at least substantially parallel to the aircraft cabin center axis 16b. Viewed in the direction of flight 24b, an aircraft seat is arranged behind the seventh aircraft seat 700b, the seating direction of which 710b is at least substantially parallel to the aircraft cabin center axis 16b, and the seating direction of which is angled to the aircraft cabin center axis 16b.Viewed in the direction of flight 24b, an aircraft seat is arranged in front of the seventh aircraft seat 700b, the seating direction of which 710b is arranged at least substantially parallel to the aircraft cabin center axis 16b, the seating direction of which is arranged at least substantially parallel to the aircraft cabin center axis 16b.

[0118] The first aircraft seat assembly 100b, the second aircraft seat assembly 200b and the third aircraft seat assembly 300b in the aircraft cabin section 26b differ in at least one comfort category, wherein the aircraft seat assemblies 100b, 200b, 300b each have a different value for the at least one comfort category, which is due to a different arrangement of the aircraft seats 120b, 220b, 320b and to the at least partially different design of the aircraft seat assemblies 100b, 200b, 300b.The fifth aircraft seat 500b, the sixth aircraft seat 600b, and the seventh aircraft seat 700b in aircraft cabin section 26b differ in at least one comfort category, with aircraft seat assemblies 500b, 600b, and 700b each having a different value for the at least one comfort category. This difference is due to a different arrangement of aircraft seats 520b, 620b, and 720b, and to the at least partially different design of the aircraft seat assemblies 500b, 600b, and 700b. The at least one comfort category describes a living space.

[0119] In the first inner seat column 38b, one of the additional second aircraft seat assemblies 200'b is arranged in the first seat row of the aircraft cabin section 26b, viewed against the direction of flight 24b. Viewed in the direction of flight 24b, another aircraft cabin module can be arranged in the central area 44b immediately behind the additional second aircraft seat assembly 200'b located in the first seat row of the aircraft cabin section 26b. This additional aircraft cabin module can be designed, in particular, as a front-row monument. This allows for greater comfort in the first seat row compared to the second aircraft seat assembly 200b, as more space is available in the first seat row.The additional second aircraft seat 200'b arranged in the first row of seats in the aircraft cabin section 26b can, in principle, differ in at least one comfort category from at least one aircraft seat of the several aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b.

[0120] In the second inner seat column 40b, one of the additional sixth aircraft seat assemblies 600'b is arranged in the first row of aircraft cabin section 26b, viewed against the direction of flight 24b. Viewed in the direction of flight 24b, another aircraft cabin module can be arranged in the central area 44b immediately behind the additional sixth aircraft seat assembly 600'b located in the first row of aircraft cabin section 26b. The additional sixth aircraft seat assembly 600'b located in the first row of aircraft cabin section 26b can, in principle, differ in at least one comfort category from at least one of the several aircraft seat assemblies 100b, 200b, 300b, 500b, 600b, 700b.

[0121] The Figure 6Figure 1 shows an unclaimed aircraft seating arrangement 14c in a third embodiment. The aircraft seating arrangement 14c is intended for use in a partially illustrated aircraft cabin 12c. The aircraft cabin 12c has a cabin centerline 16c. The cabin centerline 16c is configured as a longitudinal axis of the aircraft. The aircraft cabin 12c has two opposing cabin exterior walls 18c, 20c. The aircraft cabin 12c has a cabin floor 22c. The aircraft has a flight direction 24c in at least one operating state. The aircraft cabin 12c has a cabin section 26c along the cabin centerline 16c. In this case, the cabin section 26c is bounded by several schematically depicted cabin modules 30c along the cabin centerline 16c.The aircraft cabin 12c has a first cabin aisle 32c and a second cabin aisle 34c in cabin section 26c. The aircraft seating arrangement 14c includes a first outer seat column 36c. The aircraft seating arrangement 14c includes a first inner seat column 38c. The aircraft seating arrangement 14c includes a second inner seat column 40c. The aircraft seating arrangement 14c includes a second outer seat column 42c. The aircraft cabin 12c has a central section 44c.

[0122] The aircraft seating arrangement 14c comprises several aircraft seating assemblies 100c, 200c, 300c, 500c, 600c, and 700c arranged in the aircraft cabin section 26c. The several aircraft seating assemblies 100c, 200c, 300c, 500c, 600c, and 700c are configured differently from one another. In the present case, six differently configured aircraft seating assemblies 100c, 200c, 300c, 500c, 600c, and 700c are arranged in the aircraft cabin section 26c. The aircraft seating assemblies 100c, 200c, 300c, 500c, 600c, and 700c each have one aircraft seat. The aircraft seating assemblies 100c, 200c, 300c, 500c, 600c, and 700c each have a console. The aircraft seating arrangement 14c comprises a first aircraft seating assembly 100c, one of several aircraft seating assemblies 100c, 200c, 300c, 500c, 600c, and 700c. The first aircraft seating assembly 100c has a seating direction 110c. The first aircraft seating assembly 100c has a first aircraft seat 120c.The first aircraft seat assembly 100c has a first console 130c. The aircraft seat assembly 14c comprises a second aircraft seat assembly 200c, which can be one of several aircraft seat assemblies 100c, 200c, 300c, 500c, 600c, 700c. The second aircraft seat assembly 200c has a seating direction 210c. The second aircraft seat assembly 200c has a second aircraft seat 220c. The second aircraft seat assembly 200c has a second console 230c. The aircraft seat assembly 14c comprises a third aircraft seat assembly 300c, which can be one of several aircraft seat assemblies 100c, 200c, 300c, 500c, 600c, 700c. The third aircraft seat assembly 300c has a seating direction 310c. The third aircraft seating unit 300c includes a third aircraft seat 320c. The third aircraft seating unit 300c includes a third console 330c.Aircraft seating arrangement 14c includes a fifth aircraft seat 500c of the multiple aircraft seat assemblies 100c, 200c, 300c, 500c, 600c, 700c. The fifth aircraft seat 500c has a seating direction 510c. The fifth aircraft seat 500c has a fifth aircraft seat 520c. The fifth aircraft seat 500c has a fifth console 530c. Aircraft seating arrangement 14c includes a sixth aircraft seat 600c of the multiple aircraft seat assemblies 100c, 200c, 300c, 500c, 600c, 700c. The sixth aircraft seat 600c has a seating direction 610c. The sixth aircraft seat 600c has a sixth aircraft seat 620c. The sixth aircraft seat assembly 600c has a sixth console 630c. The aircraft seat assembly 14c includes a seventh aircraft seat assembly 700c of the several aircraft seat assemblies 100c, 200c, 300c, 500c, 600c, 700c.The seventh aircraft seating assembly 700c has a seating direction 710c. The seventh aircraft seating assembly 700c has a seventh aircraft seat 720c. The seventh aircraft seating assembly 700c has a seventh console 730c. The aircraft seating assembly 14c comprises several further first aircraft seating assemblies 100'c, which are designed at least substantially identically to the first aircraft seating assembly 100c. The aircraft seating assembly 14c comprises several further second aircraft seating assemblies 200'c, which are designed at least substantially identically to the second aircraft seating assembly 200c. The aircraft seating assembly 14c comprises several further third aircraft seating assemblies 300'c, which are designed at least substantially identically to the third aircraft seating assembly 300c.Aircraft seating arrangement 14c comprises several further fifth aircraft seating assemblies 500'c, which are designed at least substantially identically to the fifth aircraft seating assembly 500c. Aircraft seating arrangement 14c comprises several further sixth aircraft seating assemblies 600'c, which are designed at least substantially identically to the sixth aircraft seating assembly 600c. Aircraft seating arrangement 14c comprises several further seventh aircraft seating assemblies 700'c, which are designed at least substantially identically to the seventh aircraft seating assembly 700c.

[0123] In the aircraft cabin section 26c, two aircraft seat assemblies of the several aircraft seat assemblies 100c, 200c, 300c, 500c, 600c, 700c, namely the third aircraft seat assembly 300c and the seventh aircraft seat assembly 700c, form a seat pair 46c in two immediately adjacent seat gaps, namely the first inner seat gap 38c and the second inner seat gap 40c, wherein the seating directions 310c, 710c of the two aircraft seat assemblies 300c, 700c are arranged at least substantially parallel to the aircraft cabin center axis 16c and the aircraft seats 320c, 720c of the two aircraft seat assemblies 300c, 700c are arranged facing away from the aisle, wherein at least two of the seat pairs 46c are located in the two immediately adjacent seat gaps 38c, 40c. are arranged.The aircraft seating arrangement 14c has a first seating grouping 52c of three aircraft seating devices arranged directly one behind the other in the first inner seat column 38c in the aircraft cabin section 26c, namely the first aircraft seating device 100c, the second aircraft seating device 200c and the third aircraft seating device 300c, each having different seating directions 110c, 210c, 310c and whose aircraft seats 120c, 220c, 320c are arranged facing the aisle or away from the aisle.The aircraft seating arrangement 14c has a second seating grouping 54c of three aircraft seating devices arranged directly one behind the other in the second inner seating column 40c in the aircraft cabin section 26c, namely the fifth aircraft seating device 500c, the sixth aircraft seating device 600c and the seventh aircraft seating device 700c, each having different seating directions 510c, 610c, 710c and whose aircraft seats 520c, 620c, 720c are arranged facing the aisle or away from the aisle.

[0124] The first aircraft seat assembly 100c, the second aircraft seat assembly 200c and the third aircraft seat assembly 300c in the aircraft cabin section 26c differ in at least one comfort category, wherein the aircraft seat assemblies 100c, 200c, 300c each have a different value for the at least one comfort category, which is due to a different arrangement of the aircraft seats 120c, 220c, 320c and to the at least partially different design of the aircraft seat assemblies 100c, 200c, 300c.The fifth aircraft seat 500c, the sixth aircraft seat 600c and the seventh aircraft seat 700c in the aircraft cabin section 26c differ in at least one comfort category, wherein the aircraft seat assemblies 500c, 600c, 700c each have a different value for the at least one comfort category, which is due to a different arrangement of the aircraft seats 520c, 620c, 720c and to the at least partially different design of the aircraft seat assemblies 500c, 600c, 700c.

[0125] In contrast to the second embodiment, viewed in the direction of flight 24c, a further third aircraft seat 300'c is arranged in the first inner seat column 38c, and a further seventh aircraft seat 700'c is arranged in the second inner seat column 40c, in a final row of seats in the central area 44c of the aircraft cabin section 26c, viewed against the direction of flight 24c. In the first inner seat column 38c, viewed in the direction of flight 24c, two aircraft seats are arranged immediately behind the further third aircraft seat 300'c, the seating directions of which are arranged at least substantially parallel to the aircraft cabin center axis 16c.In the second inner seat column 40c, viewed in the direction of flight 24c, two aircraft seat assemblies are arranged immediately behind the further seventh aircraft seat assembly 700'c, the seating directions of which are arranged at least substantially parallel to the aircraft cabin center axis 16c.

[0126] The Figure 7 shows an unclaimed aircraft seat arrangement 14d in a fourth embodiment.

[0127] The aircraft seating arrangement 14d is intended for use in a partially depicted aircraft cabin 12d. The aircraft cabin 12d has a cabin centerline 16d. The cabin centerline 16d is configured as a longitudinal axis of the aircraft. The aircraft cabin 12d has two opposing cabin exterior walls 18d, 20d. The aircraft cabin 12d has a cabin floor 22d. The aircraft has a flight direction 24d in at least one operating state. The aircraft cabin 12d has a cabin section 26d along the cabin centerline 16d. In this case, the cabin section 26d is bounded by several schematically depicted cabin modules 30d along the cabin centerline 16d. The aircraft cabin 12d has a first cabin aisle 32d and a second cabin aisle 34d in the cabin section 26d.The aircraft seating arrangement 14d comprises a first outer seat column 36d. The aircraft seating arrangement 14d comprises a first inner seat column 38d. The aircraft seating arrangement 14d comprises a second inner seat column 40d. The aircraft seating arrangement 14d comprises a second outer seat column 42d. The aircraft cabin 12d has a central section 44d.

[0128] The aircraft seating arrangement 14d comprises several aircraft seating assemblies 100d, 200d, 300d, 500d, 600d, and 700d arranged in the aircraft cabin section 26d. The several aircraft seating assemblies 100d, 200d, 300d, 500d, 600d, and 700d are configured differently from one another. In the present case, six differently configured aircraft seating assemblies 100d, 200d, 300d, 500d, 600d, and 700d are arranged in the aircraft cabin section 26d. The aircraft seating assemblies 100d, 200d, 300d, 500d, 600d, and 700d each have one aircraft seat. The aircraft seating assemblies 100d, 200d, 300d, 500d, 600d, and 700d each have a console. The aircraft seating arrangement 14d comprises a first aircraft seating assembly 100d, one of several aircraft seating assemblies 100d, 200d, 300d, 500d, 600d, and 700d. The first aircraft seating assembly 100d has a seating direction 110d. The first aircraft seating assembly 100d has a first aircraft seat 120d.The first aircraft seat assembly 100d has a first console 130d. The aircraft seat assembly 14d comprises a second aircraft seat assembly 200d, which can be one of several aircraft seat assemblies 100d, 200d, 300d, 500d, 600d, 700d. The second aircraft seat assembly 200d has a seating direction 210d. The second aircraft seat assembly 200d has a second aircraft seat 220d. The second aircraft seat assembly 200d has a second console 230d. The aircraft seat assembly 14d comprises a third aircraft seat assembly 300d, which can be one of several aircraft seat assemblies 100d, 200d, 300d, 500d, 600d, 700d. The third aircraft seat assembly 300d has a seating direction 310d. The third aircraft seat assembly 300d includes a third aircraft seat 320d. The third aircraft seat assembly 300d includes a third console 330d.Aircraft seating arrangement 14d comprises a fifth aircraft seat 500d of the multiple aircraft seat assemblies 100d, 200d, 300d, 500d, 600d, 700d. The fifth aircraft seat 500d has a seating direction 510d. The fifth aircraft seat 500d has a fifth aircraft seat 520d. The fifth aircraft seat 500d has a fifth console 530d. Aircraft seating arrangement 14d comprises a sixth aircraft seat 600d of the multiple aircraft seat assemblies 100d, 200d, 300d, 500d, 600d, 700d. The sixth aircraft seat 600d has a seating direction 610d. The sixth aircraft seat 600d has a sixth aircraft seat 620d. The sixth aircraft seat assembly 600d has a sixth console 630d. The aircraft seat assembly 14d includes a seventh aircraft seat assembly 700d of the several aircraft seat assemblies 100d, 200d, 300d, 500d, 600d, 700d.The seventh aircraft seat assembly 700d has a seating direction 710d. The seventh aircraft seat assembly 700d has a seventh aircraft seat 720d. The seventh aircraft seat assembly 700d has a seventh console 730d. The aircraft seat assembly 14d comprises several further first aircraft seat assemblies 100'd, which are designed at least substantially identically to the first aircraft seat assembly 100d. The aircraft seat assembly 14d comprises several further second aircraft seat assemblies 200'd, which are designed at least substantially identically to the second aircraft seat assembly 200d. The aircraft seat assembly 14d comprises several further third aircraft seat assemblies 300'd, which are designed at least substantially identically to the third aircraft seat assembly 300d.The aircraft seating arrangement 14d comprises several further fourth aircraft seating assemblies 400'd, which are designed at least substantially identically to the fourth aircraft seating assembly 400a from the first embodiment. The aircraft seating arrangement 14d comprises several further fifth aircraft seating assemblies 500'd, which are designed at least substantially identically to the fifth aircraft seating assembly 500d. The aircraft seating arrangement 14d comprises several further sixth aircraft seating assemblies 600'd, which are designed at least substantially identically to the sixth aircraft seating assembly 600d. The aircraft seating arrangement 14d comprises several further seventh aircraft seating assemblies 700'd, which are designed at least substantially identically to the seventh aircraft seating assembly 700d.The aircraft seating arrangement 14d comprises several further eighth aircraft seating devices 800'd, which are designed at least substantially identically to the eighth aircraft seating device 800a from the first embodiment.

[0129] In the aircraft cabin section 26d, two aircraft seat assemblies of the several aircraft seat assemblies 100d, 200d, 300d, 500d, 600d, 700d, namely the third aircraft seat assembly 300d and the seventh aircraft seat assembly 700d, form a seat pair 46d in two immediately adjacent seat gaps, namely the first inner seat gap 38d and the second inner seat gap 40d, wherein the seating directions 310d, 710d of the two aircraft seat assemblies 300d, 700d are arranged at least substantially parallel to the aircraft cabin center axis 16d and the aircraft seats 320d, 720d of the two aircraft seat assemblies 300d, 700d are arranged facing away from the aisle, wherein at least two of the seat pairs 46d are located in the two immediately adjacent seat gaps 38d, 40d. are arranged.The aircraft seating arrangement 14d has a first seating grouping 52d of three aircraft seating devices arranged directly one behind the other in the first inner seat column 38d in the aircraft cabin section 26d, namely the first aircraft seating device 100d, the second aircraft seating device 200d and the third aircraft seating device 300d, each having different seating directions 110d, 210d, 310d and whose aircraft seats 120d, 220d, 320d are arranged facing the aisle or away from the aisle.The aircraft seating arrangement 14d has a second seating grouping 54d of three aircraft seating devices arranged directly one behind the other in the second inner seat column 40d in the aircraft cabin section 26d, namely the fifth aircraft seating device 500d, the sixth aircraft seating device 600d and the seventh aircraft seating device 700d, each having different seating directions 510d, 610d, 710d and whose aircraft seats 520d, 620d, 720d are arranged facing the aisle or away from the aisle.

[0130] The first aircraft seat assembly 100d, the second aircraft seat assembly 200d and the third aircraft seat assembly 300d in the aircraft cabin section 26d differ in at least one comfort category, wherein the aircraft seat assemblies 100d, 200d, 300d each have a different value for the at least one comfort category, which is due to a different arrangement of the aircraft seats 120d, 220d, 320d and to the at least partially different design of the aircraft seat assemblies 100d, 200d, 300d.The fifth aircraft seat 500d, the sixth aircraft seat 600d and the seventh aircraft seat 700d in the aircraft cabin section 26d differ in at least one comfort category, wherein the aircraft seat assemblies 500d, 600d, 700d each have a different value for the at least one comfort category, which is due to a different arrangement of the aircraft seats 520d, 620d, 720d and to the at least partially different design of the aircraft seat assemblies 500d, 600d, 700d.

[0131] In contrast to the third embodiment, in the first outer seat column 36d of the aircraft cabin section 26d, four differently configured aircraft seat assemblies 500'd, 600'd, 700'd, 800'd of several further aircraft seat assemblies 100'd, 200'd, 300'd, 400'd, 500'd, 600'd, 700'd, 800'd are arranged. In the first outer seat column 36d, a further fifth aircraft seat assembly 500'd, a further seventh aircraft seat assembly 700'd and a further eighth aircraft seat assembly 800'd are arranged directly one behind the other. In the first outer seat column 36d, a further eighth aircraft seat assembly 800'd, a further fifth aircraft seat assembly 500'd and a further sixth aircraft seat assembly 600'd are arranged directly one behind the other.Between a further seventh aircraft seat 700'd and a further fifth aircraft seat 500'd, two further eighth aircraft seat assemblies 800'd are arranged in the first outer seat column 36d. Between the further fifth aircraft seat 500'd and a further seventh aircraft seat 700'd, two further sixth aircraft seat assemblies 600'd are arranged in the first outer seat column 36d.

[0132] In contrast to the third embodiment, in the second outer seat column 42d of the aircraft cabin section 26d, four differently configured aircraft seat assemblies 100'd, 200'd, 300'd, 400'd of several further aircraft seat assemblies 100'd, 200'd, 300'd, 400'd, 500'd, 600'd, 700'd, 800'd are arranged. In the second outer seat column 42d, a further first aircraft seat assembly 100'd, a further third aircraft seat assembly 300'd and a further fourth aircraft seat assembly 400'd are arranged directly one behind the other. In the second outer seat column 42d, a further fourth aircraft seat assembly 400'd, a further first aircraft seat assembly 100'd and a further second aircraft seat assembly 200'd are arranged directly one behind the other.Between a further third aircraft seat 300'd and a further first aircraft seat 100'd, two further fourth aircraft seat assemblies 400'd are arranged in the second outer seat column 42d. Between the further first aircraft seat 100'd and a further third aircraft seat 300'd, two further second aircraft seat assemblies 200'd are arranged in the second outer seat column 42d.

[0133] The Figure 8Figure 1 shows an aircraft seating arrangement 14e in a fifth embodiment. The aircraft seating arrangement 14e is intended for use in a partially illustrated aircraft cabin 12e. The aircraft cabin 12e has a cabin centerline 16e. The cabin centerline 16e is configured as a longitudinal axis of the aircraft. The aircraft cabin 12e has two opposing cabin exterior walls 18e, 20e. The aircraft has a flight direction 24e in at least one operating state. The aircraft cabin 12e has a cabin section 26e along the cabin centerline 16e. In this case, the cabin section 26e is bounded by several partition elements 28e along the cabin centerline 16e. The aircraft cabin 12e has a first cabin aisle 32e and a second cabin aisle 34e in the cabin section 26e.The aircraft seating arrangement 14e comprises a first outer seat column 36e. The aircraft seating arrangement 14e comprises a first inner seat column 38e. The aircraft seating arrangement 14e comprises a second inner seat column 40e. The aircraft seating arrangement 14e comprises a second outer seat column 42e. The aircraft cabin 12e has a central section 44e. The aircraft cabin 12e comprises a first cabin side 56e and a second cabin side 58e.

[0134] The aircraft seating arrangement 14e comprises several aircraft seating assemblies 100e, 200e, 300e, 500e, 600e, 700e, and 800e arranged in the aircraft cabin section 26e. The several aircraft seating assemblies 100e, 200e, 300e, 500e, 600e, 700e, and 800e are configured differently from one another. In the present case, seven differently configured aircraft seating assemblies 100e, 200e, 300e, 500e, 600e, 700e, and 800e are arranged in the aircraft cabin section 26e. The aircraft seating assemblies 100e, 200e, 300e, 500e, 600e, 700e, and 800e each have one aircraft seat. The aircraft seating assemblies 100e, 200e, 300e, 500e, 600e, 700e, and 800e each have a console. The aircraft seating arrangement 14e comprises a first aircraft seating assembly 100e of the several aircraft seating assemblies 100e, 200e, 300e, 500e, 600e, 700e, and 800e. The first aircraft seating assembly 100e has a seating direction 110e.The first aircraft seating assembly 100e includes a first aircraft seat 120e. The first aircraft seating assembly 100e includes a first console 130e. The aircraft seating assembly 14e includes a second aircraft seating assembly 200e, one of several aircraft seating assemblies 100e, 200e, 300e, 500e, 600e, 700e, 800e. The second aircraft seating assembly 200e has a seating direction 210e. The second aircraft seating assembly 200e includes a second aircraft seat 220e. The second aircraft seating assembly 200e includes a second console 230e. The aircraft seating assembly 14e includes a third aircraft seating assembly 300e, one of several aircraft seating assemblies 100e, 200e, 300e, 500e, 600e, 700e, 800e. The third aircraft seat assembly 300e has a seating direction 310e. The third aircraft seat assembly 300e has a third aircraft seat 320e. The third aircraft seat assembly 300e has a third console 330e.Aircraft seating arrangement 14e comprises a fifth aircraft seat 500e of the multiple aircraft seat assemblies 100e, 200e, 300e, 500e, 600e, 700e, 800e. The fifth aircraft seat 500e has a seating direction 510e. The fifth aircraft seat 500e includes a fifth aircraft seat 520e. The fifth aircraft seat 500e includes a fifth console 530e. Aircraft seating arrangement 14e comprises a sixth aircraft seat 600e of the multiple aircraft seat assemblies 100e, 200e, 300e, 500e, 600e, 700e, 800e. The sixth aircraft seat 600e has a seating direction 610e. The sixth aircraft seating assembly 600e includes a sixth aircraft seat 620e. The sixth aircraft seating assembly 600e includes a sixth console 630e. The aircraft seating assembly 14e comprises a seventh aircraft seating assembly 700e of the multiple aircraft seating assemblies 100e, 200e, 300e, 500e, 600e, 700e, 800e.The seventh aircraft seating unit 700e has a seating direction of 710e. The seventh aircraft seating unit 700e has a seventh aircraft seat 720e. The seventh aircraft seating unit 700e has a seventh console 730e. The aircraft seating arrangement 14e comprises an eighth aircraft seating unit 800e of the several aircraft seating units 100e, 200e, 300e, 500e, 600e, 700e, 800e. The eighth aircraft seating unit 800e has a seating direction of 810e. The eighth aircraft seating unit 800e has an eighth aircraft seat 820e. The eighth aircraft seating unit 800e has an eighth console 830e. The aircraft seating arrangement 14e may comprise several further first aircraft seating arrangements which are designed at least substantially identically to the first aircraft seating arrangement 100e.The aircraft seating arrangement 14e comprises several further second aircraft seating assemblies 200'e, which are designed at least substantially identically to the second aircraft seating assembly 200e. The aircraft seating arrangement 14e comprises at least one further third aircraft seating assembly 300'e, which is designed at least substantially identically to the third aircraft seating assembly 300e. The aircraft seating arrangement 14e may comprise several further fifth aircraft seating assemblies, which are designed at least substantially identically to the fifth aircraft seating assembly 500e. The aircraft seating arrangement 14e comprises several further sixth aircraft seating assemblies 600'e, which are designed at least substantially identically to the sixth aircraft seating assembly 600e. The aircraft seating arrangement 14e comprises at least one further seventh aircraft seating assembly 700'e, which is designed at least substantially identically to the seventh aircraft seating assembly 700e.The aircraft seating arrangement 14e may include several further eighth aircraft seating devices which are at least substantially identical to the eighth aircraft seating device 800e.

[0135] In contrast to the first embodiment, an arrangement of aircraft seat devices 200e, 600e, 800e of the several aircraft seat devices 100e, 200e, 300e, 500e, 600e, 700e, 800e in the aircraft cabin section 26e in the first outer seat column 36e and the first inner seat column 38e on the first aircraft cabin side 56e is asymmetrically formed to an arrangement of aircraft seat devices 100e, 300e, 500e, 700e of the several aircraft seat devices 100e, 200e, 300e, 500e, 600e, 700e, 800e in the second inner seat column 38e and the second outer seat column 42e on the second aircraft cabin side 58e. The first aircraft cabin side 56e is separated from the second aircraft cabin side 58e by an imaginary aircraft cabin center plane, which is aligned perpendicular to an aircraft cabin floor 22e of the aircraft cabin 12e along the aircraft cabin center axis 16e.An arrangement of aircraft seating devices 200e, 200'e of the several aircraft seating devices 100e, 200e, 300e, 500e, 600e, 700e, 800e in the first inner seat column 38e on the first aircraft cabin side 56e is, with respect to the aircraft cabin center axis 16e, asymmetrical to an arrangement of aircraft seating devices 500e, 700e, 700'e of the several aircraft seating devices 100e, 200e, 300e, 500e, 600e, 700e, 800e in the second inner seat column 38e on the second aircraft cabin side 58e. An arrangement of aircraft seating devices 500e, 700e, 700'e of the several aircraft seating devices 100e, 200e, 300e, 500e, 600e, 700e, 800e in the second inner seat column 40e on the second aircraft cabin side 58e is symmetrical to an arrangement of aircraft seating devices 100e, 300e, 300'e of the several aircraft seating devices 100e, 200e, 300e, 500e, 600e, 700e, 800e in the second outer seat column 42e on the second aircraft cabin side 58e.

[0136] The first cabin side 56e and the second cabin side 58e each have exactly one of the cabin aisles 32e and 34e, respectively. The first cabin aisle 32e is located on the first cabin side 56e. The second cabin aisle 34e is located on the second cabin side 58e. It is conceivable that the cabin 12e in cabin section 26e has at least one partition along the central cabin axis 16e, separating the first cabin side 56e from the second cabin side 58e. This would advantageously increase privacy in a wide-body aircraft.

[0137] In the first outer seat column 36e, only aircraft seat assemblies 600e, 800e of the several aircraft seat assemblies 100e, 200e, 300e, 500e, 600e, 700e, 800e are arranged, whose seating directions 610e, 810e are angled to the aircraft cabin center axis 16e. In the first inner seat column 38e, only aircraft seat assemblies 200e, 200'e of the several aircraft seat assemblies 100e, 200e, 300e, 500e, 600e, 700e, 800e are arranged, whose seating directions 210e are angled to the aircraft cabin center axis 16e. The first inner seating column 38e contains exclusively aircraft seat assemblies 200e of the multiple aircraft seat assemblies 100e, 200e, 300e, 500e, 600e, 700e, 800e, whose aircraft seats 220e are arranged aisle-side. The first outer seating column 36e is partially mirrored across the first aircraft cabin aisle 32e to the first inner seating column 38e.

[0138] In the second inner seat column 40e, only aircraft seat assemblies 500e and 700e of the multiple aircraft seat assemblies 100e, 200e, 300e, 500e, 600e, 700e, and 800e are arranged, the seating directions of which 510e and 710e are arranged at least substantially parallel to the aircraft cabin center axis 16e. In the second outer seat column 42e, only aircraft seat assemblies 100e and 300e of the multiple aircraft seat assemblies 100e, 200e, 300e, 500e, 600e, 700e, and 800e are arranged, the seating directions of which 110e and 310e are arranged at least substantially parallel to the aircraft cabin center axis 16e. In the second inner seat column 40e, only aircraft seat units 500e, 700e of the several aircraft seat units 100e, 200e, 300e, 500e, 600e, 700e, 800e are arranged, whose aircraft seats 220e, 520e are alternately arranged facing the aisle or away from the aisle.The second outer seating column 42e contains exclusively aircraft seat assemblies 100e and 300e of the multiple aircraft seat assemblies 100e, 200e, 300e, 500e, 600e, 700e, and 800e, whose aircraft seats 120e and 320e are alternately arranged facing the aisle or away from the aisle. The second outer seating column 42e is mirrored across the second aircraft cabin aisle 34e to the second inner seating column 40e.

[0139] The aircraft seating arrangement 14e includes an intermediate space unit 60e. The intermediate space unit 60e is located in the first outer seat column 36e. The intermediate space unit 60e is positioned along an aircraft longitudinal axis between the sixth aircraft seat unit 600e and the eighth aircraft seat unit 800e. The intermediate space unit 60e is designed to functionally utilize the free space provided and / or created between two aircraft seat units. The intermediate space unit 60e can be configured as a storage compartment for items such as jackets, coats, blankets, and / or amenity kits. Alternatively, the intermediate space unit 60e can be configured as a storage compartment for hand luggage. The intermediate space unit 60e can also be configured as a bar, a vending machine, and / or a display area for in-flight shopping products.Furthermore, the intermediate unit 60e can be configured as a server rack that is electronically connected to at least some of the multiple aircraft seating units 100e, 200e, 300e, 500e, 600e, 700e, 800e in the aircraft cabin section 26e. Alternatively, the intermediate unit 60e can also be configured as a console or as a cabin monument.

[0140] In aircraft cabin section 26e, the first aircraft seat assembly 100e, the second aircraft seat assembly 200e, the third aircraft seat assembly 300e, the fifth aircraft seat assembly 500e, the sixth aircraft seat assembly 600e, the seventh aircraft seat assembly 700e, and the eighth aircraft seat assembly 800e differ in at least one comfort category, wherein the aircraft seat assemblies 100e, 200e, 300e, 500e, 600e, 700e, and 800e each have a different value for the at least one comfort category, which is achieved through a different arrangement of the aircraft seats 120e, 220e, 320e, 520e, 620e, 720e, and 820e and through the at least partially different design of the aircraft seat assemblies 100e, 200e, and 300e. 500e, 600e, 700e, 800e is conditional.

[0141] The one in Figure 8The aircraft seating arrangement 14e shown can in principle be extended by further aircraft seating arrangements 100'e, 200'e, 300'e, 500'e, 600'e, 700'e, 800'e viewed in the direction of flight 24e.

[0142] The Figure 9Figure 1 shows an aircraft seating arrangement 14f in a sixth embodiment. The aircraft seating arrangement 14f is intended for use in a partially illustrated aircraft cabin 12f. The aircraft cabin 12f has a cabin centerline 16f. The cabin centerline 16f is configured as a longitudinal axis of the aircraft. The aircraft cabin 12f has two opposing cabin exterior walls 18f, 20f. The aircraft has a flight direction 24f in at least one operating state. The aircraft cabin 12f has a cabin section 26f along the cabin centerline 16f. The aircraft cabin 12f has a first cabin aisle 32f and a second cabin aisle 34f in the cabin section 26f. The aircraft seating arrangement 14f includes a first outer seat column 36f. The aircraft seating arrangement 14f includes a first inner seat column 38f.The aircraft seating arrangement 14f includes a second inner seat column 40f. The aircraft seating arrangement 14f includes a second outer seat column 42f. The aircraft cabin 12f has a central section 44f. The aircraft cabin 12f includes a first cabin side 56f and a second cabin side 58f.

[0143] The aircraft seating arrangement 14f comprises several aircraft seating assemblies 100f, 300f, 400f, 500f, 700f arranged in the aircraft cabin section 26f. The several aircraft seating assemblies 100f, 300f, 400f, 500f, 700f are configured differently from one another. The aircraft seating assemblies 100f, 300f, 400f, 500f, 700f each have one aircraft seat. The aircraft seating assemblies 100f, 300f, 400f, 500f, 700f each have one console. The aircraft seating arrangement 14f comprises a first aircraft seating assembly 100f of the several aircraft seating assemblies 100f, 300f, 400f, 500f, 700f. The first aircraft seating arrangement 100f has a seating direction 110f. The first aircraft seating arrangement 100f has a first aircraft seat 120f. The first aircraft seating arrangement 100f has a first console 130f. The aircraft seating arrangement 14f comprises a third aircraft seating arrangement 300f of the multiple aircraft seating arrangements 100f, 300f, 400f, 500f, 700f.The third aircraft seat assembly 300f has a seating direction 310f. The third aircraft seat assembly 300f has a third aircraft seat 320f. The third aircraft seat assembly 300f has a third console 330f. The aircraft seat assembly 14f comprises a fourth aircraft seat assembly 400f of the multiple aircraft seat assemblies 100f, 300f, 400f, 500f, 700f. The fourth aircraft seat assembly 400f has a seating direction 410f. The fourth aircraft seat assembly 400f has a fourth aircraft seat 420f. The fourth aircraft seat assembly 400f has a fourth console 430f. The aircraft seat assembly 14f comprises a fifth aircraft seat assembly 500f of the multiple aircraft seat assemblies 100f, 300f, 400f, 500f, 700f. The fifth aircraft seating unit 500f has a seating direction 510f. The fifth aircraft seating unit 500f has a fifth aircraft seat 520f. The fifth aircraft seating unit 500f has a fifth console 530f.The aircraft seating arrangement 14f comprises a seventh aircraft seating device 700f of the multiple aircraft seating devices 100f, 300f, 400f, 500f, 700f. The seventh aircraft seating device 700f has a seating direction 710f. The seventh aircraft seating device 700f has a seventh aircraft seat 720f. The seventh aircraft seating device 700f has a seventh console 730f. The aircraft seating arrangement 14f comprises at least one further first aircraft seating device 100'f, which is designed at least substantially identically to the first aircraft seating device 100f. The aircraft seating arrangement 14f may comprise several further third aircraft seating devices, which are designed at least substantially identically to the third aircraft seating device 300f. The aircraft seating arrangement 14f comprises several further fourth aircraft seating arrangements 400'f, which are designed at least substantially identically to the fourth aircraft seating arrangement 400f.Aircraft seating arrangement 14f comprises at least one further fifth aircraft seating arrangement 500'f, which is designed at least substantially identically to the fifth aircraft seating arrangement 500f. Aircraft seating arrangement 14f comprises several further seventh aircraft seating arrangements 700'f, which are designed at least substantially identically to the seventh aircraft seating arrangement 700f.

[0144] In contrast to the fifth embodiment, the aircraft seating arrangement 14f comprises several alternative aircraft seating arrangements 1000f, 3000f, 5000f, 7000f, which are arranged in the aircraft cabin section 26f. The aircraft seating arrangement 14f comprises an alternative first aircraft seating arrangement 1000f. The alternative first aircraft seating arrangement 1000f has a seating direction 1100f. The seating direction 1100f of the alternative first aircraft seating arrangement 1000f is oriented opposite to the direction of flight 24f. The seating direction 1100f of the alternative first aircraft seating arrangement 1000f is oriented at least substantially parallel to the aircraft cabin centerline 16f. The alternative first aircraft seating arrangement 1000f has an alternative first aircraft seat 1200f. The alternative first aircraft seating arrangement 1000f has an alternative first console 1300f.The alternative first aircraft seating arrangement 1000f is mirrored about an axis relative to the first aircraft seating arrangement 100f, the axis being perpendicular to the aircraft cabin centerline 16f and parallel to an aircraft cabin floor 22f of the aircraft cabin 12f. The aircraft seating arrangement 14f may comprise at least one further alternative first aircraft seating arrangement, which is at least substantially identical to the alternative first aircraft seating arrangement 1000f. The aircraft seating arrangement 14f comprises an alternative third aircraft seating arrangement 3000f. The alternative third aircraft seating arrangement 3000f has a seating direction 3100f. The seating direction 3100f of the alternative third aircraft seating arrangement 3000f is oriented opposite to the direction of flight 24f. The seating direction 3100f of the alternative third aircraft seating arrangement 3000f is oriented at least substantially parallel to the aircraft cabin centerline 16f.The alternative third aircraft seating arrangement 3000f includes an alternative third aircraft seat 3200f. The alternative third aircraft seating arrangement 3000f includes an alternative third console 3300f. The alternative third aircraft seating arrangement 3000f is configured as a mirror image of the third aircraft seating arrangement 300f about an axis, the axis being perpendicular to the aircraft cabin centerline 16f and parallel to the aircraft cabin floor 22f. The aircraft seating arrangement 14f includes several further alternative third aircraft seating arrangements 3000'f, which are configured at least substantially identically to the alternative third aircraft seating arrangement 3000f. The aircraft seating arrangement 14f includes an alternative fifth aircraft seating arrangement 5000f. The alternative fifth aircraft seating arrangement 5000f has a seating direction 5100f.The seating direction 5100f of the alternative fifth aircraft seating arrangement 5000f is oriented opposite to the direction of flight 24f. The seating direction 5100f of the alternative fifth aircraft seating arrangement 5000f is oriented at least substantially parallel to the aircraft cabin centerline 16f. The alternative fifth aircraft seating arrangement 5000f includes an alternative fifth aircraft seat 5200f. The alternative fifth aircraft seating arrangement 5000f includes an alternative fifth console 5300f. The alternative fifth aircraft seating arrangement 5000f is configured as a mirror image of the fifth aircraft seating arrangement 500f about an axis that is perpendicular to the aircraft cabin centerline 16f and parallel to the aircraft cabin floor 22f. The aircraft seating arrangement 14f comprises several further alternative fifth aircraft seating arrangements 5000'f that are configured at least substantially identically to the alternative fifth aircraft seating arrangement 5000f.Aircraft seating arrangement 14f includes an alternative seventh aircraft seating arrangement 7000f. The alternative seventh aircraft seating arrangement 7000f has a seating direction 7100f. The seating direction 7100f of the alternative seventh aircraft seating arrangement 7000f is oriented opposite to the direction of flight 24f. The seating direction 7100f of the alternative seventh aircraft seating arrangement 7000f is oriented at least substantially parallel to the aircraft cabin centerline 16f. The alternative seventh aircraft seating arrangement 7000f includes an alternative seventh aircraft seat 7200f. The alternative seventh aircraft seating arrangement 7000f includes an alternative seventh console 7300f. The alternative seventh aircraft seat device 7000f is designed as a mirror image about an axis to the seventh aircraft seat device 700f, wherein the axis is perpendicular to the aircraft cabin center axis 16f and parallel to the aircraft cabin floor 22f.The aircraft seating arrangement 14f comprises several further alternative seventh aircraft seating arrangements 7000'f, which are designed at least substantially identically to the alternative seventh aircraft seating arrangement 7000f. In contrast to the preceding embodiments, the seating directions 3100f, 5100f, 7100f of some of the several aircraft seating arrangements 100f, 300f, 400f, 500f, 700f, 1000f, 3000f, 5000f, 7000f in the aircraft cabin section 26f are oriented at least substantially opposite to the direction of flight 24f. In the aircraft cabin section 26f, nine differently designed aircraft seat units 100f, 300f, 400f, 500f, 700f, 1000f, 3000f, 5000f, 7000f are arranged in the present case.

[0145] An arrangement of aircraft seating assemblies 100f, 300f, 3000f, 700f, 7000f of the multiple aircraft seating assemblies 100f, 300f, 400f, 500f, 700f, 3000f, 5000f, 7000f in the aircraft cabin section 26f in the first outer seat column 36f and the first inner seat column 38f on the first aircraft cabin side 56f is asymmetrical to an arrangement of aircraft seating assemblies 400f, 500f, 700f, 5000f, 7000f of the multiple aircraft seating assemblies 100f, 300f, 400f, 500f, 700f, 3000f, 5000f, 7000f in the second inner seat column 38f and the second outer seat column 42f on the second aircraft cabin side 58f.

[0146] In the first outer seat column 36f, only aircraft seat devices 500f, 700f, 5000f, 7000f of the several aircraft seat devices 100f, 300f, 400f, 500f, 700f are arranged, whose seating directions 510f, 710f, 5100f, 7100f are arranged at least substantially parallel to the aircraft cabin center axis 16f. In the first outer seat column, the seating directions of the seventh aircraft seat 700f, the alternative fifth aircraft seat 5000f, one of the further seventh aircraft seat 700'f, one of the further alternative fifth aircraft seat 5000'f and one of the further alternative seventh aircraft seat 7000'f are oriented alternately in the direction of flight 24f and opposite to the direction of flight 24f along a longitudinal axis of the aircraft.

[0147] The aircraft seating arrangement 14f comprises several auxiliary consoles 62f, 64f, 66f. Each auxiliary console 62f, 64f, 66f contains two footwells for two aircraft seating assemblies 1000f, 3000f, 500f, 7000f, 700f, 5000f, respectively, which are arranged directly adjacent to the corresponding auxiliary consoles 62f, 64f, 66f. Auxiliary console 62f is located in the first outermost seat column 36f, viewed along an aircraft longitudinal axis, between the seventh aircraft seating assembly 700f and the alternative fifth aircraft seating assembly 5000f. Auxiliary console 62f separates the seventh aircraft seating assembly 700f from the alternative fifth aircraft seating assembly 5000f. The seating directions 710f, 5100f of the aircraft seating arrangements 700f, 5000f, which are spaced apart by the additional console 62f, are oriented in opposite directions to each other.

[0148] The seventh aircraft seat 700f, the additional console 62f, and the alternative fifth aircraft seat 5000f form a seat grouping 68f of aircraft seat arrangement 14f in the first outer seat column 36f. The seat grouping 68f has a base area that is at least substantially rectangular. The seat grouping 68f forms a periodically repeatable sequence. Several identical seat groupings 68f can be arranged directly one behind the other along an aircraft longitudinal axis.

[0149] In the first inner seat column 38f, only aircraft seat devices 100f, 300f, 1000f, 3000f of the several aircraft seat devices 100f, 300f, 400f, 500f, 700f are arranged, whose seating directions 110f, 310f, 1100f, 3100f are arranged at least substantially parallel to the aircraft cabin center axis 16f. In the first inner seat column 38f, only aircraft seat assemblies 100f, 300f, 1000f, 3000f of the multiple aircraft seat assemblies 100f, 300f, 400f, 500f, 700f are arranged, whose aircraft seats 120f, 320f, 1200f, 3200f are alternately arranged facing the aisle or away from the aisle. The first aircraft seat assembly 100f, the third aircraft seat assembly 300f and the further first aircraft seat assembly 100'f are arranged directly one behind the other. The third aircraft seat assembly 300f separates the first aircraft seat assembly 100f from the further first aircraft seat assembly 100'f.The additional console 64f is arranged in the first inner seat column 38f, viewed along an aircraft longitudinal axis, between the first aircraft seat 100f and the alternative third aircraft seat 3000f. The additional console 64f separates the first aircraft seat 100f from the alternative third aircraft seat 3000f. The seating directions 110f and 3100f of the aircraft seats 100f and 3000f, separated from each other by the additional console 64f, are oriented in opposite directions.

[0150] In the second inner seat column 40f, only aircraft seat devices 500f, 700'f, 5000'f, 7000f of the several aircraft seat devices 100f, 300f, 400f, 500f, 700f are arranged, whose seating directions 510f, 710f, 5100f, 7100f are arranged at least substantially parallel to the aircraft cabin center axis 16f. In the second inner seating column 40f, only aircraft seating devices 500f, 700'f, 5000'f, 7000f of the several aircraft seating devices 100f, 300f, 400f, 500f, 700f are arranged, whose aircraft seats 520f, 720f, 5200f, 7200f are alternately arranged facing the aisle or away from the aisle.

[0151] The fifth aircraft seat 500f, one of the further seventh aircraft seat assemblies 700'f, and the further fifth aircraft seat assemblies 500'f are arranged directly one behind the other. The further seventh aircraft seat assemblies 700'f space the fifth aircraft seat assemblies 500f from the further fifth aircraft seat assemblies 500'f. The auxiliary console 66f is arranged in the second inner seat column 40f, viewed along an aircraft longitudinal axis, between the fifth aircraft seat assemblies 500f and the alternative seventh aircraft seat assemblies 7000f. The auxiliary console 66f spaced the fifth aircraft seat assemblies 500f from the alternative seventh aircraft seat assemblies 7000f. The seating directions 510f and 7100f of the aircraft seat assemblies 500f and 7000f, spaced from each other by the auxiliary console 66f, are oriented in opposite directions to each other.The first inner seat column 38f is mirrored across the aircraft cabin center axis 16f to the second inner seat column 40f.

[0152] In the second outer seat column 42e, only aircraft seat assemblies 400f, 400'f of the several aircraft seat assemblies 100f, 300f, 400f, 500f, 700f are arranged, whose aircraft seats 420f are arranged facing away from the aisle. In the second outer seat column 42e, only aircraft seat assemblies 400f, 400'f of the several aircraft seat assemblies 100f, 300f, 400f, 500f, 700f are arranged, whose seating directions are arranged at an angle to the aircraft cabin center axis 16f.

[0153] The one in Figure 9 The aircraft seating arrangement shown 14f can in principle be extended by further aircraft seating arrangements 100'f, 300'f, 400'f, 500'f, 700'f, 3000'f, 5000'f, 7000'f viewed in the direction of flight 24f.

[0154] In aircraft cabin section 26f, the first aircraft seat configuration 100f, the third aircraft seat configuration 300f, the fourth aircraft seat configuration 400f, the fifth aircraft seat configuration 500f, the seventh aircraft seat configuration 700f, the alternative first aircraft seat configuration 1000f, the alternative third aircraft seat configuration 3000f, the alternative fifth aircraft seat configuration and the alternative seventh aircraft seat configuration 7000f differ in at least one comfort category, wherein the aircraft seat configurations 100f, 300f, 400f, 500f, 700f, 1000f, 3000f, 5000f, 7000f for the at least one comfort category each have a different value, which is achieved by a different arrangement of the aircraft seats 120f, 320f, 420f, 520f, 720f, 1200f, 3200f, 5200f, 7200f and is due to the at least partially different design of the aircraft seat devices 100f, 300f, 400f, 500f, 700f, 1000f, 3000f, 5000f, 7000f.

[0155] In this case, a comfort category is defined as an aircraft seat orientation. A value for the aircraft seat orientation describes an angular deviation of the seat direction from an aircraft longitudinal axis. The value for the aircraft seat configuration is expressed as an angle. The first aircraft seat configuration (100f), the third aircraft seat configuration (300f), the fifth aircraft seat configuration (500f), the seventh aircraft seat configuration (700f), the alternative first aircraft seat configuration (1000f), the alternative third aircraft seat configuration (3000f), the alternative fifth aircraft seat configuration (5000f), and the alternative seventh aircraft seat configuration (7000f) each have the same value for the aircraft seat orientation. The fourth aircraft seat configuration (400f) has a value for the aircraft seat orientation that is greater than the value for the aircraft seat orientation of the first aircraft seat configuration (100f).Another value for the aircraft seat orientation describes whether the seat direction or a directional component of the seat direction is oriented in the direction of flight 24f or against the direction of flight 24f. This additional value is expressed as a "0" or "1" of a Boolean variable. The additional value "0" corresponds to an orientation of the seat direction or a directional component of the seat direction in the direction of flight 24f. The additional value "1" corresponds to an orientation of the seat direction or a directional component of the seat direction against the direction of flight 24f. In the present case, the first aircraft seat 100f, the third aircraft seat 300f, the fifth aircraft seat 500f, and the seventh aircraft seat 700f each have an additional value of "0" for the aircraft seat orientation.The alternative first aircraft seat device 1000f, the alternative third aircraft seat device 3000f, the alternative fifth aircraft seat device 5000f and the alternative seventh aircraft seat device 7000f each have a further value "1" for the aircraft seat orientation.

[0156] The Figure 10Figure 1 shows an aircraft seating arrangement 14g in a seventh embodiment. The aircraft seating arrangement 14g is intended for use in a partially illustrated aircraft cabin 12g. The aircraft cabin 12g has a cabin centerline 16g. The cabin centerline 16g is configured as a longitudinal axis of the aircraft. The aircraft cabin 12g has two opposing cabin exterior walls 18g and 20g. The aircraft has a flight direction 24g in at least one operating state. The aircraft cabin 12g has a cabin section 26g along the cabin centerline 16g. The aircraft cabin 12g has a first cabin aisle 32g and a second cabin aisle 34g in the cabin section 26g. The aircraft seating arrangement 14g includes a first outer seat column 36g. The aircraft seating arrangement 14g includes a first inner seat column 38g.The aircraft seating arrangement 14g includes a second inner seat column of 40g. The aircraft seating arrangement 14g includes a second outer seat column of 42g. The aircraft cabin 12g has a center section of 44g.

[0157] The aircraft seating arrangement 14g comprises several aircraft seating assemblies 100g, 200g, 300g, 400g, 500g, 600g, 700g, and 800g arranged in the aircraft cabin section 26g. These multiple aircraft seating assemblies 100g, 200g, 300g, 400g, 500g, 600g, 700g, and 800g are configured differently from one another. Each aircraft seating assembly 100g, 200g, 300g, 400g, 500g, 600g, 700g, and 800g contains one aircraft seat. The aircraft seat assemblies 100g, 200g, 300g, 400g, 500g, 600g, 700g, and 800g each have a console. The aircraft seat assembly 14g comprises a first aircraft seat assembly 100g and several aircraft seat assemblies 100g, 200g, 300g, 400g, 500g, 600g, 700g, and 800g. The first aircraft seat assembly 100g has a seating direction of 110g. The first aircraft seat assembly 100g has a first aircraft seat 120g. The first aircraft seat assembly 100g has a first console 130g.The aircraft seating arrangement 14g comprises a second aircraft seating device 200g, one of several aircraft seating devices 100g, 200g, 300g, 400g, 500g, 600g, 700g, 800g. The second aircraft seating device 200g has a seating direction 210g. The second aircraft seating device 200g has a second aircraft seat 220g. The second aircraft seating device 200g has a second console 230g. The aircraft seating arrangement 14g comprises a third aircraft seating device 300g, one of several aircraft seating devices 100g, 200g, 300g, 400g, 500g, 600g, 700g, 800g.

[0158] The third aircraft seat assembly (300g) has a seating direction of 310g. The third aircraft seat assembly (300g) has a third aircraft seat (320g). The third aircraft seat assembly (300g) has a third console (330g). The aircraft seat assembly (14g) comprises a fourth aircraft seat assembly (400g) of the following multiple aircraft seat assemblies: 100g, 200g, 300g, 400g, 500g, 600g, 700g, 800g. The fourth aircraft seat assembly (400g) has a seating direction of 410g. The fourth aircraft seat assembly (400g) has a fourth aircraft seat (420g). The fourth aircraft seat assembly (400g) has a fourth console (430g). The aircraft seating arrangement 14g includes a fifth aircraft seat unit 500g, one of several aircraft seat units 100g, 200g, 300g, 400g, 500g, 600g, 700g, 800g. The fifth aircraft seat unit 500g has a seating direction of 510g. The fifth aircraft seat unit 500g has a fifth aircraft seat 520g.The fifth aircraft seat assembly (500g) has a fifth console (530g). The aircraft seat assembly (14g) includes a sixth aircraft seat assembly (600g) of the following multiple aircraft seat assemblies: 100g, 200g, 300g, 400g, 500g, 600g, 700g, 800g. The sixth aircraft seat assembly (600g) has a seat direction of 610g. The sixth aircraft seat assembly (600g) has a sixth aircraft seat (620g). The sixth aircraft seat assembly (600g) has a sixth console (630g). The aircraft seat assembly (14g) includes a seventh aircraft seat assembly (700g) of the following multiple aircraft seat assemblies: 100g, 200g, 300g, 400g, 500g, 600g, 700g, 800g. The seventh aircraft seat assembly (700g) has a seating direction of 710g. The seventh aircraft seat assembly (700g) has a seventh aircraft seat (720g). The seventh aircraft seat assembly (700g) has a seventh console (730g).The aircraft seating arrangement 14g comprises an eighth aircraft seat assembly (800g) of the multiple aircraft seat assemblies (100g, 200g, 300g, 400g, 500g, 600g, 700g, 800g). The eighth aircraft seat assembly (800g) has a seating direction of 810g. The eighth aircraft seat assembly (800g) has an eighth aircraft seat (820g). The eighth aircraft seat assembly (800g) has an eighth console (830g).

[0159] The aircraft seating arrangement 14g comprises at least one further first aircraft seating arrangement 100'g, which is designed at least substantially identically to the first aircraft seating arrangement 100g. The aircraft seating arrangement 14g comprises several further second aircraft seating arrangements 200'g, which are designed at least substantially identically to the second aircraft seating arrangement 200g. The aircraft seating arrangement 14g comprises several further third aircraft seating arrangements 300'g, which are designed at least substantially identically to the third aircraft seating arrangement 300g. The aircraft seating arrangement 14g comprises at least one further fourth aircraft seating arrangement 400'g, which is designed at least substantially identically to the fourth aircraft seating arrangement 400g. The aircraft seating arrangement 14g comprises at least one further fifth aircraft seating arrangement 500'g, which is designed at least substantially identically to the fifth aircraft seating arrangement 500g.Aircraft seating arrangement 14g comprises several further sixth aircraft seating assemblies 600'g, which are at least substantially identical to the sixth aircraft seating assembly 600g. Aircraft seating arrangement 14g comprises several further seventh aircraft seating assemblies 700'g, which are at least substantially identical to the seventh aircraft seating assembly 700g. Aircraft seating arrangement 14g comprises at least one further eighth aircraft seating assembly 800'g, which is at least substantially identical to the eighth aircraft seating assembly 800g.

[0160] In contrast to the first embodiment, the aircraft seating arrangement 14g comprises several alternative aircraft seating arrangements 4000g and 8000g, which are arranged in the aircraft cabin section 26g. The aircraft seating arrangement 14g includes an alternative fourth aircraft seating arrangement 4000g. The alternative fourth aircraft seating arrangement 4000g has a seating direction 4100g. The seating direction 4100g of the alternative fourth aircraft seating arrangement 4000g has a directional component opposite to the direction of flight 24g. The seating direction 4100g of the alternative fourth aircraft seating arrangement 4000g deviates from the direction of flight 24g. In this case, the seating direction 4100g of the alternative fourth aircraft seating arrangement 4000g is angled at 30 degrees to the aircraft cabin center axis 16g. The alternative fourth aircraft seating arrangement 4000g includes an alternative fourth aircraft seat 4200g.The alternative fourth aircraft seat assembly 4000g includes an alternative fourth console 4300g. The alternative fourth aircraft seat assembly 4000g is mirrored about an axis relative to the fourth aircraft seat assembly 400g, the axis being perpendicular to the aircraft cabin centerline 16g and parallel to an aircraft cabin floor 22g of the aircraft cabin 12g. The aircraft seat assembly 14g includes at least one further alternative fourth aircraft seat assembly 4000g, which is at least substantially identical to the alternative fourth aircraft seat assembly 4000g. The aircraft seat assembly 14g includes an alternative eighth aircraft seat assembly 8000g. The alternative eighth aircraft seat assembly 8000g has a seating direction 8100g. The seating direction 8100g of the alternative eighth aircraft seat assembly 8000g has a directional component opposite to the direction of flight 24g.The seating direction 8100g of the alternative eighth aircraft seating arrangement 8000g deviates from the flight direction 24g. The seating direction 8100g of the alternative eighth aircraft seating arrangement 8000g is, in this case, angled at 30 degrees to the aircraft cabin centerline 16g. The alternative eighth aircraft seating arrangement 8000g includes an alternative eighth aircraft seat 8200g. The alternative eighth aircraft seating arrangement 8000g includes an alternative eighth console 8300g. The alternative eighth aircraft seating arrangement 8000g is mirrored about one axis compared to the eighth aircraft seating arrangement 800g, with the axis being perpendicular to the aircraft cabin centerline 16g and parallel to the aircraft cabin floor 22g. The aircraft seating arrangement 14g comprises at least one further alternative eighth aircraft seating arrangement 8000'g, which is designed at least substantially identically to the alternative eighth aircraft seating arrangement 8000g.

[0161] In the present case, the first inner seat gap 38g is symmetrically configured with respect to the second inner seat gap 40g across the aircraft cabin centerline 16g. In the present case, the first outer seat gap 36g is symmetrically configured with respect to the second outer seat gap 42g across the aircraft cabin centerline 16g. Seat directions 4100g, 8100g of some of the multiple aircraft seat assemblies 100g, 200g, 300g, 400g, 500g, 600g, 700g, 800g, 4000g, 8000g are oriented in the aircraft cabin section 26g at least substantially opposite to the flight direction 24g. In the aircraft cabin section 26g, in the present case ten differently designed aircraft seat devices 100g, 200g, 300g, 400g, 500g, 600g, 700g, 800g, 4000g, 8000g are arranged.

[0162] In the aircraft cabin section 26g, four aircraft seat assemblies of the multiple aircraft seat assemblies 100g, 200g, 300g, 400g, 500g, 600g, 700g, 800g, 4000g, 8000g are arranged in the first inner seat gap 38g, namely at least the first aircraft seat assembly 100g, the third aircraft seat assembly 300g, the fourth aircraft seat assembly 400g, and the alternative fourth aircraft seat assembly 4000g. In contrast to the first embodiment, the second aircraft seat assembly 200a from the first embodiment is replaced in the seventh embodiment by the alternative fourth aircraft seat assembly 4000g. The aircraft seat assembly 14g includes at least one additional console 62g. The additional console 62g is located in the first inner seat gap 38g along an aircraft longitudinal axis, between the third aircraft seat device 300g and the alternative fourth aircraft seat device 4000g.The additional console 62g separates the third aircraft seat 300g from the alternative fourth aircraft seat 4000g. The seating directions 310g and 4100g of the aircraft seats 300g and 4000g separated by the additional console 62g are oriented in opposite directions. The aircraft seat arrangement 14g has a first seating group 52g of four aircraft seats arranged directly one behind the other in the first inner seat gap 38g in the aircraft cabin section 26g, namely the first aircraft seat 100g, the alternative fourth aircraft seat 4000g, the third aircraft seat 300g, and the fourth aircraft seat 400g.

[0163] In the second inner seat column 40g of the aircraft cabin section 26g, four aircraft seat assemblies of the several aircraft seat assemblies 100g, 200g, 300g, 400g, 500g, 600g, 700g, 800g, 4000g, 8000g are arranged, namely at least the fifth aircraft seat assembly 500g, the seventh aircraft seat assembly 700g, the eighth aircraft seat assembly 800g and the alternative eighth aircraft seat assembly 8000g. In contrast to the first embodiment, the sixth aircraft seat assembly 600a from the first embodiment is replaced in the seventh embodiment by the alternative eighth aircraft seat assembly 8000g. The aircraft seat assembly 14g includes at least one additional console 64g. The additional console 64g is located in the second inner seat column 40g along an aircraft longitudinal axis, between the seventh aircraft seat 700g and the alternative eighth aircraft seat 8000g.The additional console 64g separates the seventh aircraft seat 700g from the alternative eighth aircraft seat 8000g. The seating directions 710g and 8100g of the aircraft seats 700g and 8000g separated by the additional console 64g are oriented in opposite directions. The aircraft seat arrangement 14g has a second seating group 54g consisting of four aircraft seats arranged directly one behind the other in the second inner seat column 40g in the aircraft cabin section 26g, namely the fifth aircraft seat 500g, the alternative eighth aircraft seat 8000g, the seventh aircraft seat 700g, and the eighth aircraft seat 800g.

[0164] In aircraft cabin section 26g, three differently configured aircraft seat assemblies are arranged in the first outermost seat column 36g: the fifth aircraft seat assembly 500'g, the sixth aircraft seat assembly 600g, and another of the seventh aircraft seat assemblies 700'g. In aircraft cabin section 26g, the sixth aircraft seat assembly 600g, the seventh aircraft seat assembly 700'g, and the fifth aircraft seat assembly 500'g are arranged directly one behind the other in the first outermost seat column 36g. In the first outermost seat column 36g, the fifth aircraft seat assembly 500'g and the sixth aircraft seat assembly 600g are separated from each other by the seventh aircraft seat assembly 700'g. In the aircraft cabin section 26g, viewed in the direction of flight 24g, another of the sixth aircraft seat devices 600'g is arranged immediately behind the sixth aircraft seat device 600g.

[0165] In aircraft cabin section 26g, three differently configured aircraft seat assemblies are arranged in the second outer seat column 42g: the first aircraft seat 100'g, the second aircraft seat 200g, and another of the third aircraft seat assemblies 300'g. In aircraft cabin section 26g, the second aircraft seat 200g, the third aircraft seat 300'g, and the first aircraft seat 100'g are arranged directly one behind the other in the second outer seat column 42g. In the second outer seat column 42g, the first aircraft seat 100'g and the second aircraft seat 200g are separated from each other by the third aircraft seat 300'g. In aircraft cabin section 26g, viewed in the direction of flight 24g, another of the second aircraft seat assemblies 200'g is arranged directly behind the second aircraft seat 200g.

[0166] In aircraft cabin section 26g, the first aircraft seat configuration (100g), the second aircraft seat configuration (200g), the third aircraft seat configuration (300g), the fourth aircraft seat configuration (400g), the fifth aircraft seat configuration (500g), the sixth aircraft seat configuration (600g), the seventh aircraft seat configuration (700g), the eighth aircraft seat configuration (800g), the alternative fourth aircraft seat configuration (4000g), and the alternative eighth aircraft seat configuration (8000g) differ in at least one comfort category, wherein the aircraft seat configurations (100g, 200g, 300g, 400g, 500g, 600g, 700g, 800g, 4000g, 8000g) each have a different value for the at least one comfort category, which is achieved through a different arrangement of the aircraft seats (120g, 220g, 320g, ... 420g, 520g, 620g, 720g, 820g, 4200g, 8200g and, due to the at least partially different design of the aircraft seat fittings, 100g, 200g, 300g, 400g, 500g, 600g, 700g, 800g, 4000g,8000g is conditional.

Claims

1. An aircraft seat arrangement for use in an aircraft cabin of an aircraft, wherein the aircraft cabin comprises at least one seat column and at least one aircraft cabin section, and wherein the aircraft seat arrangement comprises a plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g), which, in an operating state of the aircraft seat arrangement, are arranged in the at least one aircraft cabin section (26a-g) and are designed to be at least partially different from one another and each have an aircraft seat (120a-g, 220a-g, 320a-g, 420a-g, 520a-g, 620a-g, 720a-g, 820a-g, 1200f, 3200f, 4200g, 5200f, 7200f, 8200g) which is designed as a full-flat seat, wherein the aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g) differ in at least one comfort category, wherein the aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g) for the at least one comfort category each have a mutually different value which is caused by a different arrangement of the aircraft seats (120a-g, 220a-g, 320a-g, 420a-g, 520a-g, 620a-g, 720a-g, 820a-g, 1200f, 3200f, 4200g, 5200f, 7200f, 8200g) and by the at least partially different design of the aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g), wherein in the seat column (36a-g, 38a-g, 40a-g, 42a-g) at least four aircraft seat devices of the plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g) are arranged, which differ in design from one another, characterized in that the at least four aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g), in the operating state of the aircraft seat arrangement, are arranged directly one behind another in the seat column, so that they are all cut by a same aircraft longitudinal axis and in each case have a direct access to an aircraft seat aisle (32a-g, 34a-g).

2. The aircraft seat arrangement according to claim 1, characterized in that the at least one comfort category describes a living space, in particular a base area, a bed length, a bed width, a food space volume and / or a passage width in at least one region.

3. The aircraft seat arrangement according to any one of the preceding claims, characterized in that in one seat column (36a-g, 38a-g, 40a-g, 42a-g) in the aircraft cabin section (26a-g) a sitting direction (110a-g, 310a-g, 510a-g, 710a-g, 1100f, 3100f, 5100f, 7100f) of an aircraft seat device (100a-g, 300a-g, 500a-g, 700a-g, 1000f, 3000f, 5000f, 7000f) of the plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g) is arranged at least substantially parallel to an aircraft longitudinal axis, and a sitting direction (210a-g, 410a-g, 610a-g, 810a-g, 4100g, 8100g) of a further aircraft seat device (200a-g, 400a-g, 600a-g, 800a-g, 4000g, 8000g) of the plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g), is arranged angled with respect to the aircraft longitudinal axis, in particular at an angle of at least 18 degrees.

4. The aircraft seat arrangement according to any one of the preceding claims, characterized in that in the aircraft cabin section (26a-g), a sitting direction (210a-g, 610a-g) of at least one aircraft seat device (200a-g, 600a-g) of the plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g) is directed away from a directly adjacent aircraft cabin aisle (32a-g, 34a-g).

5. The aircraft seat arrangement according to any one of the preceding claims, characterized in that in the aircraft cabin section (26a-g), a sitting direction (410a-g, 810a-g, 4100g, 8100g) of at least one aircraft seat device (400a-g, 800a-g, 4000g, 8000g) of the plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g) is directed toward a directly adjacent aircraft cabin aisle (32a-g, 34a-g).

6. The aircraft seat arrangement according to claims 4 and 5, characterized in that the sitting directions (210a-g, 410a-g, 610a-g, 810a-g, 4100g, 8100g) of at least two aircraft seat devices (200a-g, 400a-g, 600a-g, 800a-g, 4000g, 8000g) which are in particular spaced apart from one another by at least one further aircraft seat device (300a-g, 700a-g) are arranged in one seat column (36a-g, 38a-g, 40a-g, 42a-g) in a manner angled with respect to an aircraft longitudinal axis by at least substantially the same angle in terms of value, wherein the sitting directions (210a-g, 410a-g, 610a-g, 810a-g, 4100g, 8100g) of the aircraft seat devices (200a-g, 400a-g, 600a-g, 800a-g, 4000g, 8000g) are formed in mirror image to an aircraft longitudinal axis.

7. The aircraft seat arrangement according to any one of the preceding claims, characterized in that an aircraft seat (120a-g, 220a-g, 520a-g, 620a-g, 1200f, 5200f) of an aircraft seat device (100a-g, 200a-g, 500a-g, 600a-g, 1000f, 5000f) of the aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g) which are arranged in one seat column (36a-g, 38a-g, 40a-g, 42a-g) in the aircraft cabin section (26a-g) is arranged on an aisle side, wherein an aircraft seat (320a-g, 420a-g, 720a-g, 820a-g, 3200f, 4200g, 7200f, 8200g) of a further aircraft seat device (300a-g, 400a-g, 700a-g, 800a-g, 3000f, 4000g, 7000f, 8000g) of the aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g) which are arranged in the seat column (36a-g, 38a-g, 40a-g, 42a-g) is arranged facing away from the aisle.

8. The aircraft seat arrangement according to any one of the preceding claims, characterized by at least one seat grouping (52a-g, 54a-g) of at least four aircraft seat devices of the plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 4000g, 4000'g, 8000g, 8000'g), which aircraft seat devices are arranged directly one behind another in one seat column (36a-g, 38a-g, 40a-g, 42a-g) in the aircraft cabin section (26a-g) and each have different sitting directions (110a-g, 210a-g, 310a-g, 410a-g, 510a-g, 610a-g, 710a-g, 810a-g, 4100g, 8100g) and / or whose aircraft seats (120a-g, 220a-g, 320a-g, 420a-g, 520a-g, 620a-g, 720a-g, 820a-g, 4200g, 8200g) are arranged on an aisle side or facing away from the aisle.

9. The aircraft seat arrangement according to claim 8, characterized in that the sitting directions (110a-d, 210a-d, 310a-d, 410a, 510a-d, 610a-d, 710a-d, 810a, 4100g, 8100g) of the aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 4000g, 4000'g, 8000g, 8000'g) arranged directly one behind another within the at least one seat grouping (52a-g, 54a-g) are arranged in an alternating manner at least substantially parallel to and in an angled manner with respect to the aircraft longitudinal axis.

10. The aircraft seat arrangement according to any one of the preceding claims, characterized in that in one seat column (36a, 38a, 40a, 42a) in the aircraft cabin section (26a), two aircraft seat devices (100a, 200a, 500a, 600a) of the plurality of aircraft seat devices (100a, 100'a, 200a, 200'a, 300a, 300'a, 400a, 400'a, 500a, 500'a, 600a, 600'a, 700a, 700'a-g, 800a, 800'a) each have an aircraft seat (120a, 220a, 520a, 620a) which is arranged on an aisle side, and two further aircraft seat devices (300a, 400a, 700a, 800a) of the plurality of aircraft seat devices (100a, 100'a, 200a, 200'a, 300a, 300'a, 400a, 400'a, 500a, 500'a, 600a, 600'a, 700a, 700'a, 800a, 800'a), which, as viewed in a flight direction (24a), are arranged directly behind or in front of the two aircraft seat devices (300a, 400a, 700a, 800a) each have an aircraft seat (320a, 420a, 720a, 820a) which is arranged facing away from the aisle.

11. The aircraft seat arrangement according to any one of the preceding claims, characterized in that in one seat column (36a-g, 38a-g, 40a-g, 42a-g) in the aircraft cabin section (26a) at least three aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 4000g, 4000'g, 8000g, 8000'g) of the plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g) are arranged, wherein a sitting direction (110a-g, 310a-g, 510a-g, 710a-g) of an aircraft seat device (100a-g, 100'a-g, 300a-g, 300'a-g, 500a-g, 500'a-g, 700a-g, 700'a-g) of the at least three aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 4000g, 4000'g, 8000g, 8000'g) is arranged at least substantially parallel to an aircraft longitudinal axis, and sitting directions (210a-g, 410a-g, 610a-g, 810a-g, 4100g, 8100g) of two further aircraft seat devices (200a-g, 200'a-g, 400a-g, 400'a-g, 600a-g, 600'a-g, 800a-g, 800'a-g, 4000g, 4000'g, 8000g, 8000'g) of the at least three aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 4000g, 4000'g, 8000g, 8000'g) are arranged in an angled manner with respect to the aircraft longitudinal axis.

12. The aircraft seat arrangement according to claim 11, characterized in that aircraft seats (220a-g, 420a-g, 620a-g, 820a-g, 4200g, 8200g) of the aircraft seat devices (200a-g, 200'a-g, 400a-g, 400'a-g, 600a-g, 600'a-g, 800a-g, 800'a-g, 4000g, 4000'g, 8000g, 8000'g), the sitting directions (210a-g, 410a-g, 610a-g, 810a-g, 4100g, 8100g) of which are arranged in an angled manner with respect to the aircraft longitudinal axis, have different distances from an aircraft cabin aisle (32a-g, 34a-g).

13. The aircraft seat arrangement according to any one of the preceding claims, characterized in that in at least one seat column (36a, 38a, 40a, 42a) in the aircraft cabin section (26a), four aircraft seat devices (100a, 100'a, 200a, 200'a, 300a, 300'a, 400a, 400'a, 500a, 500'a, 600a, 600'a, 700a, 700'a, 800a, 800'a) of the plurality of aircraft seat devices (100a, 100'a, 200a, 200'a, 300a, 300'a, 400a, 400'a, 500a, 500'a, 600a, 600'a, 700a, 700'a, 800a, 800'a) which differ from one another, are arranged directly one behind another, wherein sitting directions (110a, 310a, 510a, 710a) of two aircraft seat devices (100a, 100'a, 300a, 300'a, 500a, 500'a, 700a, 700'a) of the four aircraft seat devices (100a, 100'a, 200a, 200'a, 300a, 300'a, 400a, 400'a, 500a, 500'a, 600a, 600'a, 700a, 700'a, 800a, 800'a) are arranged at least substantially parallel to an aircraft longitudinal axis, wherein one aircraft seat (120a, 520a) of one aircraft seat device (100a, 100'a, 500a, 500'a) of the two aircraft seat devices (100a, 100'a, 300a, 300'a, 500a, 500'a, 700a, 700'a) is arranged on an aisle side and a further aircraft seat (320a, 720a) of a further aircraft seat device (300a, 300'a, 700a, 700'a) of the two aircraft seat devices (100a, 100'a, 300a, 300'a, 500a, 500'a, 700a, 700'a) is arranged facing away from the aisle, and sitting directions (210a, 410a, 610a, 810a) of two further aircraft seat devices (200a, 200'a, 400a, 400'a, 600a, 600'a, 800a, 800'a) of the four aircraft seat devices (100a, 100'a, 200a, 200'a, 300a, 300'a, 400a, 400'a, 500a, 500'a, 600a, 600'a, 700a, 700'a, 800a, 800'a) are arranged in an angled manner with respect to the aircraft longitudinal axis, wherein one aircraft seat (220a, 620a) of one aircraft seat device (200a, 200'a, 600a, 600'a) of the two further aircraft seat devices (200a, 200'a, 400a, 400'a, 600a, 600'a, 800a, 800'a) is arranged on the aisle side and a further aircraft seat (420a, 820a) of a further aircraft seat device (400a, 400'a, 800a, 800'a) of the two further aircraft seat devices (200a, 200'a, 400a, 400'a, 600a, 600'a, 800a, 800'a) is arranged facing away from the aisle.

14. The aircraft seat arrangement according to any one of the preceding claims, characterized in that in the aircraft cabin section (26a-g), two aircraft seat devices (300a-g, 700a-g) of the plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g) form a pair of seats (46a-g) in two seat columns (38a-g, 40a-g) which are arranged directly next to each other, wherein sitting directions (310a-g, 710a-g) of the two aircraft seat devices (300a-g, 700a-g) are arranged at least substantially parallel to an aircraft longitudinal aixis, and aircraft seats (320a-g, 720a-g) of the two aircraft seat devices (300a-g, 700a-g) are arranged facing away from an aisle, wherein at least two of the pairs of seats (46a-g) are arranged in the two seat columns (38a-g, 40a-g) which are arranged directly next to each other.

15. The aircraft seat arrangement according to any one of the preceding claims, characterized in that an arrangement of aircraft seat devices (100e-f, 100'f, 200e, 200'e, 300e-f, 300'e-f, 400f, 400'f, 500e-f, 500'f, 600e, 600'e, 700e-f, 700'e-f, 800e) of the plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 5000f, 5000'f, 7000f, 7000'f) in the aircraft cabin section (26e-f) in at least one seat column (36e-f, 38e-f) on a first aircraft cabin side (56e-f) is formed asymmetrically to an arrangement of aircraft seat devices (100e-f, 100'f, 200e, 200'e, 300e-f, 300'e-f, 400f, 400'f, 500e-f, 500'f, 600e, 600'e, 700e-f, 700'e-f, 800e) of the plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 5000f, 5000'f, 7000f, 7000'f) in at least one seat column (40e-f, 42e-f) on a second aircraft cabin side (58e-f), wherein the first aircraft cabin side (56e-f) is separated from the second aircraft cabin side (58e-f) by an imaginary aircraft cabin center plane which is oriented along an aircraft longitudinal axis perpendicular to an aircraft cabin floor (22e-f).

16. The aircraft seat arrangement according to claim 15, characterized in that in at least one seat column (36e, 38e; 42f), only such aircraft seat devices (200e, 400e-f, 800e) of the plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 5000f, 5000'f, 7000f, 7000'f) are arranged whose sitting directions (210e, 410e-f, 810e) are arranged in an angled manner with respect to the aircraft longitudinal axis.

17. The aircraft seat arrangement according to claim 15 or 16, characterized in that in at least one seat column (36f, 38f, 40e-f, 42e), only such aircraft seat devices (100e-f, 100'e-f, 300e-f, 300'e-f, 500e-f, 500'e-f, 700e-f, 700'e-f, 1000f, 1000'f, 3000f, 3000'f, 5000f, 5000'f, 7000f, 7000'f) of the plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 5000f, 5000'f, 7000f, 7000'f) are arranged whose sitting directions (110e-f, 310e-f, 510e-f, 710e-f, 1100f, 3100f, 5100f, 7100f) are arranged at least substantially parallel to the aircraft longitudinal axis.

18. The aircraft seat arrangement according to any one of the preceding claims, characterized in that sitting directions (1100f, 3100f, 4100g, 5100f, 7100f, 8100g) of some of the plurality of aircraft seat devices (100a-g, 100'a-g, 200a-g, 200'a-g, 300a-g, 300'a-g, 400a-g, 400'a-g, 500a-g, 500'a-g, 600a-g, 600'a-g, 700a-g, 700'a-g, 800a-g, 800'a-g, 1000f, 3000f, 3000'f, 4000g, 4000'g, 5000f, 5000'f, 7000f, 7000'f, 8000g, 8000'g) in the aircraft cabin section (26f-g) are oriented at least substantially in an opposite direction to a flying direction (24f-g).