Aircraft seat device

Abstract

Aircraft seat device (10e) with at least one seat (12e), with at least one console (26e) which is arranged at least substantially laterally next to the at least one seat (12e) and has at least one upper side (94e) which is horizontally oriented and forms an upper surface of the console (26e), and with at least one table unit (34e) which has at least one table element (38e) and at least one guide unit (48e), wherein the at least one guide unit (48e) is provided for at least substantially horizontal guidance of the at least one table element (38e) between a retracted state of the at least one table unit (34e) and an extended state of the at least one table unit (34e) and has at least one holding arm (50e) which is pivotably connected to the at least one console (26e) and movably connected to the at least one table element (38e), characterized inthat the table element (38e) in the retracted state rests completely on the upper side (94e) of the console (26e).

Description

Prior ArtThe invention relates to an aircraft seat device according to the preamble of claim 1.An aircraft seat device having at least one seat, having at least one bracket which is arranged laterally next to the at least one seat, and having at least one table unit has already been proposed.The publication EP 3 617 070 A1 discloses an aircraft seat device having at least one seat, having at least one console which is arranged at least substantially laterally next to the at least one seat, and having at least one table unit which has at least one table element and at least one guide unit, wherein the at least one guide unit is provided for at least substantially horizontal guidance of the at least one table element between a retracted state of the at least one table unit and an extended state of the at least one table unit and has at least one holding arm which is pivotably connected to the at least one console and movably connected to the at least one table element.The document US 2018 / 0 305 023 A1 discloses an aircraft seat device having at least one seat, having at least one console which is arranged at least substantially laterally next to the at least one seat, and having at least one table unit which has at least one table element and at least one guide unit, wherein the at least one guide unit is provided for at least substantially horizontal guidance of the at least one table element between a retracted state of the at least one table unit and an extended state of the at least one table unit and has at least one holding arm which is pivotably connected to the at least one console and movably connected to the at least one table element.The publication US 2013 / 0 248 653 A1 discloses an aircraft seat device having at least one seat, having at least one console, and having at least one table unit which has at least one table element and at least one guide unit, wherein the at least one guide unit is provided for at least substantially horizontal guidance of the at least one table element between a retracted state of the at least one table unit and an extended state of the at least one table unit and has at least one holding arm which is pivotably connected to the at least one console and movably connected to the at least one table element.The publication DE 43 43 242 A1 discloses an aircraft seat device having at least one seat, and having at least one table unit which has at least one table element and at least one guide unit, wherein the at least one guide unit is provided for at least substantially horizontal guidance of the at least one table element and has at least one holding arm which is pivotably connected to a backrest and movably connected to the at least one table element.FR 2 911 548 A1 discloses a seat device for a motor vehicle having a table unit integrated into a foldable backrest, which can be used in the folded state of the backrest and is pivotably connected to the backrest for this purpose.The publication US 2009 / 0 058 152 A1 discloses a seat device for a motor vehicle having a table unit integrated into a foldable backrest, which can be used in the folded state of the backrest and is pivotably connected to the backrest for this purpose.The publication US 2009 / 0 266 954 A1 discloses a seat device, in particular an office chair, to the armrest of which a table unit can be pivotably fastened.The object of the invention is in particular to provide a device of the generic type having improved properties with regard to passenger comfort and operating safety. The object is achieved according to the invention by the features of claim 1 and of secondary claims 7 and 8, while advantageous embodiments and developments of the invention can be gathered from the dependent claims.Advantages of the InventionThe invention is based on an aircraft seat device having at least one seat, having at least one console which is arranged at least substantially laterally next to the at least one seat and has at least one upper side which is aligned horizontally and forms an upper surface of the console, and having at least one table unit which has at least one table element and at least one guide unit, wherein the at least one guide unit is provided for at least substantially horizontal guidance of the at least one table element between a retracted state of the at least one table unit and an extended state of the at least one table unit and has at least one holding arm which is pivotably connected to the at least one console and movably connected to the at least one table element.It is proposed that the table element in the retracted state lies completely on the upper side of the console. The configuration according to the invention makes it possible to provide an advantageously storable table unit. As a result, an aircraft seat device with an advantageously compact construction can be made possible. The configuration according to the invention makes it possible to provide a table device which can be operated advantageously comfortably. The aircraft seat device is preferably provided for being mounted in an aircraft cabin of an aircraft, in particular on a cabin floor of the aircraft cabin. Preferably, the aircraft comprises the aircraft seat device. "Provided" is to be understood in particular as specially designed and / or equipped. The fact that an object is provided for a specific function is to be understood in particular to mean that the object fulfills and / or executes this specific function in at least one application state and / or operating state. The aircraft seat device preferably has at least one cladding, in particular at least one shell element. Preferably, the at least one cladding is connected to the at least one bracket. The at least one cladding is provided in particular for optically separating the at least one seat. Preferably, the at least one seat comprises a seat bottom and a backrest. The at least one seat preferably has at least one leg rest. The at least one seat preferably has at least one headrest. In principle, the at least one seat can also comprise at least one armrest and / or at least one footrest. Preferably, the at least one seat has a seat direction. A "seat direction" is to be understood in particular as a direction which is oriented at least substantially parallel to the cabin floor, in particular with a deviation of 3 degrees from the cabin floor, and at least substantially perpendicular to a theoretical, planar backrest oriented perpendicular to the cabin floor, wherein the direction corresponds to a normal on a front side of the backrest, wherein the front side of the backrest forms a supporting surface for a back of a passenger in a usual seat position.In principle, in connection with the present description, "at least substantially" is to be understood in particular as meaning that a deviation from a predefined value is in particular less than 25%, preferably less than 10% and particularly preferably less than 5% of the predefined value. Preferably, the at least one seat is arranged on the cabin floor, wherein the seat direction is oriented at an angle in the amount greater than zero to a flight direction of the aircraft. The angle is preferably in particular at least 10 degrees, preferably at least 20 degrees and particularly preferably at least 30 degrees. In principle, angles deviating therefrom are also conceivable. Alternatively, the seat direction can also be oriented parallel to the flight direction. Preferably, the at least one console is arranged laterally next to the at least one seat, as viewed along the seat direction. Preferably, an imaginary plane running perpendicular to the seat direction intersects at least the seat bottom, in particular in a TTL position of the at least one seat, and the at least one bracket. A "TTL position" is to be understood here in particular as an upright position of the at least one seat, which must be assumed for safety reasons, in particular in a starting phase, in a rolling phase, in a landing phase and during turbulences. In this case, the backrest and the seat bottom are substantially perpendicular to one another in the TTL position, preferably at an angle between 100 degrees and 130 degrees. Preferably, the at least one console has a trapezoidal base surface. In principle, the at least one bracket can also have a triangular or rectangular base surface. The at least one holding arm is preferably provided to transmit a force acting on the at least one table unit, in particular a weight force of the at least one table unit and / or a supporting force, into the at least one console. The at least one holding arm is preferably manufactured from a metallic material and / or from a fiber composite material. Particularly preferably, the at least one holding arm is pivotably connected to the at least one table element. The at least one guide unit preferably has at least two bearing points. A first bearing point of the at least one guide unit is provided in particular for connecting the at least one holding arm to the at least one bracket. Preferably, the first bearing point is arranged on the console or in the stowage space of the at least one console. A second bearing point of the at least one guide unit is provided in particular for the purpose of connecting the at least one holding arm to the at least one table element. Preferably, the second bearing point is arranged on or in the at least one table element. The second bearing point is preferably designed as a pivot bearing. The at least one table element is preferably designed as a plate. The at least one table element preferably forms a storage surface of the at least one table unit. Preferably, the storage surface in the extended state of the at least one table unit is arranged on a side of the at least one table element facing away from the cabin floor. Preferably, the storage surface in the extended state is arranged at least substantially parallel, in particular at an angle of 3 degrees, to the cabin floor. In principle, the at least one guide unit can have at least one rotary joint. The at least one pivot joint is provided for an angle adaptation of the at least one table element, in particular by 3 degrees, between the retracted state and the extended state. In principle, it would also be conceivable for the at least one console to have a geometry which is related to the cabin floor and is angled in particular by 3 degrees, in order in particular to ensure an at least substantially parallel alignment of the at least one table unit with respect to the at least one console.In an embodiment no longer according to the invention, it is proposed that the at least one console has at least one stowage space which is provided at least for at least substantially completely receiving the at least one table unit in an at least substantially horizontal position in the retracted state. By means of this configuration, passenger comfort and operating safety can be advantageously increased, since the at least one table device can be accommodated at least substantially completely in the stowage space. As a result, the at least one table unit can advantageously be stowed in the at least one console. Passenger comfort can be advantageously improved by this configuration, since the at least one table unit is not perceptible, in particular not perceptible, to a passenger when not in use. By "at least substantially completely" is to be understood in particular that a volume spanned by the at least one table unit in the retracted state is arranged in the at least one stowage space in particular to an extent of at least 80%, preferably to an extent of at least 90% and particularly preferably to an extent of at least 99%. Preferably, the storage surface formed by the at least one table element is completely covered by the at least one console in the retracted state. Preferably, the at least one stowage space is arranged within the at least one console. Preferably, the at least one console surrounds the at least one stowage space at least substantially completely. Preferably, the at least substantially horizontal position refers to an at least substantially horizontal orientation of the at least one table element.It is furthermore proposed that the at least one guide unit has at least one further holding arm. This configuration advantageously enables the at least one table unit to be mounted reliably. This configuration advantageously allows a guided movement of the at least one table unit to be realized by means of the at least one holding arm and the at least one further holding arm. The at least one further holding arm is preferably provided to transmit a force acting on the at least one table unit, in particular a weight force of the at least one table unit and / or a supporting force, into the at least one console. The at least one further holding arm is preferably manufactured from a metallic material and / or from a fiber composite material. Particularly preferably, the at least one further holding arm is pivotably connected to the at least one table element. The at least one guide unit preferably has at least two further bearing points. A third bearing point of the at least one guide unit is provided in particular for the purpose of connecting the at least one further holding arm to the at least one bracket. Preferably, the third bearing point is arranged on the console or in the stowage space of the at least one console. A fourth bearing point of the at least one guide unit is provided in particular for the purpose of connecting the at least one further holding arm to the at least one table element. Preferably, the fourth bearing point is arranged on or in the at least one table element. The fourth bearing point is preferably designed as a pivot bearing.In an embodiment that is no longer according to the invention, it is proposed that the at least one holding arm, in the retracted state and / or in the extended state of the at least one table unit, serves at least partially as a closure element for an opening of the at least one console to the at least one stowage space. As a result of this configuration, the at least one bracket advantageously has a closed surface. This configuration advantageously prevents a person from being able to grasp into the stowage space and / or foreign bodies from being able to pass into the stowage space by means of the closure element in the retracted state and / or the extended state. This advantageously reduces a risk of finger jamming. In this context, an "opening" is to be understood to mean, in particular, a cutout on an outer surface of the at least one console, which cutout allows access to the at least one stowage space from outside the at least one console. A "closure element" is to be understood in particular as an element which at least optically closes the opening of the at least one console. Preferably, the closure element in the retracted state and / or in the extended state is provided to close the opening of the at least one console, at least to a substantial extent, i.e. to a percentage in particular greater than 30%, preferably greater than 50% and particularly preferably greater than 75%. Preferably, the opening has an opening portion. The at least one holding arm, the at least one further holding arm and / or the at least one table element are preferably arranged at least partially in the opening region in the retracted state and the extended state. The opening preferably has a base surface which is arranged in particular parallel to the outer surface of the at least one bracket. Preferably, a distance of a plane, which is arranged in particular in a surface of the at least one table element facing the at least one seat and is oriented perpendicular to the cabin floor, from the outer surface of the at least one console is at most 2 cm. In principle, the at least one table element can have at least one region in which the at least one table element protrudes from the opening in the retracted state. In this case, the at least one region is preferably arranged at a corner of the at least one table element. Preferably, in the retracted state, an area of the at least one table element protrudes from the opening that is at most 10% of the placement area. "Closing" is to be understood in particular to mean that the at least one holding arm, the at least one further holding arm and / or the at least one table element reduce a surface of the base surface of the opening that can be freely mechanically penetrated, wherein the base surface is covered in particular by at least 90% of the at least one holding arm, the at least one further holding arm and / or the at least one table element. Furthermore, "closing" is to be understood in particular to mean that the at least one holding arm, the at least one further holding arm and / or the at least one table element are provided to prevent a penetration of the opening, in particular of the opening region of the opening, by means of a finger of a person.In an embodiment that is no longer according to the invention, it is proposed that the at least one further holding arm, in the retracted state and / or in the extended state of the at least one table unit, serves at least partially as a further closure element for the opening of the at least one console to the at least one stowage space. As a result of this configuration, the at least one bracket advantageously has a closed surface. This configuration advantageously prevents a person from being able to grasp into the stowage space and / or foreign bodies from being able to pass into the stowage space by means of the closure element in the retracted state and / or the extended state. This advantageously reduces a risk of finger jamming. Preferably, the further closure element is provided in the retracted state and / or in the extended state to close the opening of the at least one console, at least to a substantial extent, i.e. to a percentage in particular greater than 30%, in particular preferably greater than 50% and particularly preferably greater than 75%.In an embodiment no longer according to the invention, it is proposed that the opening of the at least one console to the at least one stowage space is closed in each case at least 90% in the retracted state and in the extended state of the at least one table unit. This configuration advantageously reduces a risk of finger jamming. This advantageously prevents foreign bodies and dirt from entering. Operating reliability can thereby be advantageously increased. Preferably, the opening of the at least one console to the at least one stowage space is closed in each case to an extent of at least 95% in the retracted state and in the extended state of the at least one table unit. Particularly preferably, the opening of the at least one console to the at least one stowage space is in each case completely closed in the retracted state and in the extended state of the at least one table unit. Particularly preferably, the opening of the at least one bracket is closed without any gaps by the at least one holding arm. Particularly preferably, the opening of the at least one bracket is closed without any gaps by the at least one holding arm and the at least one further holding arm. By "gap-free" is to be understood in particular that a distance, in particular a distance of an opening contour of the opening from the at least one holding arm, from the at least one further holding arm and / or from the at least one table element, is at least for the most part along the opening contour preferably less than 5 mm and particularly preferably less than 3 mm. The opening contour is preferably formed by the at least one bracket or the opening contour is formed by an opening cladding of the at least one bracket. Particularly preferably, the at least one holding arm, the at least one further holding arm and the at least one table element are provided in the retracted state and / or in the extended state to close the opening of the at least one console, in particular the base area of the opening of the at least one console, at least to 90%. The at least one table unit preferably has at least one additional closure element. The at least one additional closure element is designed in particular as a flexible seal, in particular as a flexible sealing lip. The at least one additional closure element is preferably arranged in the at least one bracket, in particular in the opening region. Preferably, the at least one additional closure element is arranged above and / or below the at least one table element. The at least one additional closure element is provided in particular for closing the distance of the opening contour of the opening from the at least one holding arm, from the at least one further holding arm and / or from the at least one table element, at least to a large extent along the opening contour.In an embodiment no longer according to the invention, it is proposed that the at least one holding arm is mounted pivotably in a front region of the at least one bracket and the at least one further holding arm is mounted pivotably in a rear region of the at least one bracket. This embodiment advantageously enables an S-shaped movement of the at least one table unit between the retracted state and the extended state. A "front region" is to be understood in particular as a region which is arranged at a front end of the at least one console, wherein the front region extends from the front end counter to the seat direction in particular over at most 20%, preferably over at most 25%, and particularly preferably over at most one third of a length of the at least one console. Preferably, the length of the at least one console is measured parallel to the seat direction. A "rear region" is to be understood in particular as a region which is arranged at a rear end of the at least one console, wherein the rear region extends from the rear end in the seat direction in particular over at most 20%, preferably over at most 25%, and particularly preferably over at most one third of the length of the at least one console. Preferably, the front end of the at least one console is arranged in front of the rear end of the at least one console, as viewed counter to the seat direction. Preferably, a theoretical plane oriented perpendicular to the seat direction first intersects the front region and then the rear region when the theoretical plane is moved counter to the seat direction. Preferably, the at least one holding arm is pivotably mounted via the first bearing point of the at least one guide unit in the front region of the at least one bracket. Preferably, the at least one further holding arm is pivotably mounted via the third bearing point of the at least one guide unit in the rear region of the at least one bracket. The first bearing point is preferably designed as a pivot bearing. The third bearing point is preferably designed as a pivot bearing. Preferably, the at least one table element and the at least one holding arm are arranged at least partially overlapping with one another in the retracted state and in the extended state. The at least one holding arm preferably has at least one overlap region with a reduced component height of the at least one holding arm. A "component height" is to be understood in particular as an extension perpendicular to the placement surface, which describes a dimension of the at least one holding arm, of the at least one further holding arm or of the at least one table element. The at least one table element preferably has at least one overlap region corresponding to the at least one overlap region of the at least one holding arm and having a reduced component height of the at least one table element. Preferably, the at least one overlap region of the at least one holding arm and the at least one corresponding overlap region of the at least one table element at least partially overlap in the retracted state and in the extended state. Particularly preferably, an imaginary line perpendicular to the storage surface, in particular the imaginary line perpendicular to the storage surface and through the second bearing point intersects the at least one overlap region of the at least one holding arm and the at least one corresponding overlap region of the at least one table element. Particularly preferably, the at least one holding arm and the at least one table element form an at least substantially constant overall component height in the at least one overlap region of the at least one holding arm and in the at least one corresponding overlap region of the at least one table element, which overall component height corresponds in particular to a largest component height of the at least one table element. Preferably, the at least one table element and the at least one further holding arm are arranged at least partially overlapping with one another in the retracted state and in the extended state. The at least one further holding arm preferably has at least one further overlap region with a further reduced component height of the at least one further holding arm. The at least one table element preferably has at least one overlap region, which corresponds further to the at least one further overlap region of the at least one further holding arm, with a further reduced component height of the at least one table element. Preferably, the at least one further overlap region of the at least one further holding arm and the at least one further corresponding overlap region of the at least one table element overlap at least partially in the retracted state and in the extended state. Particularly preferably, a further imaginary line perpendicular to the storage surface, in particular the further imaginary line perpendicular to the storage surface and through the fourth bearing point intersects the at least one further overlap region of the at least one further holding arm and the at least one further corresponding overlap region of the at least one table element. Particularly preferably, the at least one further holding arm and the at least one table element form the at least substantially constant overall component height in the at least one further overlap region of the at least one further holding arm and in the at least one further corresponding overlap region of the at least one table element, which overall component height corresponds in particular to the largest component height of the at least one table element.In an embodiment no longer according to the invention, it is proposed that the at least one holding arm and the at least one further holding arm are pivotably mounted in a front region of the at least one bracket. This configuration advantageously enables an arcuate movement of the at least one table unit between the retracted state and the extended state. Preferably, the at least one holding arm is pivotably mounted via the first bearing point of the at least one guide unit in the front region of the at least one bracket. Preferably, the at least one further holding arm is pivotably mounted via the third bearing point of the at least one guide unit in the front region of the at least one bracket.In an embodiment no longer according to the invention, it is proposed that the at least one holding arm and the at least one further holding arm are pivotably mounted in a rear region of the at least one bracket. This configuration advantageously enables an arcuate movement of the at least one table unit between the retracted state and the extended state. Preferably, the at least one holding arm is pivotably mounted via the first bearing point of the at least one guide unit in the rear region of the at least one bracket. Preferably, the at least one further holding arm is pivotably mounted via the third bearing point of the at least one guide unit in the rear region of the at least one bracket.In an embodiment no longer according to the invention, it is proposed that the at least one guide unit comprises at least one rail element which is provided for translatory guidance of the at least one table element. This configuration advantageously enables an arcuate movement of the at least one table unit between the retracted state and the extended state. Preferably, the at least one holding arm is pivotably mounted via the first bearing point of the at least one guide unit in the front region of the at least one bracket. Preferably, the at least one rail element is arranged in or on the at least one bracket. Preferably, the at least one rail element is arranged at least substantially parallel to the seat direction. Preferably, the at least one rail element extends from the rear region of the at least one bracket to a central region of the at least one bracket. Preferably, the central region extends in particular over at most 60%, preferably over at most 50% and particularly preferably over at most one third of the length of the at least one bracket. The central region is arranged in particular between the rear region and the front region. A third bearing point of the at least one guide unit is provided in particular for the purpose of connecting the at least one rail element to the at least one table element. Preferably, the third bearing point is arranged on the console or in the stowage space of the at least one console. The third bearing point is preferably designed as a pivot bearing which is designed to correspond to the at least one rail element. The at least one guide unit preferably has at least one closure element. The closure element is preferably designed as a brush or as a seal. The seal is preferably designed as a flexible sealing lip. Preferably, the at least one closure element is arranged on the at least one rail element, on the at least one console and / or in the at least one console.It is also proposed that the at least one holding arm has at least two arm elements which are pivotably connected to one another. As a result, an overall length of the at least one holding arm can advantageously be divided into a plurality of partial lengths. This allows an advantageously compact design of the at least one guide unit. Preferably, the at least one holding arm comprises a first arm element and a second arm element. Particularly preferably, the first arm element and the second arm element are pivotably connected to one another. Preferably, the at least one holding arm has a pivot bearing via which the first arm element and the second arm element are pivotably connected to one another. Preferably, the first arm element is connected to the at least one bracket via the first bearing point. The second arm element is preferably connected to the at least one table element via the second bearing point. Preferably, the at least one further holding arm has at least two further arm elements which are pivotably connected to one another. Preferably, the at least one further holding arm has a first further arm element and a second further arm element. Particularly preferably, the first further arm element and the second further arm element are pivotably connected to one another. Preferably, the at least one further holding arm has a further pivot bearing via which the first further arm element and the second further arm element are pivotably connected to one another. Preferably, the first further arm element is connected to the at least one bracket via the third bearing point. The second further arm element is preferably connected to the at least one table element via the fourth bearing point. Particularly preferably, the at least one guide unit has at least one cover element. The at least one cover element is provided in particular to cover the at least one holding arm and the at least one further holding arm at least partially, preferably in each case to an extent of at least 30% of a volume of the at least one holding arm and of the at least one further holding arm. This advantageously reduces the risk of finger jamming. By "covering" is to be understood in particular that the at least one holding arm and the at least one further holding arm are at least substantially completely covered from above and from at least three sides. Preferably, in an assembled state of the at least one table unit, a person cannot grasp under the at least one cover element in any operating state. Preferably, the at least one cover element is connected to the at least one holding arm or the at least one further holding arm. Particularly preferably, the at least one cover element is formed integrally with the at least one holding arm or the at least one further holding arm. Preferably, the at least one table element is provided, at least in the retracted state, for completely covering the at least one guide unit.It is furthermore proposed that the at least one guide unit has at least one coupling point via which the at least one holding arm is pivotably connected to the at least one further holding arm. As a result, a guide unit having an advantageously defined guide track for guiding the at least one table element can be provided. In this way, in particular a guide unit with a scissors mechanism can be made possible. The at least one coupling point is preferably designed as a pivot bearing. The at least one coupling point is provided in particular for presetting a defined movement path of the at least one table element between the retracted state and the extended state. Preferably, the first arm element or the second arm element of the at least one holding arm has at least one extension which is provided for coupling to the at least one further holding arm. Preferably, the at least one extension forms the at least one coupling point. Preferably, the first further arm element or the second further arm element has at least one extension corresponding to the at least one extension or at least one recess corresponding to the at least one extension.According to the invention, it is proposed that the at least one table element in the retracted state rests at least substantially completely on an upper side of the at least one console. An advantageously compact construction can thereby be achieved. This configuration advantageously allows a risk of finger jamming to be minimized. The upper side preferably forms an upper surface of the at least one bracket. Preferably, the top side is oriented at least substantially horizontally. Preferably, the top side is arranged at least substantially parallel to the cabin floor. Preferably, the upper side of the at least one console is spaced apart from the cabin floor in particular by at most 100 cm and preferably by at most 90 cm. Particularly preferably, the at least one table element is arranged on the upper side without gaps. Particularly preferably, the at least one cover element is arranged on the upper side without any gaps. Preferably, the first bearing point is arranged on the upper side of the at least one bracket. Preferably, the third bearing point is arranged on the upper side of the at least one bracket. Preferably, the upper side of the at least one console is in particular at least 50 cm and preferably at least 60 cm spaced apart from the cabin floor. In principle, the at least one console can form a plurality of upper sides which have a different distance from the cabin floor.In an embodiment no longer according to the invention, it is proposed that the at least one guide unit comprises at least one actuator which is provided to support a movement of the at least one table element between the retracted state and the extended state of the at least one table unit. This configuration enables an advantageously simple actuation of the at least one table unit. Passenger comfort can thereby be advantageously increased. The at least one actuator is preferably designed as a pneumatic and / or hydraulic actuator. The at least one actuator is particularly preferably designed as a spring, in particular as a gas pressure spring. In principle, the at least one actuator can also be designed as a hydraulic actuator and / or as an electromechanical actuator. A fifth bearing point of the at least one guide unit is provided in particular for connecting the at least one actuator to the at least one bracket. Preferably, the fifth bearing point is arranged on the console or in the stowage space of the at least one console. The fifth bearing point is preferably designed as a pivot bearing. A sixth bearing point of the at least one guide unit is provided in particular for connecting the at least one actuator to the at least one holding arm or the at least one further holding arm. Preferably, the sixth bearing point is arranged on the at least one holding arm or on the at least one further holding arm. The sixth bearing point is preferably designed as a pivot bearing. In principle, the sixth bearing point of the at least one guide unit can also be provided for connecting the at least one actuator to the at least one table element.In one configuration no longer according to the invention, it is proposed that the at least one actuator is designed as a lockable push-push element. This configuration makes it possible to achieve an advantageously simple actuation of the at least one table unit. Passenger comfort can thereby be advantageously increased. By "lockable" is to be understood in particular that the push-push element is lockable in at least one defined position by means of a holding force generated by the push-push element in order to position the at least one table unit in at least one defined position, in particular in the retracted state or in the extended state. The push-push element is provided in particular in the event of a compressive load to transfer the at least one table unit from the retracted state to the extended state and / or to transfer it from the extended state to the retracted state. Preferably, the push-push element can be locked in the retracted state and / or in the extended state by a compressive load on the at least one holding arm, on the at least one further holding arm and / or on the at least one table element. The push-push element can preferably be triggered by a compressive load on the at least one holding arm, on the at least one further holding arm and / or on the at least one table element in the retracted state and / or in the extended state. A "compressive load" is to be understood in particular as an introduction of a compressive force onto a component by a person, wherein the compressive force can be applied by the person in particular by means of a finger. Particularly preferably, a mechanism of the push-push element is configured according to a ballpoint pen principle. In principle, the at least one guide unit can have at least one triggering unit which is provided to trigger the at least one actuator. The at least one triggering unit preferably has a Bowden cable which is provided for triggering the at least one actuator. The triggering unit preferably has a button or a switch which is provided for actuating the Bowden cable.In an embodiment that is no longer according to the invention, it is proposed that the at least one table unit comprises at least one grip element which, in at least one operating state, is provided for a force introduction by a person in order to adjust the at least one table unit between the retracted state and the extended state of the at least one table unit. This configuration makes it possible to allow an advantageously simple adjustment of the at least one table unit by a person. Passenger comfort can thereby be advantageously increased. The at least one grip element preferably has an at least partially circular inner contour. Particularly preferably, the at least one grip element has a circular inner contour in a hand grip region which is provided for the introduction of a pulling force by a person onto the at least one grip element.In one configuration no longer according to the invention, it is proposed that the at least one grip element is designed as a holder, in particular as a beverage holder. This configuration advantageously allows achieving a multiple function of the at least one grip element. As a result, an installation space and a weight of the aircraft seat device can be advantageously reduced. As a result of the configuration, a holder, in particular a beverage holder, can advantageously be provided in a region of the at least one table unit. Particularly preferably, the holder, in particular the beverage holder, can be used in the retracted state and in the extended state of the at least one table unit. Preferably, the holder, in particular the beverage holder, is at least partially annular. The holder, in particular the beverage holder, preferably has an inner diameter which is preferably at least 5 cm and particularly preferably at least 7 cm. In principle or in addition, the holder can also be designed as a PED holder (personal electronic device holder) and / or as a remote control holder.In an embodiment no longer according to the invention, it is proposed that the at least one table unit has at least one further table element which is designed to be pivotable with respect to the at least one table element. This configuration makes it possible to provide an advantageously compactly storable table unit. This configuration advantageously allows a parking area to be enlarged. The at least one table unit preferably has at least one pivot bearing. Preferably, the at least one further table element is pivotably connected to the at least one table element by means of the at least one pivot bearing. Alternatively, the at least one table unit can have at least one further table element which is designed to be displaceable, in particular translationally, with respect to the at least one table element, wherein the at least one table unit has at least one linear bearing. The at least one further table element is preferably designed as a plate. Preferably, the at least one further table element has a base surface which at least substantially corresponds to a base surface of the at least one table element. The at least one table unit preferably has a folded-in state and a folded-out state. Preferably, the at least one further table element rests on the at least one table element in the folded-in state. Preferably, the at least one further table element can be pivoted away from the at least one seat during a transfer from the folded-in state into the unfolded state. Preferably, the at least one further table element, in the unfolded state of the at least one table unit, together with the at least one table element, forms the storage surface of the at least one table unit. Particularly preferably, the at least one further table element is arranged parallel to the at least one table element in the unfolded state.In addition, a system with the at least one table unit and with the at least one console of the aircraft seat device is proposed. This configuration advantageously allows the at least one console to be provided with at least one integrated table unit.The aircraft seat device according to the invention should not be limited to the application and embodiment described above. In particular, the aircraft seat device according to the invention can have a number that differs from a number of individual elements, components and units mentioned herein in order to fulfil a mode of operation described herein.DRAWINGSFurther advantages are evident from the following description of the drawings. Five exemplary embodiments of the invention are shown in the drawing. The drawings, specification and claims contain numerous features in combination. The skilled person will expediently also consider the features individually and summarize them to form meaningful further combinations.The following are shown: FIG. 1 shows a schematic illustration of an aircraft seat device no longer according to the invention, having a table unit in a retracted state in a first exemplary embodiment, FIG. 2 shows a schematic plan view of the aircraft seat device no longer according to the invention with the table unit in the retracted state in the first exemplary embodiment, FIG. 3 shows a schematic illustration of the aircraft seat device no longer according to the invention with the table unit in an extended state and in a folded-in state in the first exemplary embodiment, FIG. 4 shows a schematic plan view of the aircraft seat device no longer according to the invention with the table unit in the extended state and in the folded-in state in the first exemplary embodiment, FIG. 5 shows a schematic illustration of the aircraft seat device no longer according to the invention with the table unit in the extended state and in a deployed state in the first exemplary embodiment, FIG. 6 shows a schematic plan view of the aircraft seat device no longer according to the invention with the table unit in the extended state and the deployed state in the first exemplary embodiment, FIG. 7 shows a schematic plan view of an aircraft seat device no longer according to the invention with a table unit in a retracted state in a second exemplary embodiment, FIG. 8 shows a schematic plan view of the aircraft seat device no longer according to the invention with the table unit in an extended state and in a folded-in state in the second exemplary embodiment, FIG. 9 shows a schematic plan view of the aircraft seat device no longer according to the invention with the table unit in the extended state and in a deployed state in the second exemplary embodiment, FIG. 10 shows a schematic plan view of an aircraft seat device no longer according to the invention with a table unit in a retracted state in a third exemplary embodiment, FIG. 11 shows a schematic plan view of the aircraft seat device no longer according to the invention with the table unit in an extended state and in a folded-in state in the third exemplary embodiment, FIG. 12 shows a schematic plan view of the aircraft seat device no longer according to the invention with the table unit in the extended state and in a deployed state in the third exemplary embodiment, FIG. 13 shows a schematic plan view of an aircraft seat device no longer according to the invention with a table unit in a retracted state in a fourth exemplary embodiment, FIG. 14 shows a schematic plan view of the aircraft seat device no longer according to the invention with the table unit in an extended state in the fourth exemplary embodiment, FIG. 15 shows a schematic illustration of an aircraft seat device according to the invention with a table unit in a retracted state in a fifth exemplary embodiment, FIG. 16 is a schematic bottom perspective view of the table unit in the retracted state in the fifth embodiment, FIG. 17 shows a schematic plan view of the aircraft seat device according to the invention with the table unit in the retracted state in the fifth exemplary embodiment, and FIG. 18 shows a schematic plan view of the aircraft seat device according to the invention with the table unit in an extended state in the fifth exemplary embodiment.DESCRIPTION OF THE EMBODIMENTSFIGS. 1 to 6 show an aircraft seat device 10 ain a first exemplary embodiment no longer according to the invention. The aircraft seat device 10 ais provided for being mounted in an aircraft cabin of an aircraft, not shown in more detail. The aircraft seat device 10 ais provided to be mounted on a cabin floor of the aircraft cabin, which floor is not shown in more detail. The aircraft comprises the aircraft seat device 10 a.The aircraft seat device 10 aincludes a seat 12 a. The seat 12a has a seat bottom 14a. The seat 12a has a backrest 16a. The seat 12a includes a leg rest 18a. The seat 12a has a head rest 20a. The seat 12a has a seat direction 22a. The seat 12 ais arranged on the cabin floor, wherein the seat direction 22 ais oriented at an angle in the amount greater than zero to a flight direction 24 aof the aircraft. In the present case, the angle is 30 degrees. In principle, the angle can also be a value deviating therefrom. The seat 12a is shown in a TTL position.The aircraft seat device 10 aincludes a console 26 a, which is arranged laterally next to the seat 12 a. The console 26 ais arranged laterally next to the seat 12 a, as viewed along the seat direction 22 a. An imaginary plane running perpendicular to the seat direction 22 aintersects at least the seat bottom 14 ain the TTL position of the seat 12 aand the at least one bracket 26 a. In the present case, the console 26 a, on a side of the console 26 afacing away from the seat 12 a, adjoins a cabin wall of the aircraft cabin, which is not illustrated in any more detail. The console 26a has a trapezoidal base in the present case. The console 26a includes a storage compartment 28a. The stowage compartment 28 ais provided for receiving personal objects of a passenger or for receiving a life vest.The aircraft seat device 10 acomprises a cladding 30 a. The cladding 30 ais designed as a shell element. The fairing 30a is connected to the bracket 26a. The fairing 30a is formed integrally with the bracket 26a. The cladding 30 ais provided for permanent optical separation of the seat 12 ato adjacent aircraft seat devices, not shown in more detail. The aircraft seat devices, not shown in more detail, are arranged in front of and behind and next to the aircraft seat device 10 a, as viewed in the flight direction 24 a. The aircraft seat device 10 acomprises a door unit 32 a. The door unit 32a is provided for temporary optical separation of the seat 12a from a not shown aisle of the aircraft cabin. The door unit 32 ais coupled to the trim panel 30 a.The aircraft seat device 10 aincludes a table unit 34 a. The console 26a and the table unit 34a constitute a system. In FIGS. 2, 4 and 6, the console 26 ais shown above the table unit 34 aand in section parallel to the cabin floor. The table unit 34 ahas a retracted state (FIGS. 1 and 2 ) and an extended state (FIGS. 3 to 6 ). The console 26a has a storage space 36a. The stowage space 36 ais provided at least for at least substantially completely receiving the table unit 34 ain the retracted state in an at least substantially horizontal position.The table unit 34a has a table member 38a. The table member 38a is formed as a plate. The table element 38 aconstitutes a placement surface 40 aof the table unit 34 a. In the extended state of the table unit 34 a, the storage surface 40 ais arranged on a side of the table element 38 afacing away from the cabin floor. In the retracted state, the storage surface 40 ais completely covered by the console 26 a. In the extended state, the storage surface 40 ais arranged at least substantially parallel to the cabin floor. The table element 38 ais oriented at least substantially horizontally in the retracted state and in the extended state.The table unit 34a has a further table element 42a. The further table element 42 ais designed to be pivotable with respect to the table element 38 a. The table unit 34a has a pivot bearing, not shown in detail. The further table element 42 ais pivotably connected to the table element 38 aby means of the pivot bearing. The further table element 42 ais formed as a plate. The further table element 42 acomprises a base surface which at least substantially corresponds to a base surface of the table element 38 a. The table unit 34 ahas a folded state (FIGS. 1 to 4 ) and a deployed state (FIGS. 5 and 6 ). The further table element 42 ain the folded-in state rests on the table element 38 a. The further table element 42 acan be pivoted away from the seat 12 awhen it is transferred from the folded-in state into the unfolded state. The further table element 42 a, in the unfolded state of the table unit 34 a, together with the table element 38 a, forms the storage surface 40 aof the table unit 34 a. The further table element 42 ais arranged parallel to the table element 38 ain the unfolded state.The table unit 34 aincludes a grip member 44 a. The grip element 44 ais provided in at least one operating state for a force introduction by a person in order to adjust the table unit 34 abetween the retracted state and the extended state of the table unit 34 a. The grip element 44a has a circular inner contour 46a. The grip element 44 acomprises the circular inner contour 46 ain a hand-grip region which is provided for the introduction of a pulling force by a person onto the grip element 44 a. The grip element 44 ais designed as a beverage holder in the present case. The cup holder is usable in the retracted state and in the extended state of the table unit 34 a. The cup holder is partially formed annularly. The cup holder has an inner diameter which is at least 5 cm.The table unit 34a has a guide unit 48a. The guide unit 48 ais provided for at least substantially horizontal guidance of the table element 38 abetween the retracted state of the table unit 34 aand the extended state of the table unit 34 a. The guide unit 48a has a holding arm 50a. The support arm 50a is pivotally connected to the bracket 26a and movably connected to the table member 38a. The holding arm 50 ais provided to transmit a force acting on the table unit 34 a, in particular a weight force of the table unit 34 aand a supporting force, into the bracket 26 a. The support arm 50a is pivotally connected to the table member 38a. In the present case, the guide unit 48a has six bearing points 52a, 54a, 56a, 58a, 60a, 62a. A first bearing point 52 aof the guide unit 48 ais provided for the purpose of connecting the holding arm 50 ato the bracket 26 a. The first storage location 52 ais disposed in the storage space 36 aof the console 26 a. The first bearing point 52 ais designed as a pivot bearing. A second bearing point 54 aof the guide unit 48 ais provided for the purpose of connecting the holding arm 50 ato the table element 38 a. The second bearing point 54 ais arranged on the table element 38 a. The second bearing point 54 ais designed as a pivot bearing.The guide unit 48a has a further holding arm 64a. The grip element 44 ais arranged on the further holding arm 64 a. The grip element 44 ais formed integrally with the further holding arm 64 a. The further holding arm 64 ais provided for transmitting a force acting on the table unit 34 a, in particular a weight force of the table unit 34 aand a supporting force, into the bracket 26 a. The further holding arm 64 ais pivotably connected to the table element 38 a. A third bearing point 56 aof the guide unit 48 ais provided for the purpose of connecting the further holding arm 64 ato the bracket 26 a. The third storage location 56 ais arranged in the stowage space 36 aof the console 26 a. The third bearing point 56 ais designed as a pivot bearing. A fourth bearing point 58 aof the guide unit 48 ais provided for the purpose of connecting the further holding arm 64 ato the table element 38 a. The fourth bearing point 58 ais arranged on the table element 38 a. The fourth bearing point 58 ais designed as a pivot bearing.The holding arm 50a is pivotably mounted in a front region 66a of the bracket 26a and the further holding arm 64a is pivotably mounted in a rear region 68a of the bracket 26a. The front region 66 aof the console 26 ais arranged in front of the rear region 68 aof the console 26 awhen viewed counter to the seat direction 22 a. A theoretical plane oriented perpendicular to the seat direction 22 afirst intersects the front region 66 aand then the rear region 68 awhen the theoretical plane is moved counter to the seat direction 22 a. The holding arm 50 ais pivotably mounted via the first bearing point 52 aof the guide unit 48 ain the front region 66 aof the bracket 26 a. The further holding arm 64 ais pivotably mounted via the third bearing point 56 aof the guide unit 48 ain the rear region 68 aof the bracket 26 a. The table element 38 aand the holding arm 50 aare arranged at least partially overlapping with one another in the retracted state and in the extended state. The holding arm 50a has an overlap region 70a with a reduced component height of the holding arm 50a. The table element 38a has an overlap region 72a corresponding to the overlap region 70a of the holding arm 50a and having a reduced component height of the table element 38a. The overlap region 70 aof the holding arm 50 aand the corresponding overlap region 72 aof the table element 38 aadcreate at least partially in the retracted state and in the extended state. An imaginary line perpendicular to the placement surface 40 aand through the second bearing point 54 aintersects the overlap region 70 aof the holding arm 50 aand the corresponding overlap region 72 aof the table element 38 a. The holding arm 50 aand the table element 38 aform an at least substantially constant overall component height in the overlap region 70 aof the holding arm 50 aand in the corresponding overlap region 72 aof the table element 38 a, which total component height corresponds to a largest component height of the table element 38 a. The table element 38 aand the further holding arm 64 aare arranged at least partially overlapping with one another in the retracted state and in the extended state. The further holding arm 64 acomprises a further overlap region 74 awith a further reduced component height of the further holding arm 64 a. The table element 38a has an overlap region 76a, which corresponds to the further overlap region 74a of the further holding arm 64a and has a further reduced component height of the table element 38a. The further overlap region 74 aof the further holding arm 64 aand the further corresponding overlap region 76 aof the table element 38 aadcreate at least partially in the retracted state and in the extended state. A further imaginary line perpendicular to the placement surface 40 aand through the fourth bearing point 58 aintersects the further overlap region 74 aof the further holding arm 64 aand the further corresponding overlap region 76 aof the table element 38 a. The further holding arm 64 aand the table element 38 aform the at least substantially constant overall component height in the further overlap region 74 aof the further holding arm 64 aand in the further corresponding overlap region 76 aof the table element 38 a, which total component height corresponds to the largest component height of the table element 38 a. The guide unit 48 aincludes an actuator 78 a. The actuator 78 ais provided to assist movement of the table member 38 abetween the retracted state and the extended state of the table unit 34 a. The actuator 78 ais designed as a pneumatic actuator. The actuator 78 ais designed as a gas pressure spring in the present case. A fifth bearing point 60 aof the guide unit 48 ais provided for connecting the actuator 78 ato the bracket 26 a. The fifth bearing 60 ais disposed in the storage space 36 aof the console 26 a. The fifth bearing point 60 ais designed as a pivot bearing. A sixth bearing point 62 aof the guide unit 48 ais provided for the purpose of connecting the actuator 78 ato the holding arm 50 a. The sixth bearing point 62 ais arranged on the holding arm 50 a. The sixth bearing point 62 ais designed as a pivot bearing.The holding arm 50 a, in the retracted state and in the extended state of the table unit 34 a, serves at least partially as a closure element for an opening 80 aof the console 26 ato the stowage space 36 a. The closure element, in the extended state, is provided to close the opening 80 aof the console 26 a, at least to a substantial extent, i.e. to a percentage greater than 30%. The opening 80a has an opening portion. The holding arm 50 a, the other holding arm 64 a, and the table member 38 aare partially disposed in the opening portion in the retracted state and the extended state. The opening 80a has a base surface, not shown in detail, which is arranged parallel to an outer surface 84a of the bracket 26a. A distance of a plane, which is arranged in a surface of the table element 38 afacing the seat 12 aand is oriented perpendicularly to the cabin floor, from the outer surface 84 aof the console 26 ais in the present case at most 0.5 cm. The holding arm 50 a, the further holding arm 64 aand the table element 38 a reduce a mechanically freely penetrable area of the base surface of the opening 80 a, wherein the base surface is covered by the holding arm 50 a, the further holding arm 64 aand the table element 38 ato the extent of at least 90%. The holding arm 50 a, the further holding arm 64 aand the table element 38 aare provided to prevent a person from passing through the opening 80 a, in particular the opening region of the opening 80 a, by means of a finger. The bracket 26a has an opening cladding 82a. The opening trim 82 aconstitutes a frame around the opening 80 a. The opening cladding 82 aof the bracket 26 aconstitutes an opening contour. The opening trim 82 ais arranged at least substantially flush with the outer surface 84 aof the bracket 26 a. The holding arm 50 ais arranged on a side facing the seat 12 aat least substantially flush with the opening cladding 82 a. The holding arm 50 ais arranged on the side facing the seat 12 aat least substantially flush with the outer surface 84 aof the bracket 26 a.The further holding arm 64 a, in the retracted state and in the extended state of the table unit 34 a, serves at least partially as a further closure element for the opening 80 aof the console 26 ato the stowage space 36 a. The further closure element is provided in the retracted state to close the opening 80 aof the console 26 a, at least to a substantial extent, i.e. to a percentage greater than 40%. In the extended state, the holding arm 50 a, the further holding arm 64 aand the table element 38 aare provided to close the opening 80 aof the console 26 a, in particular the base area of the opening 80 aof the console 26 a, at least to 90%. The holding arm 50 a, the further holding arm 64 a, the table element 38 aand the further table element 42 aare provided in the retracted state to close the opening 80 aof the console 26 a, in particular the base area of the opening 80 aof the console 26 a, at least to 90%.The opening 80 aof the console 26 ato the stowage space 36 ais in each case closed to an extent of at least 90% in the retracted state and in the extended state of the table unit 34 a. In the retracted state, the opening 80 aof the bracket 26 ais closed without any gaps by the holding arm 50 a, the further holding arm 64 a, the table element 38 aand the further table element 42 a. In the extended state, the opening 80 aof the bracket 26 ais closed without any gaps by the holding arm 50 a, the further holding arm 64 aand the table element 38 a. A distance of the opening contour of the opening 80 ato the holding arm 50 a, to the further holding arm 64 a, to the table element 38 aand to the further table element 42 ais at least to a large extent less than 5 mm along the opening contour. The table element 38a has a vertically extending extension 86a on a side of the table element 38a facing the stowage space 36a. The extension 86 ais designed as a diaphragm. The extension 86a is provided in the extended and deployed state to at least partially close the opening 80a of the console 26a.Four further exemplary embodiments are shown in FIGS. 7 to 18. The following descriptions and the drawings are limited substantially to the differences between the exemplary embodiments, wherein with regard to identically denoted components, in particular with regard to components with the same reference numerals, reference can in principle also be made to the drawings and / or the description of the other exemplary embodiments, in particular of FIGS. 1 to 6. To distinguish between the exemplary embodiments, the letter a is appended to the reference numerals of the exemplary embodiment in FIGS. 1 to 6. In the exemplary embodiments of FIGS. 7 to 18, the letter a is replaced by the letters b to e.FIGS. 7 to 9 show an aircraft seat device 10 bin a second exemplary embodiment no longer according to the invention. The aircraft seat device 10 bis provided for being mounted on a cabin floor, not shown in more detail, of an aircraft cabin of an aircraft. The aircraft seat device 10 bincludes a seat 12 b. The seat 12 bhas a seat bottom 14 b. The seat 12 bhas a backrest 16 b. The seat 12b has a leg rest that is not visible. The seat 12 bhas a headrest 20 b. The seat 12 bhas a seat direction 22 b. The seat 12 bis arranged on the cabin floor, wherein the seat direction 22 bis oriented at an angle in the amount greater than zero to a flight direction 24 bof the aircraft. In the present case, the angle is 30 degrees. The aircraft seat device 10 bincludes a bracket 26 b, which is arranged laterally next to the seat 12 b. The console 26 bhas a trapezoidal base surface in the present case. The aircraft seat device 10 bhas a cladding 30 b. The aircraft seat device 10 bhas a door unit 32 b.The aircraft seat device 10 bincludes a table unit 34 b. The console 26b and the table unit 34b constitute a system. In FIGS. 7 to 9, the console 26 bis shown above the table unit 34 band in section parallel to the cabin floor. The table unit 34 bhas a retracted state (FIG. 7 ) and an extended state (FIGS. 8 and 9 ). The console 26 bhas a stowage space 36 b. The stowage space 36 bis provided at least for at least substantially completely receiving the table unit 34 bin an at least substantially horizontal position in the retracted state. The table unit 34 bincludes a table member 38 b. The table member 38b is formed as a plate. The table element 38 bconstitutes a placement surface 40 bof the table unit 34 b. In the extended state of the table unit 34 b, the storage surface 40 bis arranged on a side of the table element 38 bfacing away from the cabin floor. In the retracted state, the storage surface 40 bis at least substantially covered by the console 26 b. The table unit 34 bhas a further table element 42 b. The further table element 42 bis designed to be pivotable with respect to the table element 38 b. The table unit 34 bhas a pivot bearing, not shown in more detail. The further table element 42 bis pivotably connected to the table element 38 bby means of the pivot bearing. The further table element 42 bis formed as a plate. The further table element 42 bhas a base surface which at least substantially corresponds to a base surface of the table element 38 b. The table unit 34 bhas a folded state (FIGS. 7 and 8 ) and a deployed state (FIG. 9 ). The further table element 42 b,in the folded-in state, rests on the table element 38 b. The further table element 42 bcan be pivoted away from the seat 12 bwhen it is transferred from the folded-in state into the unfolded state. The further table element 42 b, in the unfolded state of the table unit 34 b, together with the table element 38 b, forms the storage surface 40 bof the table unit 34 b. The further table element 42 bis arranged parallel to the table element 38 bin the unfolded state.The table unit 34 bincludes a guide unit 48 b. The guide unit 48 bis provided for at least substantially horizontal guidance of the table element 38 bbetween the retracted state of the table unit 34 band the extended state of the table unit 34 b. The guide unit 48 bhas a holding arm 50 b. The support arm 50b is pivotally connected to the bracket 26b and movably connected to the table member 38b. The holding arm 50 bis provided to transmit a force acting on the table unit 34 b, in particular a weight force of the table unit 34 band a supporting force, into the bracket 26 b. The support arm 50 bis pivotally connected to the table member 38 b. In the present case, the guide unit 48 bhas four bearing points 52 b, 54 b, 56 b, 58 b. A first bearing point 52 bof the guide unit 48 bis provided for the purpose of connecting the holding arm 50 bto the bracket 26 b. The first bearing point 52 bis arranged on the bracket 26 b. The first bearing point 52 bis designed as a pivot bearing. A second bearing point 54 bof the guide unit 48 bis provided for the purpose of connecting the holding arm 50 bto the table element 38 b. The second bearing point 54 bis arranged on the table element 38 b. The second bearing point 54 bis designed as a pivot bearing.The guide unit 48 bhas a further holding arm 64 b. The further holding arm 64 bis provided for transmitting a force acting on the table unit 34 b, in particular a weight force of the table unit 34 band a supporting force, into the bracket 26 b. The further holding arm 64 bis pivotably connected to the table element 38 b. A third bearing point 56 bof the guide unit 48 bis provided for the purpose of connecting the further holding arm 64 bto the bracket 26 b. The third storage location 56 bis disposed in the storage space 36 bof the console 26 b. The third bearing point 56 bis designed as a pivot bearing. A fourth bearing point 58 bof the guide unit 48 bis provided for the purpose of connecting the further holding arm 64 bto the table element 38 b. The fourth bearing point 58 bis arranged on the table element 38 b. The fourth bearing point 58 bis designed as a pivot bearing.The holding arm 50 band the further holding arm 64 bare pivotably mounted in a front region 66 bof the bracket 26 b. The holding arm 50 bis pivotably mounted via the first bearing point 52 bof the guide unit 48 bin the front region 66 bof the bracket 26 b. The further holding arm 64 bis pivotably mounted via the third bearing point 56 bof the guide unit 48 bin the front region 66 bof the bracket 26 b. The table element 38 band the holding arm 50 bare arranged partially overlapping with one another in the retracted state and in the extended state. The table element 38 band the further holding arm 64 bare arranged partially overlapping with one another in the retracted state and in the extended state.FIGS. 10 to 12 show an aircraft seat device 10 cin a third exemplary embodiment no longer according to the invention. The aircraft seat device 10 cis provided for being mounted on a cabin floor, not shown in more detail, of an aircraft cabin of an aircraft. The aircraft seat device 10 ccomprises a seat 12 c. The seat 12c has a seat bottom 14c. The seat 12c includes a backrest 16c. The seat 12c has a leg rest not visible. The seat 12c includes a head rest 20c. The seat 12c has a seating direction 22c. The seat 12 cis arranged on the cabin floor, wherein the seat direction 22 cis oriented at an angle in the amount greater than zero to a flight direction 24 cof the aircraft. In the present case, the angle is 30 degrees. The aircraft seat device 10 ccomprises a bracket 26 c, which is arranged laterally next to the seat 12 c. The console 26c has a trapezoidal base in the present case. The aircraft seat device 10 ccomprises a cladding 30 c. The aircraft seat device 10 ccomprises a door unit 32 c.The aircraft seat device 10 ccomprises a table unit 34 c. The console 26c and the table unit 34c constitute a system. In FIGS. 10 to 12, the console 26c is shown above the table unit 34c and in section parallel to the cabin floor. The table unit 34 ccomprises a retracted state (FIG. 10 ) and an extended state (FIGS. 10 and 11 ). The console 26c includes a storage space 36c. The stowage space 36 cis provided at least for at least substantially completely receiving the table unit 34 cin an at least substantially horizontal position in the retracted state. The table unit 34c includes a table member 38c. The table member 38c is formed as a plate. The table element 38c forms a storage surface 40c of the table unit 34c. In the extended state of the table unit 34 c, the storage surface 40 cis arranged on a side of the table element 38 cfacing away from the cabin floor. In the retracted state, the storage surface 40 cis at least substantially covered by the console 26 c. The table unit 34c comprises a further table element 42c. The further table element 42 cis designed to be pivotable with respect to the table element 38 c. The table unit 34c has a pivot bearing, not shown in detail. The further table element 42 cis pivotably connected to the table element 38 cby means of the pivot bearing. The further table element 42 cis formed as a plate. The further table element 42 ccomprises a base surface which at least substantially corresponds to a base surface of the table element 38 c. The table unit 34 cincludes a folded state (FIGS. 10 and 11 ) and a deployed state (FIG. 12 ). The further table element 42 cis resting on the table element 38 cin the folded-in state. The further table element 42 cis pivotable away from the seat 12 cin a transfer from the folded-in state to the unfolded state. The further table element 42 c, in the unfolded state of the table unit 34 c, together with the table element 38 c, forms the storage surface 40 cof the table unit 34 c. The further table element 42 cis arranged parallel to the table element 38 cin the unfolded state.The table unit 34c includes a grip member 44c. The grip element 44 cis provided in at least one operating state for a force introduction by a person in order to adjust the table unit 34 cbetween the retracted state and the extended state of the table unit 34 c. The grip element 44 ccomprises a circular inner contour 46 c. The grip element 44 cis designed as a beverage holder in the present case. The cup holder is usable in the retracted state and the extended state of the table unit 34c. The beverage holder is formed as a recess in the placement surface 40 c. The beverage holder is in each case formed as a mutually corresponding recess in the table element 38 cand in the further table element 42 c. In the unfolded state, the grip element 44 cis divided into two.The table unit 34c includes a guide unit 48c. The guide unit 48 cis provided for at least substantially horizontal guidance of the table element 38 cbetween the retracted state of the table unit 34 cand the extended state of the table unit 34 c. The guide unit 48c has a holding arm 50c. The support arm 50c is pivotally connected to the bracket 26c and movably connected to the table member 38c. The holding arm 50 cis provided to transmit a force acting on the table unit 34 c, in particular a weight force of the table unit 34 cand a supporting force, into the bracket 26 c. The support arm 50 cis pivotally connected to the table member 38 c. In the present case, the guide unit 48c has four bearing points 52c, 54c, 56c, 58c. A first bearing point 52 cof the guide unit 48 cis provided for the purpose of connecting the holding arm 50 cto the bracket 26 c. The first bearing point 52 cis arranged on the bracket 26 c. The first bearing point 52 cis designed as a pivot bearing. A second bearing point 54 cof the guide unit 48 cis provided for the purpose of connecting the holding arm 50 cto the table element 38 c. The second bearing 54 cis arranged on the table element 38 c. The second bearing point 54 cis designed as a pivot bearing.The guide unit 48c has a further holding arm 64c. The further holding arm 64 cis provided for transmitting a force acting on the table unit 34 c, in particular a weight force of the table unit 34 cand a supporting force, into the bracket 26 c. The further holding arm 64 cis pivotably connected to the table element 38 c. A third bearing point 56 cof the guide unit 48 cis provided for the purpose of connecting the further holding arm 64 cto the bracket 26 b. The third bearing point 56 cis arranged on the bracket 26 c. The third bearing point 56 cis designed as a pivot bearing. A fourth bearing point 58 cof the guide unit 48 cis provided for the purpose of connecting the further holding arm 64 cto the table element 38 c. The fourth bearing 58 cis arranged on the table element 38 c. The fourth bearing point 58 cis designed as a pivot bearing.The holding arm 50 cand the further holding arm 64 care pivotably mounted in a rear region 68 cof the bracket 26 c. The holding arm 50 cis pivotably mounted via the first bearing point 52 cof the guide unit 48 cin the rear region 68 cof the bracket 26 c. The further holding arm 64 cis pivotably mounted via the third bearing point 56 cof the guide unit 48 cin the rear region 68 cof the bracket 26 c. The table element 38 cand the holding arm 50 care arranged partially overlapping with one another in the retracted state and in the extended state. The table element 38 cand the further holding arm 64 care arranged partially overlapping with one another in the retracted state and in the extended state. The holding arm 50 cand the further holding arm 64 care provided to support the further table element 42 cin the deployed state of the table unit 34 c.FIGS. 13 and 14 show an aircraft seat device 10 din a fourth exemplary embodiment no longer according to the invention. The aircraft seat device 10 dis provided for being mounted on a cabin floor, not shown in more detail, of an aircraft cabin of an aircraft. The aircraft seat device 10 dcomprises a seat 12 d. The seat 12 dcomprises a seat bottom 14 d. The seat 12 dcomprises a backrest 16 d. The seat 12d has a leg rest which is not visible. The seat 12 dcomprises a headrest 20 d. The seat 12 dcomprises a seat direction 22 d. The seat 12 dis arranged on the cabin floor. The seat direction 22 dis oriented parallel to a flight direction 24 dof the aircraft. The aircraft seat device 10 dcomprises a bracket 26 d, which is arranged laterally next to the seat 12 d. The console 26 dhas a rectangular base area in the present case. The aircraft seat device 10 dcomprises a cladding 30 d. The aircraft seat device 10 dcomprises a door unit 32 d.The aircraft seat device 10 dcomprises a table unit 34 d. The console 26d and the table unit 34d constitute a system. In FIGS. 13 and 14, the console 26 dis shown above the table unit 34 dand in section parallel to the cabin floor. The table unit 34 dhas a retracted state (FIG. 13 ) and an extended state (FIG. 14 ). The console 26 dincludes a storage space 36 d. The stowage space 36 dis provided at least for at least substantially completely receiving the table unit 34 din the retracted state in an at least substantially horizontal position. The table unit 34 dcomprises a table element 38 d. The table member 38d is formed as a plate. The table element 38 dconstitutes a placement surface 40 dof the table unit 34 d. In the extended state of the table unit 34 d, the storage surface 40 dis arranged on a side of the table element 38 dfacing away from the cabin floor. In the retracted state, the storage surface 40 dis at least substantially covered by the console 26 d. The table member 38d is formed integrally.The table unit 34 dincludes a guide unit 48 d. The guide unit 48 dis provided for at least substantially horizontal guidance of the table element 38 dbetween the retracted state of the table unit 34 dand the extended state of the table unit 34 d. The guide unit 48 dcomprises a holding arm 50 d. The support arm 50d is pivotally connected to the bracket 26d and movably connected to the table member 38d. The holding arm 50 dis provided to transmit a force acting on the table unit 34 d, in particular a weight force of the table unit 34 dand a supporting force, into the bracket 26 d. The support arm 50 dis pivotally connected to the table member 38 d. In the present case, the guide unit 48 dcomprises five bearing points 52 d, 54 d, 60 d, 62 d, 88 d. A first bearing point 52 dof the guide unit 48 dis provided for the purpose of connecting the holding arm 50 dto the bracket 26 d. The first storage location 52 dis disposed in the storage space 36 dof the console 26 d. The first bearing point 52 dis designed as a pivot bearing. A second bearing point 54 dof the guide unit 48 dis provided for the purpose of connecting the holding arm 50 dto the table element 38 d. The second bearing point 54 dis arranged on the table element 38 d. The second bearing point 54 dis designed as a pivot bearing.The guide unit 48 dcomprises a rail element 90 d. The rail element 90 dis provided for translatory guidance of the table element 38 d. The holding arm 50 dis pivotably mounted in a front region 66 dof the bracket 26 d. The holding arm 50 dis pivotably mounted via the first bearing point 52 dof the guide unit 48 din the front region 66 dof the bracket 26 d. The rail element 90 dis arranged in the bracket 26 d. The rail element 90 dis arranged at least substantially parallel to the seat direction 22 d. The rail member 90d extends from a rear portion 68d of the bracket 26d to a central portion 92d of the bracket 26d. The central region 92 dis disposed between the rear region 68 dand the front region 66 d. A further bearing point 88 dof the guide unit 48 dis provided for the purpose of connecting the rail element 90 dto the table element 38 d. The further bearing point 88 dis arranged in the stowage space 36 dof the console 26 d. The further bearing point 88 dis designed as a pivot bearing which is designed to correspond to the rail element 90 d. The table element 38 dand the holding arm 50 dare arranged partially overlapping with one another in the retracted state. The table element 38 dand the holding arm 50 dare arranged at least substantially completely overlapping one another in the extended state.The guide unit 48 dcomprises an actuator 78 d. The actuator 78 dis provided to assist in movement of the table member 38 dbetween the retracted state and the extended state of the table unit 34 d. The actuator 78 dis designed as a pneumatic actuator. The actuator 78 dis designed in the present case as a gas pressure spring. A fifth bearing point 60 dof the guide unit 48 dis provided for connecting the actuator 78 dto the bracket 26 d. The fifth storage location 60 dis disposed in the storage space 36 dof the console 26 d. The fifth bearing point 60 dis designed as a pivot bearing. A sixth bearing point 62 dof the guide unit 48 dis provided for the purpose of connecting the actuator 78 dto the holding arm 50 d. The sixth bearing point 62 dis arranged on the holding arm 50 d. The sixth bearing point 62 dis designed as a pivot bearing. The actuator 78 dis designed as a lockable push-push element. The push-push element is provided, under a compressive load, for transferring the table unit 34 dfrom the retracted state to the extended state and for transferring it from the extended state to the retracted state. The push-push member is lockable in the retracted state by a compressive load on the table member 38 d. The push-push member is triggerable by a compressive load on the table member 38 din the retracted state.In the present case, the guide unit 48 dcomprises a closure element, not shown in more detail. The closure element is designed as a brush or as a seal. The closure element is arranged on the rail element 90d and in the bracket 26d.In the retracted state of the table unit 34 a, the holding arm 50 dis used at least partially as a closure element for an opening 80 dof the console 26 dto the stowage space 36 d. The closure element is provided in the retracted state to close the opening 80 dof the console 26 d, at least to a substantial extent, i.e. to a percentage greater than 20%. The opening 80 dincludes an opening portion. The holding arm 50 dand the table member 38 dare partially disposed in the opening portion in the retracted state and the extended state. The opening 80 dhas a base surface, not shown in detail, which is arranged parallel to an outer surface 84 dof the bracket 26 d. A distance of a plane, which is arranged in a surface of the table element 38 dfacing the seat 12 dand is oriented perpendicularly to the cabin floor, from the outer surface 84 dof the console 26 dis at most 0.5 cm in the present case. The holding arm 50 dand the table element 38 dreduct a mechanically freely penetrable area of the base surface of the opening 80 d, wherein the base surface is covered by the holding arm 50 dand the table element 38 dto the extent of at least 90% in the retracted state. The holding arm 50 dand the table member 38 dare provided to prevent a finger of a person from penetrating the opening 80 d, particularly the opening portion of the opening 80 d. The holding arm 50 dis arranged on the side facing the seat 12 don least substantially flush with the outer surface 84 dof the bracket 26 d. The opening 80 dof the console 26 dto the stowage space 36 dis closed in each case to an extent of at least 90% in the retracted state and in the extended state of the table unit 34 d.FIGS. 15 to 18 show an aircraft seat device 10 ein a fifth exemplary embodiment according to the invention. The aircraft seat device 10 eis provided to be mounted on a cabin floor, not shown in more detail, of an aircraft cabin of an aircraft. The aircraft seat device 10 ecomprises a seat 12 e. The seat 12 ecomprises a seat bottom 14 e. The seat 12 ecomprises a backrest 16 e. The seat 12e has a leg rest which is not visible. The seat 12 ecomprises a headrest 20 e. The seat 12 ehas a seat direction 22 e. The seat 12 eis arranged on the cabin floor, wherein the seat direction 22 eis oriented at an angle in the amount greater than zero with respect to a flight direction 24 eof the aircraft. In the present case, the angle is 12 degrees. In principle, the angle can also be a value deviating therefrom. The seat 12 eis shown in a TTL position.The aircraft seat device 10 ecomprises a bracket 26 ewhich is arranged laterally next to the seat 12 e. The console 26 ein the present case has a trapezoidal base surface. The bracket 26 ehas an upper side 94 e. The top surface 94 eis oriented at least substantially horizontally. The top surface 94e forms an upper surface of the bracket 26e. The top side 94 econstitutes an at least substantially planar surface. The top side 94 eis arranged at least substantially parallel to the cabin floor. The upper side 94 eof the console 26 eis in the present case spaced apart 70 cm from the cabin floor. In principle, the console 26 ecan also form a plurality of upper sides which have a different distance from the cabin floor. The aircraft seat device 10 ecomprises an operating panel 96 e. The control panel 96 eis arranged on the console 26 e. The control panel 96 eis designed as a user interface which is provided at least for controlling the seat 12 e. The aircraft seat device 10 ecomprises a cladding 30 e.The aircraft seat device 10 ecomprises a table unit 34 e. The console 26e and the table unit 34e constitute a system. The table unit 34 ehas a retracted state (FIGS. 15 to 17 ) and an extended state (FIG. 18 ). The table unit 34 eincludes a table member 38 e. The table member 38 eis formed as a plate. The table element 38 econstitutes a placement surface 40 eof the table unit 34 e. The storage surface 40 eis arranged on a side of the table element 38 efacing away from the cabin floor in the extended state of the table unit 34 eand in the retracted state of the table unit 34 e. The table member 38e is formed integrally. In the retracted state, the table element 38 elies completely on the upper side 94 eof the console 26 e. In the retracted state, the table element 38 eis arranged without gaps on the upper side 94 e.The table unit 34 eincludes a guide unit 48 e. The guide unit 48 eis provided for at least substantially horizontal guidance of the table element 38 ebetween the retracted state of the table unit 34 eand the extended state of the table unit 34 e. In the present case, the guide unit 48 ehas four bearing points 52 e, 54 e, 60 e, 62 e. The table element 38 ehas a recess 120 e(FIG. 16 ). The recess 120 eis arranged on an underside of the table element 38 e, which underside is opposite the placement surface 40 e. In the retracted state, the guide unit 48 eis arranged at least substantially completely in the recess 120 eof the table element 38 e.The guide unit 48 ecomprises a holding arm 50 e. The support arm 50e is pivotally connected to the bracket 26e and movably connected to the table member 38e. The holding arm 50 eis provided to transmit a force acting on the table unit 34 e, in particular a weight force of the table unit 34 eand a supporting force, into the bracket 26 e. The support arm 50 eis pivotally connected to the table member 38 e. A first bearing point 52 eof the guide unit 48 eis provided for the purpose of connecting the holding arm 50 eto the bracket 26 e. The first bearing point 52 eis arranged on the bracket 26 d. The first bearing point 52 eis arranged on the upper side 94 eof the bracket 26 e. The first bearing point 52 eis designed as a pivot bearing. A second bearing point 54 eof the guide unit 48 eis provided for the purpose of connecting the holding arm 50 eto the table element 38 e. The second bearing point 54 eis arranged on the table element 38 e. The second bearing point 54 eis designed as a pivot bearing. In the present case, the holding arm 50 eis embodied in multiple parts. The holding arm 50 ecomprises two arm elements 98 e, 100 e. The arm members 98e, 100e are pivotally connected to each other. The support arm 50 ecomprises a first arm member 98 eand a second arm member 100 e. The first arm member 98 eand the second arm member 100 eare pivotally connected to each other. The holding arm 50 ecomprises a pivot bearing 102 e, via which the first arm element 98 eand the second arm element 100 eare pivotably connected to one another. The first arm element 98 eof the holding arm 50 eis connected to the bracket 26 evia the first bearing point 52 e. The second arm element 100 eof the holding arm 50 eis connected to the table element 38 evia the second bearing point 54 e.The guide unit 48 ecomprises a further holding arm 64 e. The further holding arm 64 eis provided for transmitting a force acting on the table unit 34 e, in particular the weight force of the table unit 34 eand a supporting force, into the bracket 26 e. The further holding arm 64 eis pivotably connected to the table element 38 e. A third bearing point 56 eof the guide unit 48 eis provided for the purpose of connecting the further holding arm 64 eto the bracket 26 e. The third bearing point 56 eis arranged on the bracket 26 e. The third bearing point 56 eis arranged on the upper side 94 eof the bracket 26 e. The third bearing point 56 eis designed as a pivot bearing. A fourth bearing point 58 eof the guide unit 48 eis provided for the purpose of connecting the further holding arm 64 eto the table element 38 e. The fourth bearing point 58 eis arranged on the table element 38 e. The fourth bearing point 58 eis designed as a pivot bearing. The further holding arm 64 eis embodied in multiple parts. The further holding arm 64 ecomprises two further arm elements 104 e, 106 e. The two further arm elements 104 e, 106 eof the further holding arm 64 eare pivotably connected to one another. The further holding arm 64 ecomprises a first further arm element 104 eand a second further arm element 106 e. The first further arm element 104 eand the second further arm element 106 eare pivotably connected to one another. The further holding arm 64 ehas a further pivot bearing 108 e, via which the first further arm element 104 eand the second further arm element 106 eare pivotably connected to one another. The first further arm element 104 eof the further holding arm 64 eis connected to the bracket 26 evia the third bearing point 56 e. The second further arm element 106 eof the further holding arm 64 eis connected to the table element 38 evia the fourth bearing point 58 e.The guide unit 48 ehas a coupling point 110 e, via which the holding arm 50 eis pivotably connected to the further holding arm 64 e. The coupling point 110 eis designed as a pivot bearing. The coupling point 110 eis provided to preset a defined movement path of the table element 38 ebetween the retracted state and the extended state. In the present case, the first arm element 98 eof the holding arm 50 ehas an extension which is provided for coupling to the further holding arm 64 e. The extension forms the coupling point 110 e. In the present case, the second further arm element 106 ehas an extension corresponding to the extension of the first arm element 98 e. In principle, another connection that appears suitable to the skilled person for coupling the holding arm 50 eand the further holding arm 64 ealso would be conceivable.The guide unit 48 ecomprises a cover element 112 e. The cover element 112 eis provided to partially cover the holding arm 50 eand the further holding arm 64 e. The cover element 112 eis arranged partially without gaps on the upper side 94 ein the extended state. A person cannot grasp under the cover member 112 ein an operating state in an assembled state of the table unit 34 e. In the present case, the cover element 112 eis connected to the holding arm 50 e. The cover element 112 eis formed integrally with the holding arm 50 ein the present case. The cover element 112 eis arranged without gaps on the upper side 94 ein the retracted state. The table element 38 eis provided in the retracted state to completely conceal the guide unit 48 e.The aircraft seat device 10 ecomprises a stowage compartment 114 e. The storage compartment 114 eis connected to the console 26 e. The storage compartment 114 eis disposed over a rear portion 66 eof the console 26 e. The stowage compartment 114 eis provided in the present case for receiving personal objects of a passenger. The storage compartment 114 eis disposed above the top surface 94 eof the console 26 e. The storage compartment 114 ecomprises a roller shutter 116 e. Between the console 26 eand the stowage compartment 114 e, a stowage space 118 eof the aircraft seat device 10 eis formed. The storage space 118 eis provided to partially receive the table member 38 ein the retracted state. In the present case, the stowage space 118 eis provided in the retracted state to receive 30% of the storage area 40 e. In the retracted state, the storage space 118 eis at least substantially completely filled by the table member 38 e.Alternatively, the console 26 emay have a stowage space which is provided at least for at least substantially completely receiving the table unit 34 ein an at least substantially horizontal position in the retracted state.

Claims

Aircraft seat device (10e) having at least one seat (12e), having at least one console (26e) which is arranged at least substantially laterally next to the at least one seat (12e) and has at least one upper side (94e) which is aligned horizontally and forms an upper surface of the console (26e), and having at least one table unit (34e) which has at least one table element (38e) and at least one guide unit (48e), wherein the at least one guide unit (48e) is provided for at least substantially horizontal guidance of the at least one table element (38e) between a retracted state of the at least one table unit (34e) and an extended state of the at least one table unit (34e) and has at least one holding arm (50e), which is pivotably connected to the at least one console (26e) and movably connected to the at least one table element (38e), characterized in that the table element (38e) in the retracted state rests completely on the upper side (94e) of the console (26e).Aircraft seat device (10e) according to claim 1, characterised in that the at least one guide unit (48e) has at least one further holding arm (64e).Aircraft seat device (10e) according to claim 1 or 2, characterized in that the at least one holding arm (50e) comprises at least two arm elements which are pivotably connected to one another.Aircraft seat device (10e) according to Claims 2 and 3, characterized in that the at least one guide unit (48e) has at least one coupling point via which the at least one holding arm (50e) is pivotably connected to the at least one further holding arm (64e).Aircraft seat device (10e) according to one of the preceding claims, characterized in that the table element (38e) is arranged on the upper side (94e) without any gaps in the retracted state.Aircraft seat device (10e) according to one of the preceding claims, characterized in that the table element (38e) has a recess (120e) on an underside opposite its placement surface (40e), wherein the guide unit is arranged completely in the recess (120e) of the table element (38e) in the retracted state.Table unit (34e) for an aircraft seat device (10e) according to one of claims 1 to 6.System with at least one table unit (34e) and with at least one console (26e) of an aircraft seat device (10e) according to one of Claims 1 to 6.

Images