43 results about "Airplane passenger" patented technology

A seat unit for a passenger of an aircraft, including a seat and a shell, the seat including a sitting portion and a backrest movable on a base, respectively actuated by a motor-driven mechanism, the unit including a means for detecting the presence of the passenger on the seat, the seat being configured to adopt a takeoff / taxiing / landing position when a presence of the passenger is detected, in which the sitting portion is away from the shell and in which the backrest is reclined in the direction of the shell, and a docking position when a presence of the passenger is not detected, in which the sitting portion is close to the shell, and in which the backrest is substantially parallel to the shell, so as to widen the egress between two seat units.

A seat unit for a passenger of an aircraft, including a seat and a shell, the seat including a sitting portion and a backrest movable on a base, respectively actuated by a motor-driven mechanism, the unit including a means for detecting the presence of the passenger on the seat, the seat being configured to adopt a takeoff / taxiing / landing position when a presence of the passenger is detected, in which the sitting portion is away from the shell and in which the backrest is reclined in the direction of the shell, and a docking position when a presence of the passenger is not detected, in which the sitting portion is close to the shell, and in which the backrest is substantially parallel to the shell, so as to widen the egress between two seat units.

The invention relates to the technical field of zone control of illumination, in particular to a zone control method of an airplane passenger cabin scene illumination system, which comprises the following steps: acquiring real-time external natural light parameters of each porthole area in a passenger cabin and real-time passenger distribution data of each zone in the passenger cabin, and generating a first illumination distribution diagram through a ray tracing algorithm; real-time biological rhythm feedback signals of the passenger groups in all the partitions are obtained based on a non-imaging microwave radar sensor, the biological rhythm feedback signals comprise a first type of signals and a second type of signals, the current overall activity state of the passenger groups in all the partitions is judged based on the first type of signals, and the rest state depth is subdivided based on the second type of signals; and when the adjustment amplitude of the illumination parameters of the adjacent partitions exceeds a fifth preset threshold value, generating a natural transition zone of the illumination parameters between the adjacent partitions. By arranging the transition zone, the visual boundary is eliminated through gradient change of the transition zone of the adjacent partitions, and discomfort is reduced.

The disclosure concerns a double bench seat for transport craft passengers having a sitting configuration and a lying configuration, and including a substantially vertical shell surrounding two independent twin seats. The two twin seats are oriented along the longitudinal axis of the aircraft, the two twin seats each assume, independently of one another, at least one chair-like position and one bed-like position, the two twin seats include a backrest and a seat, in the bed-like position, the two twin seats are extended by an extension. When the double bench seat is in the lying configuration, the two twin seats are in the bed-like position and arranged to be at the same height and to form a continuous horizontal surface with a width and length adapted to form a double bed that can accommodate two lying persons.

An aircraft passenger seat assembly includes a frame subassembly mounted on a base subassembly. The frame subassembly interfaces with the base subassembly through a plurality of position adjustable receivers configured to adjust an angle of the frame assembly relative to the base assembly. In embodiments, the positions of the receivers are reconfigurable to provide a particular fixed seat angle at the time of installation of the passenger seat assembly in an aircraft. The base subassembly may be implemented as a frame assembly or a plinth permitting the frame subassembly to be mounted forward or aft facing. In embodiments, the frame subassembly defines a motion path for a seat pan movably mounted to the frame subassembly.

The present patent describes a mechanical system for transporting pets in passenger areas of vehicles and aircraft which, according to the features thereof, enables the formation of a mechanical system (1) for transporting pets having its own specific structure mounted by means of a structured assembly on the seat (A) inside the means of transportation (C) such as vehicles and aircraft and based on an anchoring base (2) fastened to the internal seat (A), a comfort platform (3) fitted onto the anchoring base (2) to support the pet, and a safety harness / chest strap (4) fastened around the pet and to the comfort platform (3) to anchor the pet, with a view to allowing complete optimization of efficiently ergonomic pet transportation procedures through effective, safe, and comfortable restraint in the passenger areas inside the cabin of the means of transportation (C).

A safety system for aircraft passenger seats is described. A pallet that can be removably coupled to seats can also be removably coupled to the aircraft floor and one or more brackets, tension fittings, or machined straps that can be coupled to structural beams or components in an aircraft. A keel tension fitting can be attached to a keel beam and then be coupled to the pallet and thereby the seats. By attaching to the keel beam the safety system allows the seating arrangement (pallet and seats) to withstand greater stresses and forces, resulting in increased safety.

The invention provides a seat embedded type circulating humidification and ventilation system used under a low-humidity mixed ventilation background. The seat embedded type circulating humidification and ventilation system can be applied to scenes such as an airplane passenger cabin or a train cabin. The invention relates to an independent embedded seat circulating ventilation system, which is integrally embedded in a cabin seat and is provided with an air supply pipeline, an air return pipeline, an air treatment device and an air blower, and an air supply port and an air return port at the tail end of the air supply pipeline and the air return pipeline are embedded in a seat partition plate; the air supply outlet delivers wet air to the passenger breathing area, and then the wet air and airflow generated by passenger breathing are recycled to the air processing device through the air return inlet to be re-purified and re-humidified and delivered again. The air supply pipeline and the air return pipeline are suitable for sitting and lying postures and can operate independently, and the height of an air supply port and the height of an air return port are set according to the height of the head of a passenger in the two postures. Wet air is recycled through 100% return air supply, the water consumption is reduced to the maximum extent, the humidification cost is reduced, meanwhile, an air curtain is formed at the head position of a passenger, and pollutant diffusion is prevented.

The utility model discloses a passenger service unit interface device for an airplane passenger cabin, which comprises an interface body and a fixing frame, the fixing frame is arranged on the left side wall and the right side wall of the interface body, the fixing frame comprises a fixing frame surface and a fixing frame surface, the fixing frame surface and the fixing frame surface are distributed in an L shape, and the fixing frame surface and the fixing frame surface are arranged on the left side wall and the right side wall of the interface body. A first installation hole is formed in one face of the fixing frame, a second installation hole corresponding to the first installation hole is formed in the connector body, the connector body and one face of the fixing frame are fixed through bolts via the first installation hole and the second installation hole, and positioning holes are formed in the two faces of the fixing frame. The interface body is fixedly connected with a station through the positioning holes in the second face of the fixing frame and bolts, and the side wall of the interface body is provided with a communication interface. By providing diversified communication interfaces, a stable installation mode, enhanced structural strength and convenient identification and use, the satisfaction degree of passengers is greatly improved.

The utility model discloses a low-pressure buffer cavity of an air conditioning system of an airplane passenger cabin, which particularly relates to the field of airplane ventilation structures and comprises a shell sleeve, a buffer space is arranged in the shell sleeve, and airflow in the buffer space is conveyed to the cabin; the gas buffering assembly comprises an upper buffering layer, a lower buffering layer and a buffering partition piece, the buffering partition piece divides the buffering space in the shell sleeve into the upper buffering layer and the lower buffering layer which are arranged up and down, and a plurality of air guiding openings are formed in the buffering partition piece; the air inlet pipe assembly is used for guiding airflow generated by the air conditioner host to the buffer space; wherein the density degree of the air guide openings is in negative correlation with the distance between the air guide openings and the air inlet pipe assembly, the smaller the distance is, the larger the number of the air guide openings in the unit area is, airflow and sound field distribution is optimized through the trapezoidal geometric structure, the noise reduction performance is improved, meanwhile, airflow pressure loss can be relieved, and two purposes are achieved.

The invention provides an aircraft ground air conditioner control method and system, electronic equipment and a program product, and relates to the technical field of civil aviation airport ground guarantee. The method comprises the steps that a boarding bridge control unit receives triggering operation of entering an airplane ground air conditioner parameter setting mode; in response to the triggering operation, user identity verification is executed, and an air conditioner operation parameter setting interface is provided after verification is passed; obtaining a target operation parameter input by a user through the setting interface, and generating a control instruction based on the target operation parameter; and the control instruction is sent to an aircraft ground air conditioner control unit. According to the embodiment of the invention, the response speed of the adjustment requirement of the aircraft ground air conditioner can be improved, the airport operation working efficiency is effectively improved, and the taking experience of aircraft passengers is improved.

The present invention relates to facilities for passengers on board aircraft. To provide passengers of an aircraft with improved user comfort, a passenger compartment (10) for an aircraft cabin is provided, comprising a partition (12) and a compartment space (14) formed by the partition, in which at least one passenger seat (16) is arranged. The partition has wall sections (18) that extend from the floor at least to the head height of a standing passenger. At least a portion of the wall sections is designed as hybrid walls, each comprising a lower wall segment (20) and an upper wall segment (22), wherein the lower wall segment is fixed and the upper wall segment is adjustable, allowing for variable airflow in this area.

The utility model discloses a special lamp for airplane passenger cabin maintenance, which comprises a lamp body, the right side of the lamp body is fixedly connected with a rechargeable battery, the right side of the rechargeable battery and the left side of the lamp body are provided with a rotating mechanism, and the lower end of the rotating mechanism is provided with a lifting mechanism. A hook mechanism is arranged at the outer end of the lifting mechanism; an auxiliary reset mechanism is arranged in the rotating mechanism, the rotating mechanism comprises an outer frame, an inner ring column is arranged in the outer frame, and multiple sets of blocking pieces are fixedly connected to the inner wall of the outer frame; when the lamp is used, the lamp is fixed, the irradiation direction of the lamp body can be rotated through rotation of the lamp body and the rotating mechanism, and therefore the illumination direction can be adjusted, when the high position needs to be adjusted, lifting can be conducted through the lifting mechanism, and when the high position needs to be fixed, hanging storage can be conducted on the high position through the hook mechanism.

The utility model discloses an explosion-proof type airplane passenger cabin lighting device, which relates to the technical field of airplane passenger cabin lighting, and comprises a fixing ring, the outer side of the fixing ring is fixedly connected with an assembly flange, the fixing ring is arranged in a passenger cabin through the assembly flange, and the fixing ring is flush with the inner wall of the passenger cabin; a mounting ring is in threaded connection with the interior of the fixing ring, two symmetrically-distributed clamping blocks are connected with the interior of the mounting ring in a clamped mode, the two clamping blocks are spliced to form a ball seat structure, a ball joint is rotationally connected with the interior of the ball seat structure, and a lighting structure is mounted in the ball joint. According to the anti-explosion type airplane passenger cabin lighting device, the lighting assembly is allowed to rotate freely in any direction through a ball seat structure formed by a ball joint and a clamping block, precise angle fixing is achieved through cooperation with damping, and the irradiation range of LED lamp beads can be adjusted through the linkage design of a movable sleeve and a lens; the requirement for multi-dimensional adjustment of the lighting direction and range in a passenger cabin scene is met, and meanwhile safety is ensured through an anti-explosion material and a sealing structure.

The utility model discloses an air filter applied to an airplane passenger cabin. The air filter comprises a filter element and a filter frame assembly, the filter element is arranged on the filter frame assembly, the filter element is a cylinder with a hollow interior and an upper opening and a lower opening, at least one rubber line is arranged in the filter element, the rubber line is annularly adhered to the inner surface of the filter element, and at least one circular-ring-shaped binding belt is arranged on the outer surface of the filter element in a sleeving manner; the filter element is of an annular structure formed by bending filter paper, and the filter paper comprises bending parts which are connected end to end and are uniformly arranged. The filter frame assembly plays a role in supporting and protecting the filter element, the rubber lines can enable bent areas on the inner side of the filter element to be evenly distributed, and therefore it is guaranteed that in the bending process of manufacturing the filter element, adjacent folded corners are not bonded, and the wind receiving area of the filter element is not reduced. The bridle is arranged on the outer surface of the filter element in a sleeving mode after the filter element is shaped, and the service life of the filter element is prolonged. Due to the arrangement of the bent part, the contact area between the filter element and air is increased, and the filtering efficiency of the filter element is further improved.

According to the invention, a computer-implemented method for controlling a passenger seating area (14, 16) is proposed, wherein in a method step (102) at least one passenger destination parameter is recorded and in a determination method step (106) a flight time activity plan (210) is created from at least the passenger destination parameter and at least one flight and / or destination parameter, which has at least one activity time window (212 - 232), and in a setting method step (110) at least one presetting according to the flight time activity plan (210) is preset on the passenger seating area (14, 16).

A passenger service unit fixing element for releasably fixing a passenger service unit in a passenger cabin of an aircraft comprises a clamping body and a locking element that is rotatably arranged in the clamping body. The clamping body comprises at least one clamp, and each of the at least one clamp comprises a coupling portion for being coupled to the passenger service unit and a clamping portion for being clamped to a support member provided in the passenger cabin. The clamping portion comprises two clamp arms that are elastically movable with respect to each other between a clamped configuration, in which the support member is clampable between the two clamp arms, and a released configuration, in which the clamping portion is detachable from the support member.

An aircraft passenger reading light comprises a plurality of pairs of light sources. Each of the plurality of pairs of light sources includes: a first light source for emitting light having a first color, and a second light source for emitting light having a second color, wherein the second color differs from the first color. The aircraft passenger reading light further comprises, for each of the plurality of pairs of light sources: a first optical system for forming a first light output from the light emitted by the first light source, and a second optical system for forming a second light output from the light emitted by the second light source.

The present invention relates to an aircraft information system and a method for providing information to passengers, such as flight information or entertainment information, to passengers of an aircraft by means of communication between at least one passenger device and the aircraft information system. The system comprises: storage means for storing information, one or more processing units for processing the information, power supply means for powering the aircraft information system, and data communication means, such as wireless communication means, for communicating with at least one passenger device. The aircraft information system is configured as a self-contained unit to operate autonomously, i.e., independently of other aircraft systems.and where the aircraft information system comprises: - receiving means for receiving source information relating to the aircraft to form, on the basis of said information, the corresponding passenger information for transmission to at least one passenger device.

The invention relates to a table device of a vehicle seat, in particular an aircraft passenger seat (12; 30), which has at least one storage surface (16) and a storage unit (20) which is provided to guide the at least one storage surface (16) during a movement between at least one operating position and at least one first stowing position. It is proposed that the table device has a locking unit (26; 33) which is designed to use a movement of the storage surface (16) at an angle of less than 15 degrees relative to the storage surface (16) as a locking movement, wherein the locking unit (26; 33) has a lifting unit (34) for lifting at least the storage surface (16) by moving the storage surface (16) from the first stow position to a second, locked stow position, wherein the lifting unit (34) includes a rotary knob (35) which is rotatably mounted on an underside (36) of the storage surface (16) facing a floor (11) of an interior space (10) in a central position about a pivot axis (37) within a predetermined rotation range.

The utility model relates to the field of storage frame, concretely refers to a convenient storage frame for clothes in airplane passenger cabin, including the clothes hanger with the ring, and can freely rotate, carry out a variety of combination collocation seat number signboard etc.

This invention relates to an aircraft seat module comprising: a housing unit (14a; 14b; 14c) that at least partially defines an aircraft passenger seat area (10a; 10b; 10c); and a door unit (22a; 22b; 22c) that is at least configured to close, at least in an operational state, a passageway area (18a; 19a; 10b) leading to the aircraft passenger seat area (10a; 10c). 8b); a bearing assembly (24a; 24b; 24c) configured to movably support the door unit (22a; 22b; 22c) relative to the housing unit (14a; 14b) between an open position and a closed position; and a locking device (28a; 28b; 28c) configured to lock the door unit (22a; 22b; 22c) in the open position. It is proposed that the locking device (28a; 28b; 28c) has at least one electrically and / or electronically actuated actuator device (56a; 56b; 56c), which is at least configured to be electrically and / or electronically actuated to unlock the door unit (22a; 22b; 22c).

The invention provides a data acquisition system, method and device for an airplane passenger cabin, relates to the technical field of data transmission, and is used for solving the problem that the content of acquired data on an airplane is less. The system comprises a passenger cabin server which is used for receiving and storing resource data pushed by a ground server through a satellite communication subsystem and storing a data storage state. And the onboard gateway equipment is used for receiving the data request message sent by the passenger terminal and distributing a request processing path for the data request message according to the data storage state in the passenger cabin server. The onboard gateway equipment is also used for determining to process the data request message through the passenger cabin server under the condition that the data is stored in the passenger cabin server; if the data is not stored in the cabin server, it is determined that a request is sent to the ground server via the satellite communication subsystem such that the ground server processes the data request message.

An adjustable seat 100 for an aircraft, comprising: a seat pan 101; a seat back 103 comprising; a first portion 104 pivotably mounted to the seat pan 101 , a second portion 105 pivotably mounted to the first portion 104; a lever arm 122 mounted to one of the first 104 and second portion 105 of the seat back 103; and a linear actuator 120 mounted on the other of the first 104 and second portion 105 of the seat back 103, and arranged to move a drive arm 120; wherein the drive arm 120 engages with the lever arm 122 to pivot the second portion 105 with respect to the first portion 104. The second portion 105 may be a headrest, and the seat 100 can move into a bed configuration. Another actuator may also pivot the first portion 104 with respect to the seat pan 101. Figures 1 and 2.

An aircraft passenger seat is proposed, having a support, wherein the support is provided for fastening to a floor of an aircraft passenger cabin, wherein the support comprises a seat partition (37) and a crossbeam which extends transversely to the seat direction, wherein the seat partition is held by the crossbeam, wherein a housing having a structural component (38) is provided, wherein the housing at least partially surrounds a backrest. According to the invention, the seat partition (37) is connected to the structural component (38) by means of a connection device (40), wherein the connection device (40) is configured as a plug-in connection device.

An aircraft seating unit (10) for an aircraft passenger, the aircraft seating unit comprising: a seat (12) comprising a seat pan (16), the seat pan having a seat pan cushion (22) mounted thereon, and a backrest (18); an ottoman (20), having an ottoman cushion (24) mounted thereon; and a footwell (28) positioned between the seat (12) and the ottoman (20); wherein one of the seat pan cushion (22) and ottoman cushion (24) is arranged to be rotated from a first folded position to a second unfolded position, such that in the unfolded position the footwell (28) is substantially covered. Figure 5a to accompany abstract on publication.

Systems, apparatuses, and methods provide for a door handle mechanism including a vent panel, a handle lever, and a four bar mechanism. The handle lever has a lift-to-open configuration. The four bar mechanism is coupled to the handle lever and the vent panel. The four bar mechanism is to time sequence operations to close an aircraft passenger door, latch the aircraft passenger door, lock the aircraft passenger door, and close the vent panel in response to the handle lever being toggled between a closed position and an open position.

An aircraft seating unit (10) for an aircraft passenger, the aircraft seating unit comprising: a seat (12) comprising a seat pan (16), the seat pan having a seat pan cushion (22) mounted thereon, and a backrest (18); an ottoman (20), having an ottoman cushion (24) mounted thereon; and a footwell (28) positioned between the seat (12) and the ottoman (20); wherein one of the seat pan cushion (22c) and ottoman cushion (24) is arranged to be rotated from a first folded position to a second unfolded position, such that in the unfolded position the footwell (28) is substantially covered.