Abstract: An aircraft seat device has a multi-part backrest frame unit comprising at least one first side frame element, at least one second side frame element, which is arranged on a side of the backrest frame unit that is opposite from the first side frame element, and at least one transverse frame element which is realized separately from the side frame elements and connects the side frame elements, wherein the transverse frame element is realized at least substantially plate-shaped.

Abstract: An assembly kit for an aircraft seat comprising at least one mounting unit, at least one backrest which is fixedly coupled with the mounting unit in a state when assembled and ready for flight, and at least one connection module, via which the backrest is in particular oriented rigidly in a position relative to the mounting unit in the assembled and ready-for-flight state, and the connection module comprises at least one adjusting element, by means of which the backrest is orientable respectively in at least two different backrest adjustment angles relative to the mounting unit without requiring new approval, and/or comprises at least two connection elements, by means of which the backrest can be fixedly mounted respectively in at least two different backrest adjustment angles relative to the mounting unit, the at least two connection elements being mountable without requiring new approval.

Abstract: The invention relates to an aircraft seat assembly (14a; 14b; 14c; 14d) comprising at least one aircraft seat device (46a; 46b; 46c; 46d) and at least one additional aircraft seat device (48a; 48b; 48c; 48d) which are arranged at least partly next to one another in at least one common column of seats (36a; 36b; 36c; 36d) and each of which can be adjusted between a sitting position and a lying position. According to the invention, the lying direction (64a; 64b; 64c; 64d) of the at least one aircraft seat device (46a; 46b; 46c; 46d) is oriented in the opposite direction to another lying direction (96a; 96b; 96c; 96d) of the at least one other aircraft seat device (48a; 48b; 48c; 48d).

Abstract: An aircraft seat module having a flight passenger seating area has a door unit which in at least one operating state is configured at least to close a passage region to the flight passenger seating area, and has a locking device for the door unit, which is configured to lock the door unit in an open position, in particular a maximally open stowage position, and to this end comprises at least one actuator device which has at least two movably supported locking elements, which are in each case adjustable between a locking position and an unlocking position, wherein that the locking device has a locking state indication unit which at least in the maximally open position of the door unit is configured to detect and indicate incomplete locking of at least one of the two locking elements.

Abstract: An aircraft seat fixation device for a fixation at least of a portion of an aircraft seat on at least one fixation rail that is fixated on an aircraft structure comprises a seat base structure which is configured such that at least the aircraft seat is mounted thereon at least partially, further comprises at least one seat foot which is connected to the seat base structure, and comprises at least one fitting element which is connected to the seat foot and is at least configured to be coupled with the fixation rail, wherein the aircraft seat fixation device comprises at least one compensation unit, which is arranged on the seat base structure, the seat foot and/or the fitting element and which is configured to permit at least one compensation movement of the seat base structure at least in an overload case.

Abstract: Aircraft passenger seat device includes an aircraft seat row, comprising having a mounting unit, and three or more neighboring seat areas. In the two outer seat areas, an aircraft seat with a seat bottom and a backrest is mounted to the mounting unit. In the middle seat area a backrest base body is mounted to the mounting unit. In one or more operating states a detachable center console is detachably mounted to the mounting unit in the middle seat area forming a separation between the two outer seats. The backrest base body has one or more functional elements on its rear side provided for the use by a passenger sitting behind.

Abstract: An aircraft seat device with at least one shell element, with at least one table unit, with at least one support device that is configured to obliquely connect the at least one table unit to the shell element at least in a stowage position, the support device comprising at least one rotational bearing unit, which is configured for pivoting the table unit between the stowage position and at least one intermediate position that is situated substantially in a horizontal plane, the support device comprising at least one linear bearing unit, which is configured for traversing the table unit between the intermediate position and at least one completely deployed usage position that is close to a seat.

Abstract: An aircraft seat module includes an enclosure unit which delimits a flight passenger seating region at least partially, and includes a door unit which at least closes a passage region to the flight passenger seating region in one or more operation states. The aircraft seat module further includes a bearing device which supports the door unit movably relative to the enclosure unit and has for this purpose a bearing module having a first bearing element and a second bearing element which are supported such that they are movable relative to each other.

Abstract: In a passenger seating arrangement in an aircraft cabin, the passenger seating arrangement has exactly two rows of seat units and exactly one aisle. A first row of seat units and a second row of seat units are separated by the aisle. The rows of seat units and the aisle all extend in a longitudinal direction parallel to a longitudinal axis of the aircraft cabin. Each seat unit includes a seat, an upper shell and a lower shell, the lower shell forming a footwell. The seats are arranged in parallel to each other in a seating direction. An upper shell of a first seat unit and a lower shell of a second seat unit, which, viewed in the longitudinal direction, is arranged behind the first seat unit, partially overlap in a vertical direction.

Abstract: An airplane seat device includes at least one functional unit that is configured at least for a locking, a controlling and/or a movement of at least one airplane seat element, wherein the functional unit includes at least one actuatable shape-memory element.

Abstract: The invention relates to a life vest container device, in particular aircraft seat life vest container device, for a life vest unit, with a life vest container comprising an accommodation unit that has an accommodation space as well as an access opening to the accommodation space, and with a monitoring device. It is proposed that the monitoring device is at least configured to capture a change of at least one characteristic via at least one electric and/or electronic signal.

Abstract: A life vest device, for a fixation on one or more aircraft seats, with a life vest unit, which is embodied as a lift vest with a packaging unit for a sealed accommodation of the life vest unit and with an opening unit for an opening of the packaging unit, which features one or more pull straps. The opening unit is functionally connected with the life vest unit and the packaging unit comprises one or more fixation units for a fixation on an aircraft seat. For a retrieval of the life vest unit from the packaging unit, the opening unit is connected in a tear-proof manner with the life vest unit. The pull strap and the life vest are embodied integrally with each other.

Abstract: An aircraft seat device for an aircraft seat includes at least one mounting unit, having at least one seat bottom which is coupled with the mounting unit and is configured to implement a seating region and to this end has at least one main unit and at least one sub-unit that in relation to the mounting unit is implemented so as to be adjustable between a stowage position and a use position. The at least one adjustable sub-unit is configured for enlarging the seating region in at least one position, and having at least one actuation mechanism by means of which the adjustable sub-unit of the seat bottom is adjustable between its stowage position and its use position.

Abstract: A table device for a seat, in particular for an aircraft seat, includes a table unit which is configured for being adjustable at least between a use position and a stowage position, and has at least one locking module which has at least one attachment unit which is configured for being at least in part fixedly connected to a seat component, wherein the table unit at least in the stowage position is lockable to the attachment unit. The locking module has at least two force-fit and/or form-fit elements, by means of which the table unit in a locked state is coupled in a form-fitting and/or force-fitting manner to the attachment unit.

Abstract: A transport seat system, in particular aircraft seat system, includes at least one first seat, with at least one mounting module that is configured, for the purpose of mounting the seat, to be connected on a guide rail, and with at least one second seat, which is arranged behind the first seat with at least one mounting module that is configured, for the purpose of mounting the seat, to be connected on the same guide rail, the two seats being configured, for the purpose of implementing a usage position and a stowage position of at least one of the seats, to be displaced on the guide rail relative to one another, wherein at least one mounting module of at least one of the seats includes a seat foot unit, which is movably supported relative at least to a portion of the mounting module.

Abstract: An aircraft device includes at least one control and/or regulation unit which is configured for controlling an aircraft passenger seat unit, and of a PED in which at least one operating program is stored, wherein the control and/or regulation unit is configured to receive control signals from the PED for controlling the aircraft passenger seat unit.

Abstract: A seat device, particularly aircraft seat device, includes at least one head-support module, which device has a central cushion unit and at least one lateral cushion unit, wherein the lateral cushion unit is supported movably relative to the central cushion unit.

Abstract: A headrest device for a seat, in particular for an airplane seat, with a headrest implementing at least one head support zone. The headrest device comprises at least one fixation module with at least one fixation means, which is configured to arrange at least one personal item in the head support zone.

Abstract: An aircraft seat device includes at least one seat bottom unit, a mounting unit, and at least one carrier element. The at least one seat bottom unit at least partly implements a seat surface. The at least one carrier element couples the seat bottom unit with the mounting unit and transfers force from the seat bottom unit to the mounting unit.

Abstract: An aircraft seat system has at least one first aircraft seat region, which includes a first aircraft seat, and at least one second aircraft seat region, which is arranged behind the first aircraft seat region and includes a second aircraft seat, wherein, in a mounted state, the aircraft seat of the second aircraft seat region is arranged, at least in a lying position, at least partially overlapping beneath the first aircraft seat region.