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: An airplane seat device with at least one airplane seat is at least configured to be adjusted between a use position and a stowage position. In the stowage position, the airplane seat has a maximum height which is equal to or less than a maximum height in the use position.

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: An airplane seat device with at least one airplane seat is at least configured to be adjusted between a use position and a stowage position. In the stowage position, the airplane seat has a maximum height which is equal to or less than a maximum height in the use position.

Abstract: A seat fixing device for fixing a vehicle seat, in particular an aircraft passenger seat, to at least one fixing rail that is attached to a vehicle structure, comprising a fixing means that is to be coupled to the at least one fixing rail, and comprising a force transmitting unit that is used in a normal olperating mode to provide a first force application path of a weight and acceleration force that is introduced into the vehicle structure via the vehicle seat. The force transmitting unit has a transmitting means that is used in an impact mode to at least initiate a generation of at least one second force application path of the weight and acceleration force that is introduced into the vehicle structure via the vehicle seat.

Abstract: A seating device, in particular on a flight passenger seating device includes a moveably mounted primary unit and a moveably mounted secondary unit. The seating device has a locking unit which, depending on at least one operating position of the secondary unit, avoids a movement of the primary unit relative to a mounting unit.

Abstract: An airplane passenger seat device includes a seat part, which has a seat surface, a seat direction and a main body, which abuts an aisle in a installed state in a means of transportation and which, in a usage position, laterally covers the seat surface in a region that is lateral to the seat surface with respect to the seat direction. It is proposed that the passenger seat device has a bearing unit for moveably mounting the main body, which is provided to move the main body from the usage position into a release position by way of a movement relative to the seat surface, which causes the region lateral to the seat surface to be released.

Abstract: A fitting body having at least one fitting unit is produced, at least to a large part, from a material having a density of less than 7000 kg/m3.

Abstract: A connecting device, system and method for use in an industrial installation is disclosed, which includes at least one first industrial bus interface configured to receive first industrial bus input data and transmit first industrial bus output data using a first industrial bus protocol, and a second industrial bus interface configured to receive second industrial bus input data and transmit second industrial bus output data using a second industrial bus protocol. A modulator is configured to produce first energy bus output data by modulating the first industrial bus input data onto an industrial Ethernet protocol and configured to produce second energy bus output data by modulating the second industrial bus input data onto the industrial Ethernet protocol. An energy communicator is configured to transmit the first and second energy bus output data together as an energy bus output signal on the energy supply line using a carrier frequency method.

Abstract: A seat fixing device for fixing a vehicle seat, in particular an aircraft passenger seat, to at least one fixing rail that is attached to a vehicle structure, comprising a fixing means that is to be coupled to the at least one fixing rail, and comprising a force transmitting unit that is used in a normal olperating mode to provide a first force application path of a weight and acceleration force that is introduced into the vehicle structure via the vehicle seat. The force transmitting unit has a transmitting means that is used in an impact mode to at least initiate a generation of at least one second force application path of the weight and acceleration force that is introduced into the vehicle sttucture via the vehicle seat.

Abstract: A seat device, in particular a motor vehicle or airplane seat device, has a table mounting unit. It is suggested that the table mounting unit comprises at least one coupling gear.

Abstract: An airplane passenger seat device includes a seat part, which has a seat surface, a seat direction and a main body, which abuts an aisle in a installed state in a means of transportation and which, in a usage position, laterally covers the seat surface in a region that is lateral to the seat surface with respect to the seat direction. It is proposed that the passenger seat device has a bearing unit for moveably mounting the main body, which is provided to move the main body from the usage position into a release position by way of a movement relative to the seat surface, which causes the region lateral to the seat surface to be released.

Abstract: A passenger seat device, in particular an airplane passenger seat device, which comprises a support assembly of stretched fabric for holding a stretched fabric element, the support assembly of stretched fabric comprising a frame unit.

Abstract: The invention relates to a seat, in particular, a vehicle or aircraft passenger seat with seat components such as a seat base (12), a backrest (14) and a coupling device (16) for coupling the movement of at least one part of the seat components between an exit (I) and at least one comfortable (II) position and vice versa. According to the invention, the coupling device (16) comprises at least one control piece, which may be controlled using the movement of the backrest (14) and/or the seat base (12) and hence by means of at least one further control piece to move the seat base (12) and/or the backrest (14) between said positions (I, II), whereby an adjustment, in particular, tilting movement of the backrest is linked with a simultaneous adjustment movement of the seat base which, preferably in the rearward transition region into the backrest descends by a given amount relative to the front edge of the seat which simultaneously moves forward to increase the seat depth.

Abstract: A seat device, in particular an aircraft seat device, with a bearing unit and with a seat unit which is mounted movably by means of the bearing unit, with a locking unit for locking the seat unit in at least one position, and with an overload protection unit which permits movement of the seat unit in the event of an overload. It is proposed that the overload protection unit has a delay unit which is provided in order to bring about a delay at least over a large part of an overload displacement.

Abstract: A seat arrangement for an aircraft seat includes a seat frame for mounting the seat on a cabin floor and a seat region. The seat arrangement has a backrest unit and is designed to improve stiffness of the backrest unit against one-sided torsional load. The backrest unit is coupled to the seat frame by a kinematic unit having at least first and second kinematic parts coupled to a first side and a second side of the backrest unit, respectively. A stiffening member is located in the seat region that couples the first and second kinematic parts and is provided for transmitting a torsional moment from the first side of the backrest unit to the second side of the backrest unit.

Abstract: A seat device, in particular a motor vehicle or airplane seat device, has a table mounting unit. It is suggested that the table mounting unit comprises at least one coupling gear.

Abstract: In a seating system for passenger service vehicles, and for aircraft in particular, having a seat structure (19), a seat element, a backrest (5), an arm rest (7), and table element (1), the table element (1) is movable between a storage position and a use position. In the use position, the table element (1) faring a table surface (3). The table element (1) is pivotally connected to the seat structure (19, 27) by lever mechanism (23, 33), and a power drive (21) is provided, which is coupled to the lever mechanism (23, 33) to form an over-center mechanism. The power drive (21) pivots the table element (1) from the storage position into an intermediate position, which is defined by the over-center mechanism, and from the intermediate position into the use position after over-centering of the intermediate position has been overcome by application of a force to the table element (1).

Abstract: A seating apparatus, and in particular a vehicle or aircraft seating apparatus, includes a seat base bearing unit which is provided in order to mount a seat base in a movable manner. The seat base bearing unit comprises at least one movably mounted stiffening member which has at least two coupling points in the transverse direction of the seat base bearing unit.

Abstract: The invention is based on a seat arrangement, in particular for an aircraft seat, with a back rest unit. It is proposed that the back rest unit has at least one stiffening means in a seat region.