摘要:
A cabin attendant seat (14) comprises a backrest element (20) and a seat element (22) which is secured to the backrest element (20). The backrest element (20) is rotatable about a rotation axis (24a, 24b) in order to move the cabin attendant seat (14) between a rest position and an operating position. A fastening device (18) for fastening the cabin attendant seat (14) to a side wall (16) of an aircraft monument (12) is constructed and sized in such a manner that it is capable of directing away a predetermined maximum force which can be introduced into the cabin attendant seat (14) during operation of the cabin attendant seat (14) via the side wall (16) of the aircraft monument (12).
摘要:
A safety seat for vehicles, including a seat portion having a rear end supported against vertical support straps of a strap framework secured to a vehicle. Each of two supports laterally disposed on the seat portion as a first end secured to the set. From the first end, each support extends in an inclined path, below the seat portion, to the vertical support straps. Each support has a free end remote from the first end and suspended in a loop formed on the vertical support straps. To tensioning straps are disposed beneath the seat portion and extend along side edges thereof from a front securement and the seat portion to a connection with the vertical support straps. Each tensioning strap has a length less than the distance between the front securement and the rear end of the seat portion.
摘要:
The child's seat for airplanes comprises a mounting adapted to be fastened to a partition wall of an airplane, and a seat fastened to the mounting such that the seat can assume two different vertical positions. In an upper takeoff and landing position, the seat is located above the head strike arc of a person seated on an airplane seat, while in a lower communicating position, assumed during the flight, the seat is at chest level of the accompanying person. Thanks to the child's seat, the number of adult passengers normally occupying passenger seats of an airplane need not be reduced.
摘要:
An energy attenuating apparatus for use with a seat includes an elongated attenuator having a resistance to bending which varies along its length. A bending mechanism defining a nonlinear path receives the attenuator. Translation of the bending mechanism relative to the attenuator in a lengthwise direction of the attenuator produces bending of the attenuator to absorb energy applied to the energy attenuating apparatus.
摘要:
A bulkhead-mounted aircraft seat assembly configured for independent vertical and horizontal adjustment includes an aircraft seat (seatback and seat frame/cushion) for supporting a pilot, passenger, or other occupant. Parallel rails attach to the bulkhead and extend along the bulkhead (vertically or near vertically) with opposing slots set into each rail. A sled translates along the rails via paired sliding members set into the slots, each pair of sliding members connected to an axle extending through the sled. A four-bar linkage attached to the sled and to the aircraft seat; the four-bar linkage extends from a default position to allow the aircraft seat to translate along a horizontal linear rail under the seat while maintaining a stable vertical reference point above the cabin floor. The seat is independently configured for substantially vertical adjustment via a metering plate attached to the bulkhead.
摘要:
An aircraft seat assembly including stanchions defining elongated guide channels and elongated motion sleds nested in the guide channels and affixed to a seat bucket. An energy absorber implemented as a wire bender assembly is coupled between the stanchions and the motion sled. In use, the elongated guide channels guide motion of the motion sleds and the wire bender assemblies attenuate energy during a dynamic event exceeding a predetermined threshold load value. The elongated interface between the guide channels and motion sleds serve to transfer excessive loading to the seat frame thereby protecting the seat assembly from damage and the occupant from excessive lumbar spinal loads.
摘要:
A crew attendant seat assembly configured to be installed in an aircraft cabin and including a seat including a seat bottom hinged to a seatback to rotate between a stowed position and a deployed position, a spring member mountable to a static structure adjacent the and to an adjustable aperture on the hinge, the spring having two mounting positions, a harness mounted to the seat for restraining a seated passenger including a shoulder strap and a lap belt, and a storage area for retaining at least one of the lap belt and the buckle when the seat bottom is stowed, wherein at least one of the lap belt and the buckle are enclosed by the crew attendant seat assembly when the seat bottom is stowed.
摘要:
A cabin segment for a vehicle includes a first lateral segment module having a first main extension axis, a second lateral segment module having a second main extension axis, and an aisle arranged in the cabin segment. The main extension axes parallel to each other, and the first and second lateral segment modules are distanced from each other in a direction perpendicular to the main extension axes and enclose the aisle, which runs parallel to the main extension axes. At least one of the first lateral segment module and the second lateral segment module includes a lavatory accessible through a lavatory opening positioned outside the aisle. The first lateral segment module includes at least one receiving space to receive serving trolleys. The at least one receiving space has a receiving opening facing into the aisle.
摘要:
An aircraft assembly with first and second seat rails for interlocking with an aircraft seat, and a systems component mounting member interlocked with those seat rails. The mounting member has a first anchor member interlocked with the first seat rail and a second anchor member interlocked with the second seat rail. The assembly includes an aircraft systems component mounted on the mounting member. Existing seat rails or tracks of the aircraft can be used for attachment of support brackets for aircraft systems components. A novel way of using existing seat rails to provide anchorage points for systems brackets for systems components is disclosed.
摘要:
An apparatus for holding a cabin attendant seat in a cabin of a vehicle includes a base body attachable to a wall surface in the cabin, at least one holding mechanism for holding a cabin attendant seat, at least one linear movement mechanism, and at least one arresting mechanism. The at least one linear movement mechanism is attached to the base body and supports the at least one holding mechanism. The at least one linear movement mechanism is configured for laterally moving the at least one holding mechanism between at least two laterally distanced discrete positions. The at least one arresting mechanism is coupled with the at least one linear movement mechanism and is configured for arresting the at least one linear movement mechanism in the at least two discrete positions. By this apparatus a very space effective provision of a cabin attendant seat especially on a monument is given.