A seat attached to a vehicle structure by at least four attachment points comprises, on at least one of the attachments an extendable connecting element (40) which transmits load between the main structure (11) of the seat and the structure of the vehicle, the extendable connecting element (40) including: a first position in which a structure pin (62), which attaches the extendable connecting element (40) to the structure of the vehicle, is in a position close to a seat pin (64) that attaches the extendable connecting element (40) to the main structure (11) of the seat; a second position in which the structure pin (62) is in a position away from the seat pin (64) and in which the extendable connecting element (40) is able to transmit load between the structure pin (62) and the seat pin (64).

There is disclosed an energy absorption device comprising a plurality of pillars mountable to a ceiling of a hull, each pillar having a fixed portion and a movable portion, the movable portion slidable relative to the fixed portion; a deformable material disposed between the fixed portion and movable portion such that the deformable material resist the sliding movement of the movable portion in one direction; the deformable material further adapted to permanently deform when a blast energy is directed towards the ceiling; and a seat assembly attached to the movable portion, the seat assembly adapted for an occupant.

There is disclosed an energy absorption device comprising a plurality of pillars mountable to a ceiling of a hull, each pillar having a fixed portion and a movable portion, the movable portion slidable relative to the fixed portion; a deformable material disposed between the fixed portion and movable portion such that the deformable material resist the sliding movement of the movable portion in one direction; the deformable material further adapted to permanently deform when a blast energy is directed towards the ceiling; and a seat assembly attached to the movable portion, the seat assembly adapted for an occupant.

An energy absorbing assembly includes an attachment component configured to be coupled to a mounting structure. The energy absorbing assembly also includes an anchor that has a tip portion, a shaft, and a head. The anchor is configured to extend through the attachment component such that the head is disposed on a first side of the attachment component and the tip portion is disposed on a second side of the attachment component and is configured to be coupled to the mounting structure. The energy absorbing assembly also includes a deformable member configured to be positioned concentrically around the shaft of the anchor. The deformable member is configured to be retained between the first side of the attachment component and the head of the anchor.

The invention relates to device for providing a safety for passengers and to devices, providing the passenger comfort. There are disclosed variants of load limiter accomplishment for a restraint a passenger in a vehicle, which have a possibility to hold the preliminarily given force. The invention concerns a multi-passenger modular array oftiered passenger supports, having a several levels, means for attaching the modules, locking devices, attaching the modules to the vehicle floor, a drive mechanism for seats in the module, a mechanism for protecting the head of passenger, which is positioned on the seat. The means for providing the passenger comfort head are characterized by the position of steps in the modules, providing a sufficient space for free positioning the legs of the passenger in the upper and lower modules and in the zone of passage between rows. There are also disclosed the presence and position of the bins for storing packages, a construction of armrest and means for lighting, air conditioning, for information drop on the screen and for supplying an oxygen, in necessary.

The invention relates to device for providing a safety for passengers and to devices, providing the passenger comfort. There are disclosed variants of load limiter accomplishment for a restraint a passenger in a vehicle, which have a possibility to hold the preliminarily given force. The invention concerns a multi-passenger modular array oftiered passenger supports, having a several levels, means for attaching the modules, locking devices, attaching the modules to the vehicle floor, a drive mechanism for seats in the module, a mechanism for protecting the head of passenger, which is positioned on the seat. The means for providing the passenger comfort head are characterized by the position of steps in the modules, providing a sufficient space for free positioning the legs of the passenger in the upper and lower modules and in the zone of passage between rows. There are also disclosed the presence and position of the bins for storing packages, a construction of armrest and means for lighting, air conditioning, for information drop on the screen and for supplying an oxygen, in necessary.

A singular energy absorber and an offset pilot seat including the same. The pilot seat includes a seat base, a seat bucket positioned laterally offset relative to a centerline of the seat base, a singular motion controller movably coupling the seat bucket to the seat base, wherein the singular motion controller is centered relative to the seat bucket and laterally offset relative to the seat base, and the singular energy absorber associated with the singular motion controller, the singular energy absorber operative to maintain relative positions of components of the singular motion controller during normal use of the rotorcraft pilot seat and allow relative motion between the components of the singular motion controller during a dynamic event.

A singular energy absorber and an offset pilot seat including the same. The pilot seat includes a seat base, a seat bucket positioned laterally offset relative to a centerline of the seat base, a singular motion controller movably coupling the seat bucket to the seat base, wherein the singular motion controller is centered relative to the seat bucket and laterally offset relative to the seat base, and the singular energy absorber associated with the singular motion controller, the singular energy absorber operative to maintain relative positions of components of the singular motion controller during normal use of the rotorcraft pilot seat and allow relative motion between the components of the singular motion controller during a dynamic event.

A compact aircraft cabin crew attendant seat includes a seat back portion, a shell that encloses the seat back portion, a head rest portion mounted to a top portion of the seat back portion, and a seat portion or squab. The seat portion includes a hinge that is slidably attached within a vertical slot in the shell, allowing the seat portion to be folded down in an open position of the crew attendant seat for use. The seat portion hinge moves vertically between an upper position in the compact closed position and a lower position in the open position. A major portion of the crew attendant seat is formed from high strength carbon fiber reinforced composite to reduces weight. A vertical shock absorption system is configured to absorb energy during a crash landing.

A compact aircraft cabin crew attendant seat includes a seat back portion, a shell that encloses the seat back portion, a head rest portion mounted to a top portion of the seat back portion, and a seat portion or squab. The seat portion includes a hinge that is slidably attached within a vertical slot in the shell, allowing the seat portion to be folded down in an open position of the crew attendant seat for use. The seat portion hinge moves vertically between an upper position in the compact closed position and a lower position in the open position. A major portion of the crew attendant seat is formed from high strength carbon fiber reinforced composite to reduces weight. A vertical shock absorption system is configured to absorb energy during a crash landing.