Abstract:
A passenger seat (100) that includes at least one back rest frame (191-194) with at least one through-hole, at least one lateral structural member (101,102) that is perpendicular to the at least one back rest frame (191-194) and is disposed in the at least one through-hole, and at least one floor attachment frame (195,196) with at least one through-hole that is coaxial with the at least one through-hole of the at least one back rest frame (191-194). Each lateral structural member include an internal composite tube (101,102) that extends a full lateral width of the passenger seat and a plurality of outer tubes (151-162) disposed on an outer surface of the internal composite tube.
Abstract:
Follow-up performance to respiratory movements is made higher than that of the prior art without obstructing movements of the pelvis of a person. A configuration is adopted that a cushioning member arrangement frame for a seat back 34, 140 and a cushioning member arrangement frame for a seat cushion are displaced according to load fluctuation to a cushioning member for a seat back 40, 150 or a cushioning member for a seat cushion 20. That is, such a configuration is adopted that the cushioning member arrangement frame for a seat back 34, 140 or the cushioning member for a seat cushion 20 not only moves according to load fluctuation but also frames themselves supporting them move via tension structure members spread over the frames (a cushioning member for a seat back and a cushioning member for a seat cushion). Accordingly, when a person lays his/her pelvis at his/her sitting position for deep breathing, the cushioning member arrangement frame for a seat back is displaced to push the vicinity of an upper portion of the cushioning member for a seat back, so that the vicinity of a lower portion of the cushioning member for a seat back is pushed forward to enrich support of the sacrum of the person.
Abstract:
Describes are passenger seats including a seat pan assembly with a reclining mechanism, a seat back pivotally coupled to the aft end of the seat pan assembly, and a lumbar mechanism coupled to the seat back and/or the seat pan assembly. As examples, the seat pan assembly includes at least one track having a reclining path and a sleeper path, and a sleeper selection control configured to pull a diverter into a position substantially blocking the opening to the reclining path and to push the diverter into a position substantially blocking the opening to the sleeper path. In certain cases, the seat pan assembly also includes a tilting mechanism with a fixed component and a variable component adjustably engaged with each other.
Abstract:
A structural element that includes a central part formed of a fibrous material suspended in a thermoplastic matrix and at least one side part formed of a fibrous material suspended in a thermoplastic matrix and having at least one void therein. The central part and the at least one side part are bonded together while in a heated thermoplastic state to form a single, integral structure characterized by the absence of discontinuity across the bond plane of the structure.
Abstract:
A pod assembly for use in an aircraft that includes a seat with a seat bottom and a seat back, a shell that at least partially surrounds the seat, and a bed associated with the shell. The bed is movable between a stowed position and a deployed position where the bed is generally flat. The bed is supported by the shell in the deployed position.
Abstract:
A three dimensional lattice panel structure having a multitude of mutually offset holes formed in a respective top and bottom of the panel and intersecting to form voids with interspersed support posts interconnecting the top and bottom of the panel in areas not encompassed by the mutually offset holes.
Abstract:
The invention relates to a hybrid tube (22), in particular for an aircraft seat structure S, said structure comprising ribs (10) intended to receive the hybrid tube (22), said hybrid tube (22) including a monolithic carbon tube (24) and at least one sleeve (26) made from a ductile material and connected to the carbon tube by means of gluing, shrink-fitting or over-moulding.