The invention relates to a seat floor comprising a seat floor structure (11) comprising: a first longitudinal member (12.1) having a front end portion (13.1) and a rear end portion (14.1); -a second longitudinal member (12.2) having a front end portion (13.2) and a rear end portion (14.2); -a front cross member (15.1) mechanically interconnecting the front end portion (13.1) of the first longitudinal member (12.1) and the front end portion (13.2) of the second longitudinal member (12.2); and-a rear cross member (15.2) mechanically interconnecting the rear end portion (14.1) of the first longitudinal member (12.1) and the rear end portion (14.2) of the second longitudinal member (12.2); the seat floor structure (11) further comprises a kinetic energy absorbing tube (27) extending between the first longitudinal member (12.1) and the second longitudinal member (12.2).
本发明涉及一种座椅底板,包括座椅底板结构(11),所述座椅底板结构包括:-具有前端部分(13.1)和后端部分(14.1)的第一纵向构件(12.1);-具有前端部分(13.2)和后端部分(14.2)的第二纵向构件(12.2);-前横向构件(15.1),所述前横向构件机械地互连所述第一纵向构件(12.1)的前端部分(13.1)和所述第二纵向构件(12.2)的前端部分(13.2);以及-后横向构件(15.2),所述后横向构件机械地互连所述第一纵向构件(12.1)的后端部(14.1)和所述第二纵向构件(12.2)的后端部分(14.2);所述座椅底板结构(11)还包括在所述第一纵向构件(12.1)和所述第二纵向构件(12.2)之间延伸的动能吸收管(27)。
Seating surface with kinetic energy absorbing tubes for seats, in particular aircraft seats
用于座椅特别是飞机座椅的具有动能吸收管的就座表面
2024-01-09
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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