The present invention relates to a seat pan comprising a seat pan structure (11) that includes: - 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); - said seat pan structure (11) further comprising a kinetic energy absorbing tube (27) extending between the first longitudinal member (12.1) and the second longitudinal member (12.2).
ASSISE DE SIEGE, NOTAMMENT DE SIEGE D'AVION, MUNIE D'UN TUBE ABSORBEUR D'ENERGIE CINETIQUE
SEAT PAN, IN PARTICULAR FOR AN AIRCRAFT SEAT, PROVIDED WITH A KINETIC ENERGY ABSORBING TUBE
SITZSCHALE, INSBESONDERE FÜR EINEN FLUGZEUGSITZ, MIT EINEM ROHR ZUR ABSORPTION KINETISCHER ENERGIE
2024-04-10
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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