A seat pan can include a seat pan structure. The seat pan structure can include a first longitudinal member having a front end portion and a rear end portion, a second longitudinal member having a front end portion and a rear end portion, a front cross member mechanically interconnecting the front end portion of the first longitudinal member and the front end portion of the second longitudinal member; and a rear cross member mechanically interconnecting the rear end portion of the first longitudinal member and the rear end portion of the second longitudinal member. The seat pan structure can further include a kinetic energy absorbing tube extending between the first longitudinal member and the second longitudinal member.
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
10.04.2024
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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