The present invention relates to a seat pan having a seat pan structure that includes a first longitudinal member, a second longitudinal member, a front cross member and a rear cross member, wherein:each longitudinal member further includes a distal portion extending between the front end portion and the rear end portion;a gap between the first longitudinal member and the second longitudinal member measured between the distal portions is greater than a gap between the first longitudinal member and the second longitudinal member measured between the front end portions and/or a gap between the first longitudinal member and the second longitudinal member measured between the rear end portions.
ASSISE DE SIEGE, NOTAMMENT DE SIEGE D'AVION, MUNIE D'UNE ZONE DE DEGAGEMENT POUR LE BASSIN
SEAT PAN, IN PARTICULAR FOR AN AIRCRAFT SEAT, PROVIDED WITH A CLEARANCE ZONE FOR THE PELVIS
SITZSCHALE, INSBESONDERE FÜR EINEN FLUGZEUGSITZ, MIT EINEM BECKENABSTANDSBEREICH
2024-04-10
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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