An aircraft cushion includes a lower portion, upper portion, and forward portion of foam. The lower portion is configured to be located by a forward frame element (e.g., tube) and to be supported by the forward frame element and a seat diaphragm (e.g., stretched fabric). The upper portion and forward portion are softer for user comfort. The lower portion, using a shape of the foam (e.g., structural foam), may removably snap onto the forward frame element, and rotate down into place for ease of installation.
HYBRID BOTTOM SEAT CUSHION
07.12.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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