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
2023-12-07
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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