An aircraft cushion includes a lower portion (1006), upper portion (1004), and forward portion (1008) of foam. The lower portion (1006) 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 (100) (e.g., stretched fabric). The upper portion (1004) and forward portion (1008) are softer for user comfort. The lower portion (1006), 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
HYBRIDES UNTERSITZPOLSTER
COUSSIN DE SIÈGE INFÉRIEUR HYBRIDE
2025-02-26
Patent
Electronic Resource
English
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