Expandable fuel cell

Aeronautics and astronautics – Aircraft structure – Fuel supply

Patent

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244135R, B64D 3700

Patent

active

059276517

ABSTRACT:
An expandable fuel cell (72) for an aircraft (70) has a flexible structure (126) having a perimeter (124) attached to an airframe of the aircraft (70). The flexible structure (126) has an empty position, in which the flexible structure (126) approximately conforms to a moldline (76) of the aircraft (70), and a full position, in which the flexible structure (126) forms a smooth curvilinear protrusion from the moldline (76) of the aircraft (70). A fuel bladder (152) is positioned between the flexible structure (126) and the airframe.

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patent: 4948070 (1990-08-01), Lyman
patent: 5222699 (1993-06-01), Albach et al.
patent: 5467889 (1995-11-01), Ashton et al.
patent: 5803405 (1998-09-01), Ellis et al.
patent: 5810291 (1998-09-01), Geiger et al.

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