Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1993-11-23
1995-12-12
Barefoot, Galen L.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
244 90R, 244901, 244904, B64C 356
Patent
active
054742579
ABSTRACT:
The deployable wing of the present invention comprises an internal structure having diverging leading edge spars attached to a keel spar and cross spars to form a delta wing configuration. This internal structure is enclosed within a volume defined by a fabric sail having an upper section, a lower section, and fabric ribs disposed therebetween. This fabric sail volume is internally pressurized through a ram air intake at the nose stagnation point. This deployable wing can be folded and deployed in the air.
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Dam Dennis Van
Fisher Jeffrey A.
Miller Edward V.
Barefoot Galen L.
USBI Co.
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