Method and apparatus for deploying a wing

Details Method and apparatus for deploying a wing Method and apparatus for deploying a wing

B - Operations, Transporting

64

D

B64D 19/00 (2006.01) B64C 3/56 (2006.01) B64C 31/028 (2006.01)

Patent

CA 2188851

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. Alps deployable wing can be folded, extracted from an aircraft and deployed in the air.

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