Hybrid wing assembly

B - Operations – Transporting – 64 – C

Patent

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Details

244/14, 244/40

B64C 39/08 (2006.01) B64C 31/02 (2006.01) B64C 31/036 (2006.01) B64D 17/02 (2006.01)

Patent

CA 1322549

ABSTRACT OF THE DISCLOSURE A hybrid wing assembly having an articulated wing and a parafoil attached to said wing by flexible lines so that during flight, the parafoil is above and suspends the wing assembly. Rods extend upwardly from the wing and support the parafoil above the wing in operating position at rest.

591079

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