Hybrid wing assembly

Details Hybrid wing assembly Hybrid wing assembly

1988-02-16

1990-02-20

Peters, Jr., Joseph F.

Aeronautics and astronautics

Composite aircraft

244152, 244 45R, 244902, B64C 3908

Patent

active

049019457

ABSTRACT:
A hybrid wing assembly is made up of a load supporting center frame with laterally outwardly extending, articulated, wing sections. A parafoil is attached to the wing sections by flexible lines in flight, and rigid rods hold the parafoil in spaced relation to the wing at rest. Control lines extend from the parafoil to the user for controlling the assembly.

REFERENCES:
patent: 3995799 (1976-12-01), Bartolini
patent: 4417707 (1983-11-01), Leong
patent: 4424945 (1984-01-01), Dell
patent: 4596368 (1986-06-01), Schmittle
patent: 4601443 (1986-07-01), Jones
patent: 4623108 (1986-11-01), Musick
patent: 4634080 (1987-01-01), McNally

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