Powered airfoil canopy aircraft

Aeronautics and astronautics – Aircraft – heavier-than-air – Airplane sustained

Patent

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Details

244902, 244903, 244 69, B64C 3900

Patent

active

049346300

ABSTRACT:
Load lines connect chordwise spaced portions of a ram air inflated, airfoil canopy to spaced anchors connected to a pilot supporting vehicle frame on which a forward thrust producing unit is removably mounted. The geometry of the assembled aircraft enhances take-off inflation of the canopy, establishes a stable flight frame when airborne, and enables simple engine throttle control of the thrust producing unit to regulate climb, descent and level flight. Common control is applied for both ground steering of the vehicle frame and air-borne steering of the canopy.

REFERENCES:
patent: 1174679 (1916-03-01), Carroll
patent: 1431244 (1922-10-01), Mendel
patent: 1523386 (1925-01-01), Baer
patent: 2006805 (1935-07-01), Gwinn, Jr.
patent: 2938679 (1960-05-01), Walker, Jr.
patent: 3931943 (1976-01-01), Westergren et al.
patent: 4071206 (1978-01-01), Magill
patent: 4375280 (1983-03-01), Nicolaides
patent: 4426049 (1984-01-01), Stewart
Nicolaides, "Parafoil Powered Flight Performance" AFFDL-TR-72-23, 1972.

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