Deflected slipstream vertical lift airplane structure

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

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Details

244 23D, 244 55, 244 45R, B64C 2900

Patent

active

053740106

ABSTRACT:
A vertical lift and short takeoff airplane achieving a powered lift which is generated by deflecting downward on the order of nearly 90.degree. the slipstream from the driven propellors by means of the wing flap system of the airplane.

REFERENCES:
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patent: 1704831 (1929-03-01), Herbert
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patent: 2910254 (1959-10-01), Razak
patent: 3096043 (1963-07-01), Labussiere
patent: 3136499 (1964-06-01), Kessler
patent: 4709880 (1987-12-01), Bradfield et al.
patent: 5115996 (1992-05-01), Moller

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