Super-short take off and landing apparatus

Details Super-short take off and landing apparatus Super-short take off and landing apparatus

1975-06-24

1976-12-07

Blix, Trygve M.

Aeronautics and astronautics

Aircraft, heavier-than-air

Airplane and fluid sustained

244 48, 244 55, 244 60, B64C 1512

Patent

active

039957942

ABSTRACT:
An aircraft provided with airfoils of the non-rotating type that are configured and arranged to provide greater lift while at the same time offering stable flight at ultra-low airspeeds. The airfoils are arranged as a biplane and consist of a fixed wing and a movable wing which are designed so as to permit a much steeper takeoff and landing angle as well as offering more efficient flight at higher speeds with greater inherent safety.

REFERENCES:
patent: R18181 (1931-09-01), Stelzer
patent: 1867963 (1932-07-01), Blahnik
patent: 2015150 (1935-09-01), Maxwell
patent: 3136499 (1964-06-01), Kessler
patent: 3477664 (1969-11-01), Jones

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