Internal wing aircraft

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

Patent

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Details

244 121, 244 36, B64C 3900

Patent

active

045680426

ABSTRACT:
Lift for an aircraft is provided by forming a longitudinal lifting duct therethrough, said lifting duct having a substantially planar roof and a longitudinally cambered floor. When the aircraft is driven forwardly, a stream of air enters and passes through the lifting duct and the contouring of the floor of the lifting duct give rise to a pressure gradient in the air stream which result in a higher pressure on the roof of the lifting duct than on the floor thereof so that the pressure difference provides lift for the aircraft.

REFERENCES:
patent: 2380535 (1945-07-01), McDevitt
patent: 2553443 (1951-05-01), Davis
patent: 2928238 (1960-03-01), Hawkins
patent: 3053477 (1962-09-01), Reiniger
patent: 3154267 (1964-10-01), Grant
patent: 3596852 (1971-08-01), Wakefield
patent: 3785593 (1974-01-01), Von Ohain et al.
patent: 4296900 (1981-10-01), Krall

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