Vertical take-off and landing aircraft

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

Patent

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Details

244118R, 244130, 244207, 244209, 244137R, 416 20R, 416142, B64C 2730, B64C 2750

Patent

active

041098854

ABSTRACT:
A vertical take-off and landing aircraft features an improved tail-lifting rotor and rotor directional controls. A new type of suction pressure jet-mechanical-flap rotor blade with a higher coefficient of lift is employed. The aircraft has a mechanism for loading and unloading passengers and a more efficient method of handling baggage and cargo. A much more efficient utilization of space in the fuselage is achieved through a reduced height passenger space and overhead rotor storage compartment.

REFERENCES:
patent: 2376834 (1945-05-01), Thompson
patent: 2694537 (1954-11-01), Reichert
patent: 2751168 (1956-06-01), Stalker
patent: 3582021 (1971-06-01), Pender
patent: 3604661 (1971-09-01), Mayer
patent: 3762667 (1973-10-01), Pender
patent: 3884433 (1975-05-01), Alexander
patent: 3887146 (1975-06-01), Bright

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