Light aircraft for short-distance takeoff and landing

Details Light aircraft for short-distance takeoff and landing Light aircraft for short-distance takeoff and landing

1988-11-04

1989-12-26

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft, heavier-than-air

Airplanes, weight diminished by bouyant gas

244 25, 244 92, B64B 120, B64C 134

Patent

active

048892971

ABSTRACT:
A light aircraft for short distance takeoff and landing includes an airplane having a propeller provided on a rear pedestal thereof for producing vertical propulsion and an airship having a propeller provided on a rear pedestal thereof for producing vertical propulsion and also having a flight attitude sensor provided within an operating compartment thereof. The flight attitude sensor is always directed in the vertical direction, detects forward and rearward inclinations of the airship, and transmits signals corresponding to the inclinations to the two propellers, thereby rotating the two propellers to produce downward or upward propulsion to maintain the aircraft at the normal horizontal attitude at all times.

REFERENCES:
patent: 1418522 (1922-06-01), Boyle
patent: 1637133 (1927-07-01), Tew
patent: 1657955 (1928-01-01), Bylek
patent: 1901173 (1933-03-01), Kuhn
patent: 3807661 (1974-04-01), Ikeda

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