Portable helicopter

Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes

Patent

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Details

244 4A, 244 8, 244 83F, 416142, B64C 2750, B64C 2752

Patent

active

040712060

ABSTRACT:
A basic lightweight helicopter frame is strapped to the body of a pilot and includes vertical side bars interconnected above the pilot's head to rotatably support a bladed rotor assembly and carry a rearwardly extending tail rotor assembly. The lower ends of the side bars carry fuel tanks from which rocket engines at the tips of the rotor blades draw fuel. A control assembly is supported at the upper end of the frame and extends forwardly therefrom for easy access by the pilot. The aircraft includes an attachable landing gear and an attachable pusher blade and engine assembly which can be used when desired.

REFERENCES:
patent: D180311 (1951-05-01), Ziegler
patent: 2601463 (1952-06-01), Stanley
patent: 2745498 (1956-05-01), Nagler
patent: 2763447 (1956-09-01), Carrau
patent: 2905410 (1959-09-01), Bensen
patent: 3029047 (1962-04-01), Jacobsen et al.
patent: 3042347 (1962-07-01), Halsey
patent: 3220670 (1965-11-01), Fuller
patent: 3586263 (1971-06-01), Payne
patent: 3750982 (1973-08-01), Gear
"Cafe Racer's Choice", Cycle World, p. 23, July 1974.
"1948 Rotary Wing Pictoral Review", American Helicopter pp. 10-18, Dec. 1948.

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