Powered hang glider with reduction drive

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

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244 54, 244 55, 244DIG1, B64C 116

Patent

active

042628636

ABSTRACT:
A foot-launched and foot-landed hang glider is powered by an internal combustion two-cycle engine drivingly connected through a reduction-drive unit to a large relatively slow-moving propeller. A reduction mount, so referred to because it couples the reduction-drive unit closely to the engine, allows the engine to rotate a large propeller relatively slowly, thus providing more thrust at near-stalling flight conditions. The hang glider, thus powered, also obviates the necessity of being launched from the edge of a precipice and permits flight which is not predicated on the fortuitous selection of favorable air currents.

REFERENCES:
patent: D243594 (1977-03-01), Koch
patent: 591211 (1897-10-01), Daberer
patent: 983868 (1911-02-01), Bellville
patent: 991620 (1911-05-01), Hughes
patent: 1011604 (1911-12-01), French
patent: 1175307 (1916-03-01), Schroeder
patent: 1189610 (1916-07-01), Morris
patent: 1443368 (1923-01-01), Lamblin
patent: 2234758 (1941-03-01), Goldberg
patent: 2395143 (1946-02-01), Prewitt
patent: 3195837 (1965-07-01), Alvarez-Calderon
patent: 3744180 (1973-07-01), Mabuchi
patent: 4005673 (1977-02-01), Carrero
patent: 4067515 (1978-01-01), Searle
Glider Rider, 1977, p. 14.
Poynter, "Hang Gliding", pp. 138, 190-191, 1976.

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