Unmanned remotely piloted aircraft

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

Patent

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Details

244 1723, 244120, 416204R, B64C 2710

Patent

active

044783795

ABSTRACT:
An unmanned aircraft of the remotely piloted type that is characterized by its configuration and outline using rigid counter rotating propellers, positioned substantially at the height of its center of mass or slightly below to allow producing a sufficiently large control moment to use a tether line for landing the aircraft and to allow using two substantially spheroidal surfaces at the top and bottom respectively rather than a single one relatively larger and more detectable surface as when the propellers are at the top.

REFERENCES:
patent: 2847173 (1958-08-01), McCarty, Jr.
patent: 3357656 (1967-12-01), Peterson
patent: 3801050 (1974-04-01), Stone
patent: 4123018 (1978-10-01), Montaigu
patent: 4163535 (1979-08-01), Austin
patent: 4302155 (1981-11-01), Grimes
Jane's All the World Aircraft, editor J. Taylor, 1977-1978, p. 644, "Canadair CL-227."

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