Autogyro having blade tip jets

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

Patent

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Details

416 22, B64C 2702

Patent

active

040109194

ABSTRACT:
This invention relates to an improved design for autogyros. It involves a more desirable layout of cockpit/engine placement than heretofore thought of. It provides for improved efficiency, visibility and balance and solves some of the problems of recent autogyros. Further, it provides for an improved and simplified rotor spin up mechanism.

REFERENCES:
patent: 2027592 (1936-01-01), Hoffman et al.
patent: 2965178 (1960-12-01), Peterson
patent: 3225537 (1965-12-01), Parsons
patent: 3699771 (1972-10-01), Chelminski
patent: 3720060 (1973-03-01), Davies et al.
patent: 3870251 (1975-03-01), Breuner

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