Cycloidal VTOL UAV

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

Reexamination Certificate

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Details

C244S019000, C244S020000, C244S012200, C244S02300R

Reexamination Certificate

active

06932296

ABSTRACT:
A system and method for moving an aerial vehicle along a flight path includes rotatable hubs mounted on opposite sides of the vehicle. Elongated airfoils are mounted on the hubs parallel to a common hub axis for rotation about the hub axis on a blade path. Each airfoil defines a chord line and the system includes a gear assembly changeable, during hub rotation, between a first modality wherein airfoil chord lines remain tangential to the blade path (curtate flight), and a second modality wherein airfoil chord lines remain parallel to the flight path of the vehicle (prolate flight). Also, rotation of the hub can be stopped and the airfoils used for fixed wing flight.

REFERENCES:
patent: 1264152 (1918-04-01), Briggs
patent: 1334707 (1920-03-01), Martin
patent: 1795501 (1931-03-01), Platt
patent: 1803498 (1931-05-01), Chilton
patent: 2369832 (1945-02-01), Klose
patent: 2507657 (1950-05-01), Wiessler
patent: 3801047 (1974-04-01), Dell'Aquila
patent: 4194707 (1980-03-01), Sharpe
patent: 4417708 (1983-11-01), Negri
patent: 5100080 (1992-03-01), Servanty
patent: 5265827 (1993-11-01), Gerhardt
patent: 5918832 (1999-07-01), Zerweckh

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