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U.S. Patent Specifications

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 November 1954

Abstract

An aircraft comprising in combination, a fuselage having an empennage and forward propulsive means, a disk‐shaped aerofoil mounted on said fuselage for universal inclination thereon, means for rotating said aerofoil, a plurality of rotary wing blades mounted for rotation with said disk‐shaped aerofoil, and means for retracting said blades into said aerofoil and for extending said blades outside of said aerofoil.

Citation

(1954), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 26 No. 11, pp. 400-400. https://doi.org/10.1108/eb032498

Publisher

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MCB UP Ltd

Copyright © 1954, MCB UP Limited