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U.S. Patent Specifications

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 June 1939

19

Abstract

The combination with an engine cowl having a front entrance opening, of a disc disposed therein, swinging links guiding the rim of said disc for approximately helical movement, and control means for effecting said movement.

Citation

(1939), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 11 No. 6, pp. 258-258. https://doi.org/10.1108/eb030506

Publisher

:

MCB UP Ltd

Copyright © 1939, MCB UP Limited

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