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U.S. Patent Specifications

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 March 1940

Abstract

In an aircraft sustaining rotor, a pivotal blade mounting including relatively rotatable blade mounting parts subject to axial load, a torsionally yieldable member interconnecting said parts to take said axial load, and a thrust bearing interposed in series in the connection of said member with said parts, the thrust bearing having a higher frictional moment than the resistance to torsional yielding of said member within a limited range of angular displacement of the blade mounting parts when under normal flight loading.

Citation

(1940), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 12 No. 3, pp. 92-92. https://doi.org/10.1108/eb030625

Publisher

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MCB UP Ltd

Copyright © 1940, MCB UP Limited