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U.S. Patent Specifications

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 July 1936

Abstract

1. In a combination in an aeroplane shock absorber, a liquid damping means for absorbing the initial shock of landing and a resilient frictional device for resiliently supporting the load and effective to resiliently support the load only alter initial shock of landing has been absorbed by said liquid damping means.

Citation

(1936), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 8 No. 7, pp. 208-208. https://doi.org/10.1108/eb030076

Publisher

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MCB UP Ltd

Copyright © 1936, MCB UP Limited