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Aircraft Wheel Design and Proving

S.M. Smith (Chief Stressman, Dunlop Ltd, Aviation Division, Coventry)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 July 1986

158

Abstract

Aircraft manufacturers now demand wheels which are not only light but also have a long life capability. A typical civil aircraft project such as the Boeing 757, requires a fully approved wheel with a demonstrated life of 50,000 roll miles which equates to approximately 10,000 landings.

Citation

Smith, S.M. (1986), "Aircraft Wheel Design and Proving", Aircraft Engineering and Aerospace Technology, Vol. 58 No. 7, pp. 8-13. https://doi.org/10.1108/eb036311

Publisher

:

MCB UP Ltd

Copyright © 1986, MCB UP Limited

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