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Vibrations in helicopters ‐ reduction and monitoring

Terry Ford

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 April 1997

1040

Abstract

Describes the Westland active control of structural response (ACSR) technique for reducing and alleviating vibration. Examines a refined coupled rotor/flexible fuselage model based on the ACSR approach. Reports on vibration health monitoring (VHM) which has been developed by Westland and details further work which is continuing in this field.

Keywords

Citation

Ford, T. (1997), "Vibrations in helicopters ‐ reduction and monitoring", Aircraft Engineering and Aerospace Technology, Vol. 69 No. 2, pp. 119-125. https://doi.org/10.1108/00022669710164448

Publisher

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MCB UP Ltd

Copyright © 1997, MCB UP Limited

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