Helicopter Gearbox Bearing Blind Fault Identification Using a Range of Analysis Techniques-Reference-Cited by-同舟云学术

Helicopter Gearbox Bearing Blind Fault Identification Using a Range of Analysis Techniques

Published: Issue: Volume: Page:724-737
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Container-title:Engineering Asset Management
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Author:

Sawalhi N,Randall R. B

Publisher

Springer London

Link

http://link.springer.com/content/pdf/10.1007/978-1-84628-814-2_77.pdf

Reference18 articles.

1. Forrester, BD. (1991) Time-Frequency Domain Analysis Of Helicopter Transmission Vibration, Department of Defence, Aeronautical Research laboratory, Propulsion Report 180.

2. McFadden, PD & Smith, JD. (1985) An explanation for the asymmetry of the modulation sidebands about the tooth meshing frequency in epicyclic gear vibration, Proceedings of the Institution of Mechanical engineers, 199(C1), pp65–70

3. Lewicki D. & Coy J. (1987) Vibration characteristics of OH58a helicopter main rotor transmission, NASA technical paper, NASA TP-2705/AVSCOM TR 86-C-42.

4. McFadden PD & Howard IM. (1999) The detection of seeded faults in an epicyclic gearbox by signal averaging of the vibration, Department of Defence, Aeronautical Research laboratory, Propulsion Report 183.

5. Huff E & Tumer I. (2003) Using Triaxial Accelerometer Data For vibration Monitoring Of Helicopter Gearboxes, Journal of vibration and acoustics, volume 128(4), pp120–128.

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