Fault Diagnosis of Gas Turbine Engines From Transient Data

[+] Author and Article Information
G. L. Merrington

Aeronautical Research Laboratory, Defence Science and Technology Organisation, Melbourne, Australia

J. Eng. Gas Turbines Power 111(2), 237-243 (Apr 01, 1989) (7 pages) doi:10.1115/1.3240242 History: Received September 24, 1987; Online October 15, 2009


The desirability of being able to extract relevant fault diagnostic information from transient gas turbine data records is discussed. A method is outlined for estimating the effects of unmeasured fault parameters from input/output measurements. The resultant sensitivity of the technique depends on the sampling rate and the measurement noise.

Copyright © 1989 by ASME
Your Session has timed out. Please sign back in to continue.





Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In