Parameter Selection for Multiple Fault Diagnostics of Gas Turbine Engines

[+] Author and Article Information
L. A. Urban

Hamilton Standard Division of United Aircraft Corp., Windsor Locks, Conn.

J. Eng. Power 97(2), 225-230 (Apr 01, 1975) (6 pages) doi:10.1115/1.3445969 History: Received November 27, 1973; Online July 14, 2010


An introduction to the fundamentals of turbine engine multiple fault diagnosis and its relationship to engine parameter selection and measurement requirements is presented. The influence of the type (thermodynamic cycle) of the engine to be diagnosed, and the nature of its expected problems, on the required parameters and the attendant measurement repeatability requirements are discussed.

Copyright © 1975 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