Implanted component faults and their effects on gas turbine engine performance

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Proceedings titleProceedings of the ASME Turbo Expo
ConferenceASME 1991 International Gas Turbine and Aeroengine Congress and Exposition, GT 1991, 3 June 1991 through 6 June 1991
SubjectAircraft engines; Aircraft propulsion; Engines; Marine engineering; Marine engines; Turbine components; Canadian department of national defence; Component faults; Engine components; Fault identifications; National Research Council of Canada; Performance characteristics; Unscheduled maintenance; Gas turbines
AbstractUnder the sponsorship of the Canadian Department of National Defence, the Engine Laboratory of the National Research Council of Canada (NRCC) has established a program for the evaluation of component deterioration on gas turbine engine performance. The effort is aimed at investigating the effects of typical in-service faults on the performance characteristics of each individual engine component. The objective of the program is the development of a generalized fault library which will be used with fault identification techniques in the field, to reduce unscheduled maintenance. Copyright © 1991 by ASME.
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AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Peer reviewedYes
NPARC number21275135
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Record identifierab8f4f10-7170-4605-b305-78d8756f0840
Record created2015-05-11
Record modified2016-05-09
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