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Engine Performance and Health Monitoring Models Using Steady State and Transient Prediction MethodsThis lecture note discusses the role of computer modelling in the design, development, and validation of a performance monitoring system. The basic requirements of an engine health monitoring system are discussed in the context of the user environment. A form of model based on stage characteristics provides the basis for describing engine measurements. Faults are modelled in accordance with empirical data obtained from tests conducted at the stage level. The model is used to investigate various parameters that provide unambiguous identification of the fault in question. Fault libraries have been developed for field use.
Document ID
19920019224
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
B D MacIsaac
(gasTOPS Ottawa, Ontario, Canada)
Date Acquired
August 15, 2013
Publication Date
May 1, 1992
Publication Information
Publication: Steady and Transient Performance Prediction of Gas Turbine Engines
Publisher: Advisory Group for Aerospace Research and Development (AGARD)
ISBN: 928350674X
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: AGARD Lecture Series 183
Location: Chatillon / Bagneaux
Country: FR
Start Date: June 11, 1992
End Date: June 12, 1992
Sponsors: North Atlantic Treaty Organization
Accession Number
92N28467
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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