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Aircraft Engine Gas Path Diagnostic Methods: Public Benchmarking ResultsRecent technology reviews have identified the need for objective assessments of aircraft engine health management (EHM) technologies. To help address this issue, a gas path diagnostic benchmark problem has been created and made publicly available. This software tool, referred to as the Propulsion Diagnostic Method Evaluation Strategy (ProDiMES), has been constructed based on feedback provided by the aircraft EHM community. It provides a standard benchmark problem enabling users to develop, evaluate and compare diagnostic methods. This paper will present an overview of ProDiMES along with a description of four gas path diagnostic methods developed and applied to the problem. These methods, which include analytical and empirical diagnostic techniques, will be described and associated blind-test-case metric results will be presented and compared. Lessons learned along with recommendations for improving the public benchmarking processes will also be presented and discussed.
Document ID
20140003941
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Simon, Donald L.
(NASA Glenn Research Center Cleveland, OH, United States)
Borguet, Sebastien
(Liege Univ. Belgium)
Leonard, Olivier
(Liege Univ. Belgium)
Zhang, Xiaodong (Frank)
(Wright State Univ. Dayton, OH, United States)
Date Acquired
April 28, 2014
Publication Date
November 1, 2013
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-18768
GT2013-95077
NASA/TM-2013-218082
Report Number: E-18768
Report Number: GT2013-95077
Report Number: NASA/TM-2013-218082
Meeting Information
Meeting: American Society of Mechanical Engineers (ASME) Turbo Expo 2013
Location: San Antonio Texas
Country: United States
Start Date: June 3, 2013
End Date: June 7, 2013
Sponsors: American Society of Mechanical Engineers
Funding Number(s)
CONTRACT_GRANT: WBS 284848.02.04.03.02.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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