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Evaluation of a Microwave Blade Tip Clearance Sensor for Propulsion Health MonitoringThe NASA Glenn Research Center has investigated a microwave blade tip clearance system for the structural health monitoring of gas turbine engines. This presentation describes the sensors and the experiments that have been conducted to evaluate their performance along with future plans for their use on an engine ground test.
Document ID
20140000477
Document Type
Presentation
Authors
Woike, Mark R. (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
January 29, 2014
Publication Date
May 13, 2013
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-9387
Meeting Information
ISA International Instrumentation Symposium(Cleveland, OH)
Funding Number(s)
WBS: WBS 284848.02.04.03.02.01.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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