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Utilizing Non-Contact Stress Measurement System (NSMS) as a Health MonitorContinuously monitor all 156 blades throughout the entire operating envelope without adversely affecting tunnel conditions or compromise compressor shell integrity, Calculate dynamic response and identify the frequency/mode to determine individual blade deflection amplitudes, natural frequencies, phase, and damping (Q), Log static deflection to build a database of deflection values at certain compressor conditions to use as basis for real-time online Blade Stack monitor, Monitor for stall, surge, flutter, and blade damage, Operate with limited user input, low maintenance cost, safe illumination of probes, easy probe replacement, and require little or no access to compressor.
Document ID
20110015015
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Hayes, Terry
(Aerospace Testing Alliance Arnold AFB, TN, United States)
Hayes, Bryan
(Aerospace Testing Alliance Arnold AFB, TN, United States)
Bynum, Ken
(Aerospace Testing Alliance Arnold AFB, TN, United States)
Date Acquired
August 25, 2013
Publication Date
June 20, 2011
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
ARC-E-DAA-TN3765
Report Number: ARC-E-DAA-TN3765
Meeting Information
Meeting: 2nd Tip Timing Workshop
Location: Saint Louis, MO
Country: United States
Start Date: June 20, 2011
End Date: June 22, 2011
Sponsors: Air Force Materiel Command
Funding Number(s)
CONTRACT_GRANT: NNA10DE39I
Distribution Limits
Public
Copyright
Public Use Permitted.
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