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Damage Assessment of Creep Tested and Thermally Aged Udimet 520 Using Acousto-UltrasonicsDue to elevated temperatures and excessive stresses, turbine components may experience creep behavior. As a result, it is desirable to monitor and assess the current condition of such components. This study employed the Acousto-Ultrasonics (AU) method in an effort to monitor the state of the material at various percentages of used up creep life in the nickel base alloy, Udimet 520. A stepped specimen (i.e., varying cross sectional area) was employed which allowed for a postmortem nondestructive evaluation (NDE) analysis of the various levels of used up life. The overall objectives here were two fold: First, a user friendly, graphical interface AU system was developed, and second the new AU system was applied as an NDE tool to assess distributed damage resulting from creep. The experimental results demonstrated that the AU method shows promise as an NDE tool capable of detecting material changes as a function of used up creep life. Furthermore, the changes in the AU parameters were mainly attributed to the case of combined load and elevated temperature (i.e., creep) and not simply because of a timed exposure at elevated temperature (i.e., heat treatment or thermal aging).
Document ID
20010093221
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Gyekenyesi, Andrew L.
(Ohio Aerospace Inst. Brook Park, OH United States)
Kautz, Harold E.
(NASA Glenn Research Center Cleveland, OH United States)
Cao, Wei
(West Virginia Inst. of Tech. Montgomery, WV United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2001
Subject Category
Structural Mechanics
Report/Patent Number
NASA/TM-2001-210988
E-12842
NAS 1.15:210988
Report Number: NASA/TM-2001-210988
Report Number: E-12842
Report Number: NAS 1.15:210988
Meeting Information
Meeting: Turbo Expo 2001
Location: New Orleans, LA
Country: United States
Start Date: June 4, 2001
End Date: June 7, 2001
Sponsors: International Gas Turbine Inst., American Society of Mechanical Engineers
Funding Number(s)
PROJECT: RTOP 728-30-20
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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