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Effects of High-Temperature Exposures on the Fatigue Life of Superalloy Udimet(Registered Trademark) 720The purpose of this study was to examine the effects of extended exposures on the near-surface fatigue resistance of a disk superalloy. Powder metallurgy processed, supersolvus heat-treated Udimet 720 (U720) fatigue specimens were exposed in air at temperatures from 650 to 705 C for 100 hr to over 1000 hr. They were then tested using conventional fatigue tests at 650 C to determine the effects of exposure on fatigue resistance. The exposures reduced life by up to 70% and increased the scatter in life, compared to unexposed levels. Fractographic evaluations indicated the failure mode was shifted by the exposures from internal to surface crack initiations. The increased scatter in life was related to the competition between internal crack initiations at inclusions or large grains producing longer lives, and surface crack initiations at an environmentally affected surface layer producing shorter lives.
Document ID
20020076127
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Gabb, Timothy P.
(NASA Glenn Research Center Cleveland, OH United States)
Telesman, Jack
(NASA Glenn Research Center Cleveland, OH United States)
Kantzos, Peter T.
(Ohio Aerospace Inst. Brook Park, OH United States)
Sweeney, Joseph W.
(Akima Corp. Cleveland, OH United States)
Browning, Paul F.
(Solar Turbines International San Diego, CA United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2002
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:211570
E-13354
NASA/TM-2002-211570
Meeting Information
Meeting: 131st Annual Meeting and Exhibition
Location: Seattle, WA
Country: United States
Start Date: February 17, 2002
End Date: February 21, 2002
Sponsors: Minerals, Metals and Materials Society
Funding Number(s)
PROJECT: RTOP 708-24-13
Distribution Limits
Public
Copyright
Public Use Permitted.
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