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Initial Assessment of the Effects of Nonmetallic Inclusions on Fatigue Life of Powder-Metallurgy-Processed Udimet(TM) 720The fatigue lives of modern powder metallurgy (PM) disk alloys are influenced by variabilities in alloy microstructure and mechanical properties. These properties can vary due to the different steps of materials/component processing and machining. One of these variables, the presence of nonmetallic inclusions, has been shown to significantly degrade low-cycle fatigue (LCF) life. Nonmetallic inclusions are inherent defects in powder alloys that are a by-product of powder-processing techniques. Contamination of the powder can occur in the melt, during powder atomization, or during any of the various handling processes through consolidation. In modern nickel disk powder processing facilities, the levels of inclusion contamination have been reduced to less than 1 part per million by weight. Despite the efforts of manufacturers to ensure the cleanliness of their powder production processes, the presence of inclusions remains a source of great concern for the designer. the objective of this study was to investigate the effects on fatigue life of these inclusions. Since natural inclusions occur so infrequently, elevated levels of inclusions were carefully introduced in a nickel-based disk superalloy, Udimet 720 (registered trademark of Special Metals Corporation), produced using PM processing. Multiple strain-controlled fatigue tests were then performed on this material at 650 C. Analyses were performed to compare the LCF lives and failure initiation sites as functions of inclusion content and fatigue conditions. A large majority of the failures in specimens with introduced inclusions occurred at cracks initiating from inclusions at the specimen surface. The inclusions could reduce fatigue life by up to 100 times. These effects were found to be dependent on strain range and strain ratio. Tests at lower strain ranges and higher strain ratios produced larger effects of inclusions on life.
Document ID
20020076201
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Gabb, T. P.
(NASA Glenn Research Center Cleveland, OH United States)
Telesman, J.
(NASA Glenn Research Center Cleveland, OH United States)
Kantzos, P. T.
(Ohio Aerospace Inst. Brook Park, OH United States)
Bonacuse, P. J.
(Army Research Lab. Cleveland, OH United States)
Barrie, R. L.
(Army Research Lab. Cleveland, OH United States)
Date Acquired
August 29, 2013
Publication Date
August 1, 2002
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:211571
NASA/TM-2002-211571
E-13355
ARL-TR-2804
Report Number: NAS 1.15:211571
Report Number: NASA/TM-2002-211571
Report Number: E-13355
Report Number: ARL-TR-2804
Meeting Information
Meeting: Advanced Materials and Processes for Gas Turbines Symposium
Location: Copper Mountain, CO
Country: United States
Start Date: September 22, 2002
End Date: September 26, 2002
Sponsors: United Engineering Foundation, Inc.
Funding Number(s)
PROJECT: RTOP 708-24-13
PROJECT: DA Proj. 1L1-61102-AH-45
Distribution Limits
Public
Copyright
Public Use Permitted.
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