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NDE of PWA 1480 single crystal turbine blade materialCantilever bending fatigue specimens were examined by fluorescent liquid penetrant and radioactive gas penetrant (Krypton) Nondestructive Evaluation (NDE) methods and tested. Specimens with cast, ground, or polished surfaces were evaluated to study the effect of surface condition on NDE and fatigue crack initiation. Fractographic and metallurgical analyses were performed to determine the nature of crack precursors. Preliminary results show that fatigue strength was lower for specimens with cast surfaces than for specimens with machined surfaces. The liquid penetrant and gas penetrant techniques both provided indications of a large population of defects on the cast surfaces. On ground or polished specimen surfaces, the gas penetrant appeared to estimate the actual number of voids more accurately than the liquid penetrant.
Document ID
19950062052
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Klima, Stanley J.
(NASA Lewis Research Center Cleveland, OH, United States)
Orange, Thomas W.
(NASA Lewis Research Center United States)
Dreshfield, Robert L.
(NASA Lewis Research Center United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
ISSN: 0148-7191
Subject Category
Quality Assurance And Reliability
Report/Patent Number
SAE PAPER 931371
Meeting Information
Meeting: SAE, Aerospace Atlantic Conference & Exposition
Location: Dayton, OH
Country: United States
Start Date: April 20, 1993
End Date: April 23, 1993
Accession Number
95A93651
Distribution Limits
Public
Copyright
Other

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