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Automated eddy current inspection of Space Shuttle APU turbine wheel bladesAn automated inspection system based on eddy current testing (ET) techniques has been developed to inspect turbine wheel blades on the APU used in NASA's Space Transportation system. The APU is a hydrazine-powered gas turbine with a 15-cm diameter Rene 41 turbine wheel, which has 123 first-stage blades and 123 second-stage blades. The flaw detection capability of the ET system is verified through comparison with fluorescent penetrant test results. Results of the comparison indicate that ET is capable of inspecting surfaces with very restrictive geometries. The ET capability requires development of probes with extremely small coils to allow inspection within 0.4 mm of the blade root and the leading and trailing edges of the blade and within a height restriction of less than 1 mm. The color 2D presentation of the ET data provided crack-growth pattern and length information similar to those found with visual techniques. It also provided visual clues to minimize geometry effects such as generated from blade edges, a neighoring blade, and changes in the blade thickness.
Document ID
19920046038
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fisher, Jay L.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Rowland, Stephen N.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Stolte, Jeffrey S.
(Southwest Research Institute San Antonio, TX, United States)
Salkowski, Charles
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Quality Assurance And Reliability
Meeting Information
Meeting: Annual Review of Progress in Quantitative Nondestructive Evaluation
Location: La Jolla, CA
Country: United States
Start Date: July 15, 1990
End Date: July 20, 1990
Accession Number
92A28662
Distribution Limits
Public
Copyright
Other

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