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High temperature strain gage technology for gas turbine enginesThis report summarizes the results of a six month study that addressed specific issues to transfer the Pd-13Cr static strain sensor to a gas turbine engine environment. The application issues that were addressed include: (1) evaluation of a miniature, variable potentiometer for use as the ballast resistor, in conjunction with a conventional strain gage signal conditioning unit; (2) evaluation of a metal sheathed, platinum conductor leadwire assembly for use with the three-wire sensor; and (3) subjecting the sensor to dynamic strain cyclic testing to determine fatigue characteristics. Results indicate a useful static strain gage system at all temperature levels up to 1350 F. The fatigue characteristics also appear to be very promising, indicating a potential use in dynamic strain measurement applications. The procedure, set-up, and data for all tests are presented in this report. This report also discusses the specific strain gage installation technique for the Pd-13Cr gage because of its potential impact on the quality of the output data.
Document ID
19950005583
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Fichtel, Edward J.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Mcdaniel, Amos D.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1994
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-191177
NAS 1.26:191177
Accession Number
95N11996
Funding Number(s)
CONTRACT_GRANT: NAS3-25952
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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