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HOT SPIN-AND-BURST TEST METHODS FOR AIRCRAFT TURBINE WHEELSMethods are described for suspension-system vibration damping, automatically controlled induction heating through radiation pyrometers, rotating-disk temperature measurement, and unattended operation with a safety-interlock system.
Document ID
19620000263
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
A. G. Holms (Glenn Research Center Cleveland, United States)
A. J. Repko (Glenn Research Center Cleveland, United States)
Date Acquired
August 1, 2013
Publication Date
December 1, 1961
Subject Category
Structural Mechanics
Accession Number
62N10263
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BURST
SPIN TEST
AIRCRAFT
TURBINE WHEEL
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