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Types of rotor failure and characteristics of fragmentsNoncontained rotor failures in U.K. engines resulting from low cycle fatigue, low cycle fatigue with superimposed high cycle fatigue, and overheating and-or overspeeding were analyzed. The size, shape, weight, velocity, energy, and direction of the fragments released from turbines and compressors were studied and are presented in graph.
Document ID
19780002130
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mccarthy, D. (Rolls-Royce Ltd. Derby, United Kingdom)
Date Acquired
August 9, 2013
Publication Date
March 1, 1977
Publication Information
Publication: MIT An Assessment of Technol. for Turbojet Engine Rotor Failures
Subject Category
Aircraft Propulsion And Power
Accession Number
78N10073
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19780002125Collected WorksAn Assessment of Technology for Turbojet Engine Rotor Failures
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