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Vibratory Strain Distribution in an Integral-Machined Air Turbine Starter Wheel Garrett Fluid Systems Company, A Division of The Garrett Corporation

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Giard, Joel R., author.
Conference Name:
SAE Aerospace Technology Conference and Exposition (1986-10-13 : Long Beach, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1986
Summary:
Turbine blade fatigue failures began to occur on the Garrett Air Turbine Starter, Model ATS200-58, in commercial airline service. A comprehensive program including metallurgical analysis, finite-element analysis, and strain gage testing of instrumented turbine wheels resulted in large quantities of data on blade vibratory strain. The results of testing various configurations, including the addition of damping and the use of different numbers of stator vanes, are presented
Notes:
Vendor supplied data
Publisher Number:
861737
Access Restriction:
Restricted for use by site license

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