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A Radioactive Krypton Diffusion Technique for Temperature Mapping of Turbine Blade Surfaces Lycoming Div., AVCO Corporation

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Wisnieff, Stanley F., author.
Conference Name:
National Powerplant and Transportation Meetings (1965-10-18 : Cleveland, Ohio, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1965
Summary:
Development of turbine blade cooling techniques have been prompted by the demand for increased power and efficiency from existing engine envelopes. Accurate determination of temperature profiles exhibited by the turbine blades during engine operation expedite the attainment of optimum design. This paper describes the use of radioactive krypton-85 to determine the maximum temperature experienced by the blade surface during the engine operating period. Apparatus and procedures developed after considerable experimentation are described, and typical temperature evaluations are presented
Notes:
Vendor supplied data
Publisher Number:
650704
Access Restriction:
Restricted for use by site license

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