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Feasibility Demonstration of a Small Fluid-Cooled Turbine at 2300F

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Gabel, Ronald M., author.
Conference Name:
1969 International Automotive Engineering Congress and Exposition (1969-01-13 : Detroit, Michigan, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1969
Summary:
This paper presents the results of an investigation directed toward the design and demonstration of a fluid-cooled turbine for an advanced small gas turbine. The primary objective was to advance and demonstrate high turbine inlet temperature technology utilizing a thermosiphon cooling system concept for a small gas turbine engine to the level that will provide a potential for doubling the specific horsepower relative to current small aircraft propulsion engines
Notes:
Vendor supplied data
Publisher Number:
690034
Access Restriction:
Restricted for use by site license

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