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Temperature Measurement for Advanced Gas Turbine Controls Solar Div., Int'l. Harvester Company, San Diego, California
- Format:
- Conference/Event
- Author/Creator:
- Rohy, David A., author.
- Conference Name:
- 1975 Automotive Engineering Congress and Exposition (1975-02-24 : Detroit, Michigan, United States)
- Language:
- English
- Physical Description:
- 1 online resource
- Place of Publication:
- Warrendale, PA SAE International 1975
- Summary:
- Modern gas turbine engines with turbine inlet temperatures higher than metal melting temperatures must have control systems which provide subsecond response to changes in gas or metal temperatures. High quality data are required to provide for the most efficient engine operation consistent with engine safety.Recently developed instruments measure individual blade temperature; another non-immersion gas temperature sensor, not yet fully developed, will provide accurate gas temperature data up to 1900°C. These instruments are described with present and potential uses in control systems
- Notes:
- Vendor supplied data
- Publisher Number:
- 750206
- Access Restriction:
- Restricted for use by site license
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