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 measured individual blade temperature; another non-immersion gas temperature sensor, not yet fully developed, will provide accurate gas temperature data up to 1900 degrees C. These instruments are described with present and potential uses in control systems. /GMRL/

  • Corporate Authors:

    Society of Automotive Engineers (SAE)

    400 Commonwealth Drive
    Warrendale, PA  United States  15096
  • Authors:
    • Rohy, D A
    • Duffy, T E
    • Compton, W A
  • Publication Date: 1975-2

Media Info

  • Pagination: 15 p.

Subject/Index Terms

Filing Info

  • Accession Number: 00097904
  • Record Type: Publication
  • Report/Paper Numbers: SAE #750206 Proceeding
  • Files: TRIS
  • Created Date: Sep 30 1975 12:00AM