scholarly journals Development of high-temperature subsystem technology to a technology readiness state: phase I. First quarterly technical progress report, June--August 1976. [Industrial open-cycle gas turbine; coal-derived fuel]

1976 ◽  
Author(s):  
N. Carlson

Author(s):  
M. W. Horner ◽  
A. Caruvana

Final component and technology verification tests have been completed for application to a 2600°F rotor inlet temperature gas turbine. These tests have proven the capability of combustor, turbine hot section, and IGCC fuel systems and controls to operate in a combined cycle plant burning a coal-derived gas fuel at elevated gas turbine inlet temperatures (2600–3000°F). This paper presents recent test results and summarizes the overall progress made during the DOE-HTTT Phase II program.



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