Recuperated gas turbine engine system and method employing...

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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Details

C060S723000, C060S039511, C060S039520, C060S039270

Reexamination Certificate

active

07007487

ABSTRACT:
A recuperated gas turbine engine system and associated method employing catalytic combustion, wherein the combustor inlet temperature can be controlled to remain above the minimum required catalyst operating temperature at a wide range of operating conditions from full-load to part-load and from hot-day to cold-day conditions. The fuel is passed through the compressor along with the air and a portion of the exhaust gases from the turbine. The recirculated exhaust gas flow rate is controlled to control combustor inlet temperature.

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International Search Report for PCT Application No. PCT/US2004/023589; Filed Jul. 23, 2004; Date of Completion Nov. 9, 2004; Date of Mailing Nov. 17, 2004.

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