Low-cost dual-fuel combustor and related method

Power plants – Combustion products used as motive fluid – Combustion products generator

Reexamination Certificate

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C060S737000

Reexamination Certificate

active

07546735

ABSTRACT:
A combustor for a gas turbine includes a combustion chamber and a plurality of radially outer nozzles surrounding a single, center nozzle, the radially outer nozzles configured to supply only gas fuel to the combustion chamber and the center nozzle configured to supply both gas and liquid fuel to the combustion chamber.

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