Gas turbine combustor and operating method thereof

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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C060S737000, C060S746000

Reexamination Certificate

active

11136570

ABSTRACT:
A gas turbine combustor has a combustion chamber into which fuel and air are supplied, wherein the fuel and the air are supplied into said combustion chamber as a plurality of coaxial jets.

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“Development of Combustor for LNG. Oxygen Firing”, 29th Gas Turbine Regular Lecture Meeting—Collected Lecture Papers, 2001, pp. 113-118.

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