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

06928823

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.

REFERENCES:
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patent: RE34962 (1995-06-01), Shekleton et al.
patent: 5651252 (1997-07-01), Ansart et al.
patent: 5722230 (1998-03-01), Cohen et al.
patent: 5899074 (1999-05-01), Komatsu et al.
patent: 6389815 (2002-05-01), Hura et al.
patent: 6481209 (2002-11-01), Johnson et al.
patent: 6684641 (2004-02-01), Moriya et al.

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