Gas turbine combustor

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

Reexamination Certificate

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Details

C060S747000, C060S748000

Reexamination Certificate

active

07540154

ABSTRACT:
This invention aims to suppress the occurrence of smoke, for example, during a light load operation of a gas turbine, by adopting an air blast method for a pilot nozzle in a dual fuel combustion low NOxcombustor. A gas turbine combustor of the present invention is that in a gas turbine furnished with a dual fuel combustion low NOxcombustor having a pilot nozzle capable of injecting a gaseous fuel and a liquid fuel simultaneously or selectively, and a plurality of main nozzles disposed around the pilot nozzle and being capable of injecting a gaseous fuel and a liquid fuel simultaneously or selectively, wherein the pilot nozzle has a gas nozzle portion for injecting the gaseous fuel, and a liquid nozzle portion for injecting the liquid fuel, adopts an air blast method for the liquid nozzle portion, uses combustion air as air for an air blast, and throws the combustion air at a liquid film formed in the liquid nozzle portion to atomize the liquid fuel by use of a velocity difference.

REFERENCES:
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patent: 4425755 (1984-01-01), Hughes
patent: 5185997 (1993-02-01), Nishijima
patent: 5423173 (1995-06-01), Lemon et al.
patent: 5481866 (1996-01-01), Mowill
patent: 5505045 (1996-04-01), Lee et al.
patent: 6655145 (2003-12-01), Boardman
patent: 2004/0255589 (2004-12-01), Yoshida et al.
patent: 0 286 569 (1988-10-01), None
patent: 08-005076 (1996-01-01), None
patent: 08-145363 (1996-06-01), None
patent: 09-264536 (1997-10-01), None
patent: 2000-130756 (2000-05-01), None
Office Action issued Sep. 5, 2008 in Corresponding Chinese Patent Application No. 200610005944.3.

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