The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 08, 2002

Filed:

Apr. 09, 2001
Applicant:
Inventors:

Koichi Nishida, Takasago, JP;

Katsunori Tanaka, Takasago, JP;

Shigemi Mandai, Takasago, JP;

Yutaka Kawata, Takasago, JP;

Masataka Ohta, Takasago, JP;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02G 3/00 ;
U.S. Cl.
CPC ...
F02G 3/00 ;
Abstract

A gas turbine combustor improves the fuel distribution from a main fuel nozzle, suppressing fluctuations of internal pressure and elevation of inner tube metal temperature, and enhancing the combustion stability and durability of the combustor. The gas turbine combustor is a multi-nozzle type premixing combustor with a nozzle outer tube ( ) for forming and injecting a premixed gas of main fuel and combustion air divided and disposed in plural sections around a cone ( ) for forming a diffusion flame by reaction between pilot fuel and combustion air disposed in a center of a section of a combustor inner tube ( ). Nozzle holes ( ) of a main fuel nozzle ( ) are formed in three positions at equal intervals on the nozzle main body wall, and one of them is disposed at the outer periphery of the combustor inner tube ( ) on a diametral line linking between the center of the combustor inner tube ( ) and the center of the main fuel nozzle ( ), whereby the fuel distribution to the outer periphery is decreased.


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