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Title:
COMBUSTION CHAMBER OF GAS TURBINE
Document Type and Number:
Japanese Patent JPH0320524
Kind Code:
A
Abstract:

PURPOSE: To realize wide operation area in the minimum exhaust gas emission, by arranging large and small premixed burners alternately along the entire front wall of a combustion chamber, and providing an air nozzle at every time.

CONSTITUTION: A main burner B and a pilot burner C which are arranged alternately as communicate with each other at the same height in an integral front wall 10 like a ring constituting the entry surface of an annular combustion chamber A. Several air nozzles D are provided between the burners B and C at every time, and the air nozzle occupies an almost half of front wall 10 in the radial direction. The center of small vortex 15 at a high temperature around the pilot burner C, and it is located between the center and the center of large vortex at a comparatively low temperature due to the main burner B. The air nozzle works in an area therebetween. Further, it improves the stability of both vortexes definitely.


More Like This:
WO/2003/002913GAS TURBINE COMBUSTOR
Inventors:
YAAKOBU KERAA
Application Number:
JP14554190A
Publication Date:
January 29, 1991
Filing Date:
June 05, 1990
Export Citation:
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Assignee:
ASEA BROWN BOVERI
International Classes:
F23R3/04; F23C99/00; F23D11/40; F23D17/00; F23R3/00; F23R3/02; F23R3/10; F23R3/12; F23R3/28; F23R3/30; F23R3/34; F23R3/44; F23R3/50; (IPC1-7): F23C11/00; F23R3/04; F23R3/28; F23R3/30
Attorney, Agent or Firm:
Toshio Yano (1 outside)



 
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