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Global Patent Index - EP 0335978 A4

EP 0335978 A4 19891213 - GAS TURBINE COMBUSTOR.

Title (en)

GAS TURBINE COMBUSTOR.

Title (de)

GASTURBINENBRENNER.

Title (fr)

BRULEUR DE TURBINE A GAZ.

Publication

EP 0335978 A4 19891213 (EN)

Application

EP 88907798 A 19880831

Priority

  • JP 8800870 W 19880831
  • JP 22020687 A 19870904

Abstract (en)

[origin: WO8902052A1] This invention relates to a gas turbine combustor of a premixing combustion system in which a fuel and the air are mixed and burnt, consisting of a cylindrical main nozzle provided on an upstream end wall of a cylindrical combustion chamber, an auxiliary nozzle formed around the main nozzle, a main premixed gas supply means for supplying a premixed gas to the main nozzle, and an auxiliary premixed gas supply means for supplying a premixed gas, the excess air ratio of which is smaller than that of the main premixed gas, to the auxiliary nozzle. Owing to this arrangement, a lean premixed gas having an excess air ratio larger than 1 can be burnt stably under low to high loads of a gas turbine.

IPC 1-7

F23R 3/28

IPC 8 full level

F23R 3/30 (2006.01); F02C 9/34 (2006.01); F23D 14/26 (2006.01); F23D 23/00 (2006.01); F23R 3/28 (2006.01); F23R 3/32 (2006.01)

CPC (source: EP)

F23D 14/26 (2013.01); F23D 23/00 (2013.01); F23R 3/286 (2013.01)

Citation (search report)

Designated contracting state (EPC)

CH DE FR GB IT LI

DOCDB simple family (publication)

WO 8902052 A1 19890309; CN 1011064 B 19910102; CN 1032230 A 19890405; DE 3854666 D1 19951214; DE 3854666 T2 19960425; EP 0335978 A1 19891011; EP 0335978 A4 19891213; EP 0335978 B1 19951108; JP 2528894 B2 19960828; JP S6463721 A 19890309

DOCDB simple family (application)

JP 8800870 W 19880831; CN 88106413 A 19880903; DE 3854666 T 19880831; EP 88907798 A 19880831; JP 22020687 A 19870904