Title:
【発明の名称】ガスタービンの運転方法及びガスタービン
Document Type and Number:
Japanese Patent JP2002523685
Kind Code:
A
Abstract:
In a gas turbine having a plurality of hybrid burners, each of which has a pilot burner and a main burner, a different pilot fuel quantity is fed to the pilot burners as a function of the load on the gas turbine. This provides both stable operation of the gas turbine at low loads and effective suppression of combustion oscillations at high loads.
Inventors:
Hoffman, Stephan
Kessler, Michael
Cher, German
Kessler, Michael
Cher, German
Application Number:
JP2000567887A
Publication Date:
July 30, 2002
Filing Date:
August 13, 1999
Export Citation:
Assignee:
Siemens Aktiengesellschaft
International Classes:
F02C9/34; F23R3/28; F23R3/34; (IPC1-7): F02C9/34; F23R3/28
Attorney, Agent or Firm:
Iwao Yamaguchi