Title:
ガスタービン
Document Type and Number:
Japanese Patent JP2005527763
Kind Code:
A
Abstract:
The gas turbine (51) has a combustion chamber (55) and a burner (1) opening into the combustion chamber at a burner opening enclosed by a Helmholtz resonator in annular manner. The resonator has a resonator volume and opens into the burner at a resonator opening that is continued into the resonator volume by a small pipe.
Inventors:
Flor, Patrick
Krebs, Werner
Prade, Bernd
Krebs, Werner
Prade, Bernd
Application Number:
JP2003573352A
Publication Date:
September 15, 2005
Filing Date:
February 24, 2003
Export Citation:
Assignee:
Siemens Aktiengesellschaft
International Classes:
F23M20/00; F23R3/28; F23R3/50; F23R3/52; F23R3/22; (IPC1-7): F23R3/22; F23R3/28; F23R3/52
Attorney, Agent or Firm:
Iwao Yamaguchi