Title:
バーナ
Document Type and Number:
Japanese Patent JP4567266
Kind Code:
B2
Abstract:
The gas turbine burner (100) has a combustion air duct (104) in which are several spin-generating elements (108) forming spin-generators (109) in the form of spin blade rings. The ring consists of first (108A) and second (108B) blades. An extra pilot burner (106) stabilizes the mixture of fuel and combustion air emerging from the combustion air duct.
Inventors:
Hein, Olaf
Application Number:
JP2001534984A
Publication Date:
October 20, 2010
Filing Date:
October 16, 2000
Export Citation:
Assignee:
Siemens Aktiengesellschaft
International Classes:
F23R3/14; F23C7/00; F23L1/00; F23M20/00; F23R3/30; F23R3/34
Domestic Patent References:
| JP8296852A | ||||
| JP6034136A | ||||
| JP10318541A | ||||
| JP61022127A | ||||
| JP7280224A |
Attorney, Agent or Firm:
Iwao Yamaguchi
Hiroshi Yamamoto
Hiroshi Yamamoto