Title:
【発明の名称】ガスタービンの燃焼室
Document Type and Number:
Japanese Patent JP3075732
Kind Code:
B2
Abstract:
In a combustion chamber (A) having the shape of an annular combustion chamber, a series of large and small premix burners (B, C) is arranged along the annular front wall (10). The large premix burners (B), which are the main burners of the combustion chamber (A), and the small premix burners (C), which are the pilot burners of the combustion chamber (A), follow each other in alternating sequence and regularly along the front wall (10), where they also open into the combustion space of the combustion chamber (A). A plurality of air nozzles (D) are positioned between the large premix burners (B) and the small premix burners (C), their injection being directed into the combustion space of the combustion chamber (A).
Inventors:
Jacob Keller
Application Number:
JP14554190A
Publication Date:
August 14, 2000
Filing Date:
June 05, 1990
Export Citation:
Assignee:
Asea Brown Bovelli Akti Ngezershyaft
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): F23R3/30; F23R3/02; F23R3/28; F23R3/44
Other References:
【文献】仏国特許出願公開944310(FR,A1)
Attorney, Agent or Firm:
Toshio Yano (1 outside)