Title:
COMBUSTOR STRUCTURE OF GAS TURBINE
Document Type and Number:
Japanese Patent JP2001343123
Kind Code:
A
Abstract:
To provide the combustor structure of a gas turbine capable of being decreased in size.
To reduce the temperature of combustion gas generated in a combustor, the overall length of the combustor is shortened by forming an air hole to feed air in a scroll connected to the downstream side of the combustor.
Inventors:
FUKUI TOSHIMITSU
Application Number:
JP2000164399A
Publication Date:
December 14, 2001
Filing Date:
June 01, 2000
Export Citation:
Assignee:
YANMAR DIESEL ENGINE CO
International Classes:
F23R3/06; F02C3/30; F23R3/42; (IPC1-7): F23R3/06; F02C3/30; F23R3/42
Attorney, Agent or Firm:
Aoyama Ryo (1 person outside)