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Title:
DIFFUSION COMBUSTION TYPE GAS TURBINE
Document Type and Number:
Japanese Patent JPH11304151
Kind Code:
A
Abstract:

To provide a gas turbine to reduce the generation of NOx and maintain reduction of a cost being the original advantage of the diffusion type as it is, in a diffusion combustion type gas turbine to separately supply fuel and air which are burnt in a combustor.

A diffusion combustion gas turbine 3 is constituted that an exhaust route 5 for exhaust gas of the gas turbine 3 and a fuel route for fuel supply of a combustor 2 are intercommunicated through a recirculation route 8 to recirculate exhaust gas through an exhaust gas compressor 7. By mixing exhaust gas of the gas turbine 3 in fuel through the recirculation route 8, high calory fuel is reformed to low calory fuel and a flame temperature under combustion is reduced and NOx generation concentration is decreased.


Inventors:
BANDAI SHIGEMI
ITSURA TETSUO
FUKUE ICHIRO
AKAMATSU SHINJI
Application Number:
JP11070198A
Publication Date:
November 05, 1999
Filing Date:
April 21, 1998
Export Citation:
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Assignee:
MITSUBISHI HEAVY IND LTD
International Classes:
F02C3/30; F02C7/22; F23R3/00; (IPC1-7): F23R3/00; F02C3/30; F02C7/22
Attorney, Agent or Firm:
Arata Ishikawa (1 person outside)