Title:
GAS TURBINE COMBUSTOR
Document Type and Number:
WIPO Patent Application WO/2006/027989
Kind Code:
A1
Abstract:
A gas turbine combustor includes a pilot burner, and a plurality of main burners disposed around the periphery of the pilot burner on the radially outer side. Each of the main burners (2) includes an extension pipe disposed at its downstream end. The outlet port of the extension pipe is shaped to have a radial edge which is parallel with the radial direction. In this manner, occurrence of flashback is effectively prevented.
More Like This:
| JPH09243083 | GAS TURBINE COMBUSTION DEVICE |
| JP2002174425 | GAS TURBINE COMBUSTOR |
Inventors:
MORIWAKI ATSUSHI (JP)
OHTA MASATAKA (JP)
SAITOH KEIJIRO (JP)
TANIMURA SATOSHI (JP)
AKAMATSU SHINJI (JP)
NAGAI NOBUHIKO (JP)
OHTA MASATAKA (JP)
SAITOH KEIJIRO (JP)
TANIMURA SATOSHI (JP)
AKAMATSU SHINJI (JP)
NAGAI NOBUHIKO (JP)
Application Number:
PCT/JP2005/015989
Publication Date:
March 16, 2006
Filing Date:
September 01, 2005
Export Citation:
Assignee:
MITSUBISHI HEAVY IND LTD (JP)
MORIWAKI ATSUSHI (JP)
OHTA MASATAKA (JP)
SAITOH KEIJIRO (JP)
TANIMURA SATOSHI (JP)
AKAMATSU SHINJI (JP)
NAGAI NOBUHIKO (JP)
MORIWAKI ATSUSHI (JP)
OHTA MASATAKA (JP)
SAITOH KEIJIRO (JP)
TANIMURA SATOSHI (JP)
AKAMATSU SHINJI (JP)
NAGAI NOBUHIKO (JP)
International Classes:
F23R3/28; F02C7/232; F23R3/02; F23R3/12
Foreign References:
| JP2003014232A | 2003-01-15 | |||
| JPH11223341A | 1999-08-17 | |||
| JP2002372240A | 2002-12-26 | |||
| JPH09166326A | 1997-06-24 |
Attorney, Agent or Firm:
Kudoh, Minoru (24-10 Minamiooi 6-chom, Shinagawa-ku Tokyo, JP)
Download PDF:
Previous Patent: ROTARY BLADE FOR SURFACE GRINDER
Next Patent: IMMUNE NEPHELOMETRY METHOD AND REAGENT THEREFOR
Next Patent: IMMUNE NEPHELOMETRY METHOD AND REAGENT THEREFOR