Title:
METHOD FOR BURNING FUEL IN BURNER OF GAS TURBINE ENGINE
Document Type and Number:
Japanese Patent JPH10196955
Kind Code:
A
Abstract:
To reduce the trend that a flame is stabilized in the tangential inlet nozzle of a gas turbine engine.
Fuel and the air are mixed in the mixing section 28 of a fuel nozzle 10 to produce a fuel/air mixture which is isolated from combustion products by sustaining the axial velocity through the mixing section 28 at a sufficiently high level and combining the face of an internal passage 64 of a central body 12 (supplied or not supplied with fuel) with the face of a burner inlet port 20.
Inventors:
SNYDER TIMOTHY S
SOWA WILLIAM A
KRAMER STEPHEN K
SOWA WILLIAM A
KRAMER STEPHEN K
Application Number:
JP36523497A
Publication Date:
July 31, 1998
Filing Date:
December 19, 1997
Export Citation:
Assignee:
UNITED TECHNOLOGIES CORP (US)
International Classes:
F02C7/232; F02M61/16; F23C7/00; F23C7/02; F23D11/12; F23D11/36; F23D17/00; F23R3/12; F23R3/28; F23R3/30; F23R3/34; (IPC1-7): F23R3/28; F02C7/232; F23C7/02; F23D11/12; F23R3/12; F23R3/30; F23R3/34
Attorney, Agent or Firm:
Asakura Shozo
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