CAN COMBUSTOR FOR CAN-ANNULAR COMBUSTOR ARRANGEMENT IN GAS TURBINE

PROBLEM TO BE SOLVED: To provide a can combustor for a can-annular combustor arrangement in a gas turbine with an improved operability, serviceability and environmental performance.SOLUTION: Up to four premixed burners 14 are attached to a front panel 13 in a substantially annular arrangement. Each...

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Bibliographic Details
Main Authors KLAUS KNAPP, NARESH ALURI, FRANKLIN MARIE GENIN, ULRICH RATHMANN, NICOLAS TRAN
Format Patent
LanguageEnglish
Japanese
Published 17.11.2014
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION APPARATUS
COMBUSTION ENGINES
COMBUSTION PROCESSES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:PROBLEM TO BE SOLVED: To provide a can combustor for a can-annular combustor arrangement in a gas turbine with an improved operability, serviceability and environmental performance.SOLUTION: Up to four premixed burners 14 are attached to a front panel 13 in a substantially annular arrangement. Each of the premixed burners 14 has a conical swirl generator 15 and a mixing tube 16 to induce a swirl of a fuel/air mixture. 【課題】改良された操作性、保守容易性及び環境性能を有する、ガスタービンにおける缶型環状燃焼器配列用の缶型燃焼器を提供する。【解決手段】４つまでの予混合バーナ１４が、フロントパネル１３に実質的に環状の配列で取り付けられており、予混合バーナ１４のそれぞれは、燃料／空気混合物のスワールを生ぜしめるために、円錐形のスワール発生器１５及び混合管１６を有する。【選択図】図１
Bibliography:Application Number: JP20140092325