CASING MANIFOLD FOR HIGH PRESSURE AIR DELIVERY TO FUEL NOZZLE PILOT SYSTEM

PROBLEM TO BE SOLVED: To provide a pilot manifold system for a combustor of a gas turbine engine.SOLUTION: The pilot manifold system may include a casing with a casing manifold, an end cover connected to the casing and having an end cover passage in communication with the casing manifold, and a fuel...

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Bibliographic Details
Main Authors BRANDON TAYLOR OVERBY, ROMIG BRYAN WESLEY
Format Patent
LanguageEnglish
Japanese
Published 18.05.2015
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 pilot manifold system for a combustor of a gas turbine engine.SOLUTION: The pilot manifold system may include a casing with a casing manifold, an end cover connected to the casing and having an end cover passage in communication with the casing manifold, and a fuel nozzle mounted on the vicinity of the end cover. The fuel nozzle may include a pilot system in communication with the end cover passage. 【課題】本出願は、ガスタービンエンジンの燃焼器用のパイロットマニホールドシステムを提供する。【解決手段】パイロットマニホールドシステムは、ケーシングマニホールドを有するケーシングと、ケーシングに接続され、かつケーシングマニホールドと連通するエンドカバー通路を有するエンドカバーと、エンドカバーの付近に載置された燃料ノズルとを含むことができる。燃料ノズルは、エンドカバー通路と連通するパイロットシステムを含むことができる。【選択図】図１
Bibliography:Application Number: JP20140225675