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专利名称：Combustor for gas turbine engine发明人：Horikawa, Atsushi,Kazari, Masahide,Okada,
Kunio,Kitajima, Junichi,Funke,
Harald,Kusterer, Karsten,Ayed, Anis Haj
申请号：AU2015265278申请日：20150528公开号：AU2015265278B2公开日：20180405
摘要：A combustor including a combustion liner (13) having a combustion chamber(11) formed therein; and a fuel injector (15) mounted to a top portion of the combustionliner, and including a fuel injection member (34) having a plurality of fuel injection annularportions (33) and an air guide member (36) including a plurality of combustion air annularportions (35) that guide air for combustion. The fuel injection annular portions and thecombustion air annular portions are arranged concentrically and alternately. The fuelinjector injects fuel (F) and air (A) into the combustion chamber. Each of the fuel injectionannular portions includes a plurality of fuel injection holes (39) that are open in a radialdirection thereof, and each of the combustion air annular portions includes a plurality ofair guide grooves (41) that are open in an axial direction thereof, and guide the air to thefuel jetted from the fuel injection holes.
申请人：B&B Agema GmbH,Kawasaki Jukogyo Kabushiki Kaisha
代理人：Phillips Ormonde Fitzpatrick
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