发明名称 |
Combustion device for gas turbine engine |
摘要 |
This combustion device is provided with: a combustion tube (13) inside which is formed a combustion chamber (11); a fuel injector (15) for injecting fuel (F) and air (A) into the combustion chamber, the fuel injector being provided at the top of the combustion tube, and having a fuel injection member (34) that includes a plurality of fuel injection annular parts (33) and an air guide member (36) that includes a plurality of combustion-air annular parts (35) for guiding air for combustion, the fuel combustion annular parts and the combustion-air annular parts being disposed concentrically with each other; and a reheating burner (10) disposed in the downstream region of the combustion chamber, on the circumferential wall of the combustion tube. The fuel injection annular parts have a plurality of fuel injection holes (39) opening in the radial direction thereof, and have a plurality of air guide grooves (41) opening in the axial direction thereof, for guiding air to the fuel injected through the fuel injection holes. |
申请公布号 |
AU2015268509(A1) |
申请公布日期 |
2016.12.15 |
申请号 |
AU20150268509 |
申请日期 |
2015.05.28 |
申请人 |
Kawasaki Jukogyo Kabushiki Kaisha |
发明人 |
Horikawa, Atsushi;Kazari, Masahide;Okada, Kunio;Kitajima, Junichi |
分类号 |
F23R3/32;F02C7/232;F23R3/28;F23R3/30;F23R3/34 |
主分类号 |
F23R3/32 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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