发明名称 PILOT INJECTOR FOR GAS TURBINE ENGINES
摘要 <p>A combustor is disclosed capable of averting engine flameout. This combustor comprises a combustion chamber, which comprises an outlet for discharging heated combustion products. The combustor further comprises a primary injector for injecting a fuel and compressed air into a primary zone of the combustion chamber such that the fuel is induced into a recirculation zone at a corner of the primary zone. Combustion means for combusting the fuel and the compressed air in the combustion chamber resulting in heated combustion products are also incorporated in the combustor. Moreover, the combustor comprises sensing means for monitoring the combustor to substantially detect a pre-flameout condition. To realize the advantages of the present invention, the combustor additionally comprises a pilot injector for injecting a propellant into the recirculation zone in response to detecting said flameout condition by the sensing means, such that the propellant combusts as a diffusion flame.</p>
申请公布号 EP0765453(B1) 申请公布日期 2001.01.10
申请号 EP19950924648 申请日期 1995.06.21
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 HU, AARON, S.
分类号 F02C7/262;F02C9/00;F02C9/40;F23D14/74;F23D23/00;F23N5/00;F23N5/24;F23R3/28;F23R3/34;F23R3/46;(IPC1-7):F23D23/00 主分类号 F02C7/262
代理机构 代理人
主权项
地址
您可能感兴趣的专利