发明名称 Aero-slinger combustor
摘要 A combustor includes radially spaced apart outer and inner liners joined together at upstream ends through an annular dome disposed coaxially about a longitudinal centerline axis. A plurality of circumferentially spaced apart fuel injectors are disposed adjacent to an arcuate a splashplate for injecting fuel thereagainst, the splashplate being arcuate about the centerline axis. Primary air is channeled along the splashplate for mixing with the injected fuel for forming a fuel/air mixture dischargeable from the splashplate into a combustion zone defined between the liners and the dome.
申请公布号 US5265425(A) 申请公布日期 1993.11.30
申请号 US19930059342 申请日期 1993.05.11
申请人 GENERAL ELECTRIC COMPANY 发明人 HOWELL, STEPHEN J.
分类号 F23R3/14;F23R3/28;F23R3/30;F23R3/34;(IPC1-7):F02C3/14;F02C7/22 主分类号 F23R3/14
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