发明名称 Multi-stage fuel-air injector, for turbo machine combustion chamber, has secondary array of fuel feed orifices offset axially from the first set
摘要 The multi-stage air injector has an internal axial chamber (50) with an outlet (58) for the mixture charge. A first feed stage has multiple fuel feed orifices (64) opening into the chamber and spaced around its axis. An air injection opening (66) also opens into the chamber. The injector has a second fuel feed stage axially offset from the first and with openings (70) also spaced around the injector axis.
申请公布号 FR2832493(A1) 申请公布日期 2003.05.23
申请号 FR20010015042 申请日期 2001.11.21
申请人 SNECMA MOTEURS 发明人 DAVID ETIENNE;MICHAU MARION;RODRIGUES JOSE;SANDELIS DENIS;TIEPEL ALAIN
分类号 F23D11/10;F23R3/14;F23R3/28 主分类号 F23D11/10
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