发明名称 TWO STREAM TANGENTIAL ENTRY NOZZLE
摘要 A tangential air entry fuel nozzle has a combustor inlet port to permit air and fuel to exit into a combustor. The port includes a convergent surface, a divergent su rface, and a cylindrical surface extending therebetween. The convergent surface extends a f irst distance along the longitudinal axis of the nozzle, the cylindrical surface exte nds a second distance along the axis, and the second distance is at least 5% of the first dis tance.
申请公布号 CA2225309(A1) 申请公布日期 1998.06.20
申请号 CA19972225309 申请日期 1997.12.19
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 KRAMER, STEPHEN K.;HAUCK, PETER F.
分类号 F02C7/232;F02M61/16;F23C7/00;F23D11/12;F23D11/36;F23D17/00;F23R3/12;F23R3/28;F23R3/30;(IPC1-7):F23R3/14;F23D14/02;F23D14/62 主分类号 F02C7/232
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