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.
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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 |
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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