| 发明名称 |
AUGMENTOR PILOT NOZZLE |
| 摘要 |
<p>AUGMENTOR PILOT NOZZLE A gas turbine engine augmentor nozzle has an inlet for connection to an augmentor fuel conduit and an outlet for expelling a spray of fuel. A passageway between the inlet and outlet is at least partially bounded by outlet end surface portions diverging from each other. The nozzle may be used as a replacement for a non-divergent nozzle and may reorient a fuel jet centerline toward radial.</p> |
| 申请公布号 |
SG144719(A1) |
申请公布日期 |
2008.08.28 |
| 申请号 |
SG20040027124 |
申请日期 |
2004.04.23 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SNYDER TIMOTHY S.;BRDAR CHRISTOPHER R.;BUEY JOHN R. |
| 分类号 |
F02K3/00;F02K3/10;F23D11/12;F23R3/20;F23R3/28;(IPC1-7):F02K3/11;F23D11/38 |
主分类号 |
F02K3/00 |
| 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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