发明名称 |
Noise attenuating supersonic nozzle |
摘要 |
A sound attenuating supersonic nozzle has an exit to throat ratio in the range of 2.5 to 6.0, with longitudinal grooves formed in the interior wall of the supersonic passageway of the nozzle body. A shield is disposed about the exterior surface of the nozzle body, forming an exit cavity and an exit opening, and has a gill cavity through which auxiliary air flows into the exit cavity and mixes with the supersonic flow. 572
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申请公布号 |
US5050805(A) |
申请公布日期 |
1991.09.24 |
申请号 |
US19900506556 |
申请日期 |
1990.04.06 |
申请人 |
COLD JET, INC. |
发明人 |
LLOYD, DANIEL L.;MADLENER, RICHARD J. |
分类号 |
B05B1/00;B24C1/00;B24C5/04 |
主分类号 |
B05B1/00 |
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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