发明名称 |
Pulsed combustion fluidic nozzle |
摘要 |
<p>A propulsion system for producing thrust includes a turbine engine. The engine has a compressor, a combustor downstream of the compressor along a flow path, and a turbine downstream of the combustor along the flow path. A plurality of combustion conduits have outlets positioned to discharge combustion gas to form a fluidic nozzle throat.</p> |
申请公布号 |
EP1801402(A2) |
申请公布日期 |
2007.06.27 |
申请号 |
EP20060256384 |
申请日期 |
2006.12.15 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
ROBERGE, GARY D.;WOZNIAK, JAMES;TWELVES, WENDELL V., JR. |
分类号 |
F02K1/30;F02K7/075 |
主分类号 |
F02K1/30 |
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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