发明名称 |
ROCKET ENGINE HAVING GUIDE VANES IN THE NOZZLE OF THE ENGINE |
摘要 |
<p>A rocket engine having guide vanes in the engine nozzle, the guide vanes (2) being mounted for turning at or near the rearmost ends of fixed vanes (1) being parallel to the axis of the nozzle and protruding into the combustion chamber of the engine. The foremost ends (4) of the guide vanes (2) may be shielded by the rearmost ends of the fixed vanes (1), and the guide vanes (2) may be individually turnable.</p> |
申请公布号 |
WO2005028844(A1) |
申请公布日期 |
2005.03.31 |
申请号 |
WO2004NO00272 |
申请日期 |
2004.09.14 |
申请人 |
NAMMO RAUFOSS AS;OERBEKK, ERLAND |
发明人 |
OERBEKK, ERLAND |
分类号 |
F02K9/84;F02K9/88;(IPC1-7):F02K9/97;F42B10/66 |
主分类号 |
F02K9/84 |
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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