发明名称 |
PROPULSION SYSTEM WITH CANTED MULTINOZZLE GRID |
摘要 |
<p>A propulsion system includes a canted multinozzle plate (144), which has a multitude of small nozzles (150) angled (not perpendicular) to major surfaces of the multinozzle grid plate. The multinozzle plate may be a cylindrical section or plate, and the multitude of nozzles may be substantially axisymmetric about the cylindrical plate. The propulsion system includes a pressurized gas source which may be placed either forward or aft of the multinozzle grid plate. The propulsion system may have a conical insert, an internal flow separator cone (180), to aid in changing directions of flow from the pressurized gas source, to divert the flow through the multiple nozzles.</p> |
申请公布号 |
WO2008105967(A3) |
申请公布日期 |
2008.12.24 |
申请号 |
WO2007US83448 |
申请日期 |
2007.11.02 |
申请人 |
RAYTHEON COMPANY;CHASMAN, DANIEL;HAIGHT, STEPHEN D. |
发明人 |
CHASMAN, DANIEL;HAIGHT, STEPHEN D. |
分类号 |
F02K9/97;F02K9/30;F42B10/66 |
主分类号 |
F02K9/97 |
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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