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 代理人
主权项
地址