发明名称 Facetted high temperature thruster design
摘要 An apparatus and method for manufacturing the apparatus is provided as a thruster for use with a fluidic diverter valve, the fluidic diverter valve having a valve housing. The thruster has a first tube, a valve seat, and a flow path. The first tube has a first end, a second end, and an outer surface. The first tube first end is configured to be disposed within the valve housing and the outer surface has a valve seat section and a blast tube section. The valve seat section is adapted to couple to the valve housing and the blast tube section is configured to extend outside of the valve housing. The valve seat is integrally formed on the first tube first end. The flow path extends between the first tube first and second ends.
申请公布号 US2007012370(A1) 申请公布日期 2007.01.18
申请号 US20050184600 申请日期 2005.07.18
申请人 GPS AEROSPACE, INC. 发明人 CHRISTENSEN DONALD J.;MUNSON LOWELL W.;MARUSIAK RONALD J.
分类号 F15C3/00 主分类号 F15C3/00
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