发明名称 Combined cycle boundary layer turbine
摘要 A two staged fluid propulsion apparatus of the type which utilizes prior art pitched blades combined with solid boundary layer disks supported by a novel rotating tubular flow conduit perforated to allow fluid flow to from the interior of the tube to the exterior surface positioned to outlet into spaces between a plurality of solid disks mounted within a volute case housing containing a singular fluid outlet and in communication with a plurality of fluid inlet ports.
申请公布号 US2005276681(A1) 申请公布日期 2005.12.15
申请号 US20040867943 申请日期 2004.06.14
申请人 AVINA DAVID C 发明人 AVINA DAVID C.
分类号 F01D1/00;F01D1/36;(IPC1-7):F01D1/00 主分类号 F01D1/00
代理机构 代理人
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