发明名称 Turbine engine guide vane and arrays thereof
摘要 An exit guide vane array for a turbine engine includes a set of guide vanes 28 having a solidity and defining fluid flow passages 74 with a chordwisely converging forward portion 80 . The high solidity and convergent passage portion 80 resist fluid separation. The vanes may also cooperate with each other to restrict an observer's line of sight to planes upstream of the vane array.
申请公布号 US2006133930(A1) 申请公布日期 2006.06.22
申请号 US20040019870 申请日期 2004.12.21
申请人 AGGARWALA ANDREW S;GACEK RICHARD E;WAGNER JOEL H;NOALL JEFF S;SNYDER TIMOTHY S 发明人 AGGARWALA ANDREW S.;GACEK RICHARD E.;WAGNER JOEL H.;NOALL JEFF S.;SNYDER TIMOTHY S.
分类号 F01D9/00 主分类号 F01D9/00
代理机构 代理人
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