发明名称 Turbine engine guide vane and arrays thereof
摘要 <p>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 (28) may also cooperate with each other to restrict an observer's line of sight to planes (90) upstream of the vane array.</p>
申请公布号 EP2586991(B1) 申请公布日期 2016.02.03
申请号 EP20120196352 申请日期 2005.10.21
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 AGGARWALA, ANDREW S.;GACEK, RICHARD E.;WAGNER, JOEL H.;NOALL, JEFF S.
分类号 F01D9/04;F01D5/14;F01D9/06 主分类号 F01D9/04
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