发明名称 Turbine vane segment with cooling air supplying system
摘要 <p>The turbine distributor part (110) includes outer (104) and inner platform segments in between which multiple hollow blades are provided and supplied with cooling air. A cap (132) covers the base portion of the outer platform segment to define a chamber that communicates with the interior of the blades via communication openings. Air inlets are provided in the cap to allow the chamber to be supplied with cooling air. An independent claim is included for a turbine engine.</p>
申请公布号 EP1659265(A1) 申请公布日期 2006.05.24
申请号 EP20050292249 申请日期 2005.10.25
申请人 SNECMA 发明人 BERMOND, SABINE;DERVAUX, ALEXANDRE;GUIMBARD, JEAN-MICHEL;LORO, GAEL
分类号 F01D5/18;F01D5/14;F01D9/06 主分类号 F01D5/18
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