发明名称 RADIAL LOADING ELEMENT FOR TURBINE VANE
摘要 <p>A vane assembly for a gas turbine engine comprising a number of radial loading elements disposed between lugs of the vane ring and the vane support, such as to generate a radial load force against the vane ring. The radial load force prevents unwanted relative movement between the vane ring and the vane support during operation of the gas turbine engine.</p>
申请公布号 CA2638542(C) 申请公布日期 2015.12.15
申请号 CA20082638542 申请日期 2008.08.07
申请人 PRATT & WHITNEY CANADA CORP. 发明人 DUROCHER, ERIC;CARON, YVES
分类号 F01D9/02;F01D25/04 主分类号 F01D9/02
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