发明名称 RADIAL LOADING ELEMENT FOR TURBINE VANE
摘要 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.
申请公布号 US2009155068(A1) 申请公布日期 2009.06.18
申请号 US20070955867 申请日期 2007.12.13
申请人 DUROCHER ERIC;CARON YVES 发明人 DUROCHER ERIC;CARON YVES
分类号 F01D9/04 主分类号 F01D9/04
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