发明名称 Turbine engine blade and method of manufacturing said blade
摘要 A plate (10) closing the main part (5) of a two-part blade. An internal cavity (8) is closed by the plate (10). Around the bearing surface (12) of the plate (10), a groove (14) receives a resilient seal (11), and the outer edge (29) of the plate (10) extends over the groove (14) to compress the seal (11) and ensure excellent leakproofing. The position of the plate (10) can be ensured by centring pins which penetrate into holes adjacent to the seal (11) which then fills them when the pins have been removed, thus completing the closure of the cavity (8). Application: in particular for stationary gas straightening vanes in turbine engines.
申请公布号 GB2505845(A) 申请公布日期 2014.03.12
申请号 GB20140000052 申请日期 2012.07.17
申请人 SNECMA 发明人 THIERRY PAPIN;LISE LACROIX;DOMINIQUE RAULIN
分类号 F01D5/14;F01D9/04 主分类号 F01D5/14
代理机构 代理人
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