发明名称 BLADES FOR A GAS TURBINE ENGINE WITH INTEGRATED SEALING PLATE AND METHOD
摘要 A blade for a rotor assembly including a root portion, a platform with an overhang, an airfoil portion and a sealing plate. The sealing plate protrudes from the blade along a circumferential direction.
申请公布号 CA2552214(C) 申请公布日期 2014.09.02
申请号 CA20062552214 申请日期 2006.07.12
申请人 PRATT & WHITNEY CANADA CORP. 发明人 BOUCHARD, GUY;TRUMPER, RONALD
分类号 F01D5/14;F02C7/00 主分类号 F01D5/14
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