发明名称 TOOL FOR BALANCING A TURBINE ENGINE MODULE
摘要 The invention relates to tool for balancing a turbine engine module (10) in a balancer, this module including at least one stator housing (14) and one rotor (16) comprising a shaft (18) of longitudinal axis A and at least one stage of blades (20) surrounded by said stator housing (14), said tool comprising at least one balancing frame (14), comprising guide bearings for the rotor (16), first and second means (30, 32) configured to be attached to said stator housing (14), third and fourth means (34, 36) provided on said frame (24), to attach said first and second means (30, 32) to said frame, fifth means for transporting the frame (24), and sixth means for supporting the frame (84, 94), provided on said frame (24) and engaging equally with both the balancer and the fifth means for transporting the frame (24).
申请公布号 WO2017001745(A1) 申请公布日期 2017.01.05
申请号 WO2016FR51513 申请日期 2016.06.21
申请人 SAFRAN AIRCRAFT ENGINES 发明人 LUINAUD, Alain, Roland;DECOCQ, Alain;VIVIANDE, François
分类号 G01M1/02;F16F15/32 主分类号 G01M1/02
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