发明名称 Gas turbine engine balancing
摘要 An apparatus and method for balancing a gas turbine engine rotor includes a plurality of balancing weights adapted to be selectively attached to at least one of inlets or outlets of a cooling passage of the rotor. The weights include cooling access which permits coolant to communicate with the cooling passage.
申请公布号 US8246305(B2) 申请公布日期 2012.08.21
申请号 US20090572031 申请日期 2009.10.01
申请人 LECUYER DANIEL;CHATELOIS BRUNO;DI PAOLA FRANCO;PRATT & WHITNEY CANADA CORP. 发明人 LECUYER DANIEL;CHATELOIS BRUNO;DI PAOLA FRANCO
分类号 F01D5/08;F01D5/10 主分类号 F01D5/08
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