A method of balancing an assembly of rotary parts of a gas turbine engine (10) comprising measuring at least one of the concentricity and parallelism of each component and considering globally all possible component stacking positions to generate an optimized stacking position for each component of the assembly to minimize assembly unbalance.
申请公布号
CA2694165(A1)
申请公布日期
2009.01.29
申请号
CA20082694165
申请日期
2008.06.12
申请人
PRATT & WHITNEY CANADA CORP.
发明人
WALTERS, CAMERON TODD;BENOIT, RICHARD;BELLEMARE, ALPHONSE;ROBINSON, RONALD LESLIE;WANG, JIEMIN;HARRIS, HARRY
