Invention Grant
US08668457B2 Gas turbine engine trim balance 有权
燃气涡轮发动机装备平衡

Gas turbine engine trim balance
Abstract:
A trim balance for a gas turbine engine having a hollow rotatable rotor shaft includes an elongate support rod adapted for longitudinal accommodation within and mounting on an interior surface of the rotor shaft and one or more apertured balance weights supported on the support rod which extends through the weight apertures and a weight retainer for retaining the weights on the support rod.
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