Invention Grant
US09410436B2 Blade disk arrangement for blade frequency tuning 有权
用于叶片频率调谐的刀片盘布置

Blade disk arrangement for blade frequency tuning
Abstract:
A gas turbine engine and a method of tuning a rotor in the gas turbine engine wherein the rotor includes an array of blades extending from a rotor hub each having an airfoil mounted to a blade platform. The method includes adding or removing material from bladed rotor projections to alter the mass of the rotor and change the frequency of the respective airfoil.
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