Invention Grant
US09562438B2 Under-root spacer for gas turbine engine fan blade 有权
用于燃气涡轮发动机风扇叶片的根部间隔物

Under-root spacer for gas turbine engine fan blade
Abstract:
A gas turbine engine rotor includes a hub having a slot. A blade includes a root received in the slot. An under-root area is provided between the root and the fan hub in the slot. A spacer includes first and second portions that cooperate with one another to provide an adjustment feature with discrete height settings. The adjustment feature provides different radial heights of the spacer. The spacer is arranged in the under-root area beneath the root.
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