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US08944762B2 Spoked spacer for a gas turbine engine 有权
用于燃气涡轮发动机的间隔器

Spoked spacer for a gas turbine engine
Abstract:
A spacer for a gas turbine engine includes a rotor ring defined along an axis of rotation and a plurality of core gas path seals which extend from the rotor ring, each of the plurality of core gas path seals extend from the rotor ring at an interface, the interface defined along a spoke.
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