发明申请
US20130108445A1 SPOKED ROTOR FOR A GAS TURBINE ENGINE 有权
用于气体涡轮发动机的旋转转子

SPOKED ROTOR FOR A GAS TURBINE ENGINE
摘要:
A rotor for a gas turbine engine includes a plurality of blades which extend from a rotor disk, each of the plurality of blades extend from the rotor disk at an interface, the interface defined along a spoke.
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