Invention Grant
US08961132B2 Secondary flow arrangement for slotted rotor 有权
开槽转子的二次流动布置

Secondary flow arrangement for slotted rotor
Abstract:
A rotor for a gas turbine engine includes a plurality of blades which extend from a rotor disk and at least one spacer adjacent to the plurality of blades. A flow passage is defined between the rotor disk and the blades and spacer. A plurality of inlets are formed within the spacer to pump air into the flow passage.
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