发明公开
EP2586968A3 Secondary flow arrangement for slotted rotor 审中-公开
开槽转子的二次流动布置

Secondary flow arrangement for slotted rotor
摘要:
A rotor (60) for a gas turbine engine includes a plurality of blades (64) which extend from a rotor disk (66) and at least one spacer (62CA) adjacent to the plurality of blades (64). A flow passage is defined between the rotor disk (66) and the blades (62) and spacer (62CA). A plurality of inlets (88) are formed within the spacer (62CA) to pump air into the flow passage.
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