发明名称 Turbine engine spacer
摘要 A turbine (10) is provided and includes a spacer (80) having an annular body (81) formed with opposing outward and inward surfaces (82, 83) and an orifice (90) extending through the body from the outward to the inward surface, an assembly (100) to secure the spacer (80) around a rotor (30) axially between sequential buckets (110, 111) of a forward turbine stage and an aft turbine stage, the spacer (80) forming an annular passage (120) around the rotor into which a fluid flows through the orifice and a circuit (130) fluidly coupled to the annular passage (120) to deliver the fluid from between the sequential buckets (110, 111) of the forward turbine stage and the aft turbine stage to an axial location forward of the forward turbine stage.
申请公布号 EP2378070(A3) 申请公布日期 2014.09.24
申请号 EP20110162097 申请日期 2011.04.12
申请人 GENERAL ELECTRIC COMPANY 发明人 BHAGAVETHEESWARAN, ANANTHA PADMANABHAN;PRUTHI, ROHIT
分类号 F01D5/08;F01D9/06;F01D11/00 主分类号 F01D5/08
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