发明名称 TURBINE ENGINE SHAFT
摘要 A shaft for a turbine engine, the shaft having a cavity subdivided axially into first and second chambers. The shaft also includes a distributor member having an axial duct, a first radial orifice, and a second radial orifice. The axial duct has an open first end and a second end closed in the axial direction. The first radial orifice connects the second end of the axial duct to the first chamber in order to feed a first bearing with lubricating fluid, and the second radial orifice connects the second end of the axial duct to the second chamber to feed a second bearing with lubricating fluid. The first radial orifice and the second radial orifice of the distributor member are at substantially equal axial distances from the lubricating fluid inlet.
申请公布号 US2013177390(A1) 申请公布日期 2013.07.11
申请号 US201313732661 申请日期 2013.01.02
申请人 MICROTURBO;MICROTURBO 发明人 COT SERGE;LALANNE CLEMENT
分类号 F01D25/18 主分类号 F01D25/18
代理机构 代理人
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