GAS TURBINE ENGINE ROTOR DRAIN FEATURE
    1.
    发明申请
    GAS TURBINE ENGINE ROTOR DRAIN FEATURE 有权
    气体涡轮发动机转子排水功能

    公开(公告)号:US20140147249A1

    公开(公告)日:2014-05-29

    申请号:US13658876

    申请日:2012-10-24

    CPC classification number: F01D25/18 F01D5/06 F01D25/32 F02C7/06

    Abstract: An assembly for a gas turbine engine includes a rotor formed by a drum and a hub. The drum has a generally conically shaped inner surface that defines a flow path along a first cavity. The hub is connected to the drum and has a conically shaped inner surface that defines a flow path along a second cavity.

    Abstract translation: 用于燃气涡轮发动机的组件包括由滚筒和轮毂形成的转子。 滚筒具有大致圆锥形的内表面,其限定沿着第一空腔的流动路径。 轮毂连接到滚筒并且具有限定沿着第二腔的流动路径的锥形内表面。

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