ABRASIVELY MACHINED GAS TURBINE COMPONENTS
    5.
    发明申请
    ABRASIVELY MACHINED GAS TURBINE COMPONENTS 审中-公开
    易磨机气涡轮组件

    公开(公告)号:US20160319834A1

    公开(公告)日:2016-11-03

    申请号:US15106015

    申请日:2014-11-19

    Abstract: A method of making a gas turbine engine component includes providing a nickel based alloy workpiece and removing material from the workpiece surface using an abrasive machining operation to form an axisymmetric surface on the workpiece using the abrasive machining operation. The workpiece axisymmetric surface and workpiece interior portion have uniform hardness and micro structure following the removing operation.

    Abstract translation: 一种制造燃气涡轮发动机部件的方法包括:使用磨料加工操作提供镍基合金工件和从工件表面去除材料,以使用磨削加工操作在工件上形成轴对称表面。 工件轴对称表面和工件内部部分具有均匀的硬度和微观结构。

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