TURBINE COMPONENT PATCH DELIVERY SYSTEMS AND METHODS
    33.
    发明申请
    TURBINE COMPONENT PATCH DELIVERY SYSTEMS AND METHODS 有权
    涡轮组件分配系统和方法

    公开(公告)号:US20150174838A1

    公开(公告)日:2015-06-25

    申请号:US14568458

    申请日:2014-12-12

    Abstract: A turbine component patch delivery system can include a compressed gas source fluidly connected to a delivery line comprising a dispensing end. The turbine component patch delivery system can further include one or more turbine component patch carriers that can be projected out of the dispensing end of the delivery line by the compressed gas source, wherein each of the one or more turbine component patch carriers comprise a turbine component patch material housed within a breakaway shell.

    Abstract translation: 涡轮机部件补片输送系统可以包括流体连接到包括分配端的输送管线的压缩气体源。 涡轮机部件补片输送系统还可以包括一个或多个涡轮机部件补片载体,其可以通过压缩气体源从输送管线的分配端部突出出来,其中,一个或多个涡轮机部件补片载体中的每一个包括涡轮部件 贴片材料容纳在分离的外壳内。

Patent Agency Ranking