Auto-adaptive braze dispensing systems and methods

    公开(公告)号:US10780515B2

    公开(公告)日:2020-09-22

    申请号:US15963230

    申请日:2018-04-26

    Abstract: Systems and methods for moving a substrate to a vision system using a robot; using the vision system to determine where a braze material is to be applied to the substrate; moving the substrate to a braze dispenser using the robot; applying a braze material to the substrate using the braze dispenser based on the determination from the vision system; and using the vison system to determine whether to apply additional braze to the substrate, including for the substrate of a component for gas turbine engine, such as configured for use in an aircraft.

    Multi-Airfoil Split and Rejoin Method
    5.
    发明申请
    Multi-Airfoil Split and Rejoin Method 审中-公开
    多翼分裂和重合法

    公开(公告)号:US20150369070A1

    公开(公告)日:2015-12-24

    申请号:US14762630

    申请日:2013-12-16

    Abstract: A method for working an airfoil cluster is disclosed. The method may include attaching a first datum to a first portion of the airfoil cluster, and joining a second portion of the airfoil cluster to the first portion, the second portion having a second datum substantially aligned with the first datum in a common plane spaced away from the first and second portions.

    Abstract translation: 公开了一种用于加工翼型组的方法。 该方法可以包括将第一基准附接到翼型群的第一部分,以及将翼型群的第二部分连接到第一部分,第二部分具有基本上与第一基准对准的公共平面间隔开的第二基准 从第一和第二部分。

    AUTO-ADAPTIVE BRAZE DISPENSING SYSTEMS AND METHODS

    公开(公告)号:US20190329343A1

    公开(公告)日:2019-10-31

    申请号:US15963230

    申请日:2018-04-26

    Abstract: Systems and methods for moving a substrate to a vision system using a robot; using the vision system to determine where a braze material is to be applied to the substrate; moving the substrate to a braze dispenser using the robot; applying a braze material to the substrate using the braze dispenser based on the determination from the vision system; and using the vison system to determine whether to apply additional braze to the substrate, including for the substrate of a component for gas turbine engine, such as configured for use in an aircraft.

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