SELECTIVE MODIFICATION OF BUILD STRATEGY PARAMETER(S) FOR ADDITIVE MANUFACTURING

    公开(公告)号:US20190054530A1

    公开(公告)日:2019-02-21

    申请号:US15677417

    申请日:2017-08-15

    Abstract: A computerized method, system, program product and additive manufacturing (AM) system are disclosed. Embodiments provide for modifying object code representative of an object to be physically generated layer by layer by a computerized AM system using the object code. The computerized method may include providing an interface to allow a user to manually: select a region within the object in the object code, the object code including a plurality of pre-assigned build strategy parameters for the object that control operation of the computerized AM system, and selectively modify a build strategy parameter in the selected region in the object code to change an operation of the computerized AM system from the plurality of pre-assigned build strategy parameters during building of the object by the computerized AM system.

    METHODS FOR TESTING TURBINE BLADES
    47.
    发明申请
    METHODS FOR TESTING TURBINE BLADES 有权
    测试涡轮叶片的方法

    公开(公告)号:US20140115892A1

    公开(公告)日:2014-05-01

    申请号:US13665364

    申请日:2012-10-31

    Abstract: Methods for testing turbine blades. One method for testing turbine blades includes measuring dimensions of each of a first set of turbine blades. The method also includes testing airflow through first openings in each of the first set of turbine blades to determine airflow properties of each of the first set of turbine blades. The method includes determining a relationship between the dimensions and the airflow properties of each of the first set of turbine blades. The method includes measuring dimensions of each of a second set of turbine blades. The method also includes determining airflow properties for each of the second set of turbine blades based at least partially on the dimensions of the second set of turbine blades and the relationship.

    Abstract translation: 涡轮叶片测试方法。 用于测试涡轮叶片的一种方法包括测量第一组涡轮叶片中的每一个的尺寸。 该方法还包括通过第一组涡轮叶片中的每一个中的第一开口测试气流,以确定第一组涡轮叶片中的每一个的气流特性。 该方法包括确定第一组涡轮叶片中的每一个的尺寸和气流性质之间的关系。 该方法包括测量第二组涡轮叶片中的每一个的尺寸。 该方法还包括至少部分地基于第二组涡轮叶片的尺寸和关系确定第二组涡轮叶片中的每一个的气流特性。

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