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METHODS, SYSTEMS, AND HEADER STRUCTURES FOR TOOLING FIXTURE AND POST-CURE FIXTURE CALIBRATION

机译:用于固定治具和后固化治具的方法,系统和头结构

摘要

Systems and methods provide for the determination and correction of tooling deviation by comparing two different three-dimensional surface scans of a composite panel after curing. Such methods and systems may allow for less accurate post-cure fixturing (e.g., holding the panel in a less constrained state, as compared to prior art techniques), while still maintaining a sufficient amount of precision for predictive shimming and shimless techniques. Methods include performing a first three-dimensional surface scan, performing a second three-dimensional surface scan, and comparing the two to determine a deformation function corresponding to tooling deviation. In some systems, a header structure is used to hold the composite panel in a nominal configuration for the second three-dimensional surface scan. In some systems, scanning devices perform mirrored scanning on either side of the composite panel, using a common reference frame.
机译:系统和方法通过比较固化后复合板的两个不同的三维表面扫描来确定和校正工具偏差。这样的方法和系统可以允许较不精确的固化后固定(例如,与现有技术相比,将板保持在较少受约束的状态),同时仍保持足够的精度以用于预测匀场和无匀场技术。方法包括执行第一三维表面扫描,执行第二三维表面扫描,以及将两者进行比较以确定与工具偏差相对应的变形函数。在一些系统中,头部结构用于将复合面板保持在名义配置中以用于第二次三维表面扫描。在某些系统中,扫描设备使用公共参考框架在复合面板的任一侧执行镜像扫描。

著录项

  • 公开/公告号US2020326689A1

    专利类型

  • 公开/公告日2020-10-15

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US201916384533

  • 发明设计人 CLIFFORD D. BOROWICZ;

    申请日2019-04-15

  • 分类号G05B19/418;B29C70/54;G06T7;

  • 国家 US

  • 入库时间 2022-08-21 11:26:17

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