基于激光跟踪仪的大型结构元件静载荷多位置运动控制

Многопозиционный Контроль, С Помощью, Лазерного Трекера, Перемещений Элементов, Крупногабаритной Конструкции, В Процессе, Статического Нагружения, Н. А. Сазонникова
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引用次数: 0

摘要

在航空航天产品的制造中,最重要的任务之一是在生产的各个阶段控制其几何参数,并评估其是否符合设计文件的要求。使用激光自动测量系统可以提高测量速度,并使用产品数字模型作为参考点。使用激光自动测量系统,如激光扫描仪和激光跟踪器,可以获得解决此类问题的最佳结果。本文针对不同的运输条件,采用两种静态加载方式,采用双位置测量系统对所设计运载火箭的铝合金燃料部件油箱进行控制。在这种情况下,线性尺寸误差不应超过150m。建立了多位置测量系统的数学模型,得到了测量不确定度方程。在这种情况下,表示测量对象的参考点和控制点的坐标确定误差之差的误差函数值应该是最小的。该数学模型将进一步用于数值建模,以选择测量系统的最佳配置,以便在静态加载过程中对油箱几何参数进行多位置控制。
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Multi-position control of movements of large-sized structural elements during static loading using a laser tracker
One of the most important tasks in the manufacturing of aerospace products is the control of their geometric parameters at various stages of production and assessment of their compliance with the requirements of design documentation. The use of laser automated measuring systems makes it possible to increase the measurement speed and to use the product digital model as a reference point. The best results in solving such problems can be obtained using laser automated measuring systems, such as laser scanners and laser trackers. In this paper a two-position measurement system is applied to control the aluminum alloy fuel component tank of the designed launch vehicle with two modes of static loading, corresponding to different transportation conditions. In this case, the linear dimension error should not exceed 150 m. A mathematical model of a multi-position measuring system is constructed and measurement uncertainty equations are obtained. In this case, the error function value that represents the difference between the errors in determining the coordinates of the reference points and the controlled points of the measurement object should be minimal. This mathematical model will be further used for numerical modeling that will allow selecting the optimal configuration of a measuring system for multi-position control of the tank geometric parameters in the static loading process.
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