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在飞机机翼喷丸壁板的检验过程中,利用点阵化三坐标数控定位技术对飞机机翼喷丸壁板非检测部位进行柔性定位支撑,并施加壁板检验所需的外部压力;通过三坐标数控定位器上部的力传感器测量壁板检验允许施加的外部压力,利用高精度的测距传感器在平面内的两自由度移动对飞机机翼喷丸壁板检测部位进行测量,测量数据实时反馈回数据库,将数据模拟成数学模型与检测数学模型进行比对,测量位置的实际差值即为检验产品的制造误差;检测完成后,计算机软件自动生成检验报告。
In the testing process of the aircraft wing peening wall panel, the positioning and support of the non-detection site of the shot peening wall of the aircraft wing is flexibly supported and the external pressure required for siding inspection is applied by using the arrayed three-coordinate numerical control positioning technology; Three coordinate CNC positioner upper force sensor to measure the wall plate test allows the application of external pressure, the use of high-precision distance measuring sensor in the plane of the two degrees of freedom to move the aircraft wing peening wall detection site measurements, real-time measurement data Feedback to the database, the data is modeled as a mathematical model and detection of mathematical models for comparison, the actual position of the measurement error is to test the product manufacturing error; test is completed, the computer software automatically generates inspection reports.