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    • 1. 发明授权
    • Method and measuring device for measuring overlap on an aircraft wing
    • 用于测量飞机机翼上重叠的方法和测量装置
    • US07938000B2
    • 2011-05-10
    • US12554337
    • 2009-09-04
    • Michael Binder
    • Michael Binder
    • G01N7/22
    • G01M9/08
    • The present invention relates to a method and a measuring device for measuring and displaying the overlap between a rear edge of an aircraft wing and a front edge of a landing flap fixed thereto. In accordance with the invention, only the difference in the positions of the rear edge of the aircraft wing and the front edge of the landing flap relative to the longitudinal direction of the aircraft is determined. For this purpose, a first sensor is positioned, as a reference of sorts, at one of the two positions, for example at the rear edge of the aircraft wing, and the display is then reset to zero or to another reference value. By positioning the second sensor, which is also rigidly connected to the calliper, at the other respective position, for example at the front edge of the landing flap, the difference between the front edge of the landing flap relative to the rear edge of the aircraft wing is established. This value, which directly indicates the overlap value, can now be read directly from the display of the calliper.
    • 本发明涉及一种用于测量和显示飞行器机翼的后边缘与固定在其上的着陆翼的前缘之间的重叠的方法和测量装置。 根据本发明,仅确定飞行器机翼的后边缘和着陆翼片的前缘相对于飞行器的纵向的位置之间的差异。 为此目的,第一传感器作为各种类型的参考,位于两个位置中的一个位置,例如在飞行器机翼的后边缘处,然后将显示器复位到零或另一个参考值。 通过将刚好连接到卡钳的第二传感器定位在另一个相应的位置处,例如在着陆挡板的前边缘处,着陆挡板的前边缘与飞行器的后边缘之间的差异 机翼成立。 直接指示重叠值的该值现在可以直接从卡尺的显示中读取。