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Aircraft anemometer for correction in weight measurement - senses wind speed and direction for on board computer calculating take off weight and centre of gravity

机译:用于校正重量的飞机风速计-感测风速和风向,用于机载计算机计算起飞重量和重心

摘要

A vertical vane is attached by a flexible strip to an element fixed to a hollow shaft. The vane rotates the shaft which drives the rotor in a stator of an angular position sensor. The flexible strip is supported by a ball on the cap on a solid shaft inside the hollow shaft in which it moves longitudinally. It is supported at the other end by a flexible spring. This enables the force exerted by the wind on an oblique surface to move a magnetic paddle. This transmits the measurement through a stator of an inductive linear displacement sensor. The detector is enclosed in a case with a fixing flange enabling it to be mounted on an aircraft. The sensor outputs giving wind speed and direction are transmitted to a computer with data from sensors on the undercarriage to permit precise calculation of weight and c. of g.
机译:竖直叶片通过柔性条带附接到固定至空心轴的元件。叶片使轴旋转,该轴在角度位置传感器的定子中驱动转子。柔性条通过球支撑在空心轴内部的实心轴上的盖上,空心轴在其中纵向移动。它的另一端由柔性弹簧支撑。这使得风在倾斜表面上施加的力能够移动磁性桨。这将测量结果通过感应线性位移传感器的定子传输。探测器被固定在一个带有固定法兰的外壳中,使其可以安装在飞机上。给出风速和风向的传感器输出与底盘上传感器的数据一起传输到计算机,以精确计算重量和c。克

著录项

  • 公开/公告号FR2513380A1

    专利类型

  • 公开/公告日1983-03-25

    原文格式PDF

  • 申请/专利权人 SFENA;

    申请/专利号FR19810017965

  • 发明设计人 LOUIS SACRE;

    申请日1981-09-23

  • 分类号G01P5/02;G01P13/02;

  • 国家 FR

  • 入库时间 2022-08-22 10:00:27

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