首页> 外国专利> AEROMECHANICAL METHOD OF MEASUREMENT OF AIR-SPEED PARAMETERS OF FLIGHT TRAJECTORY AND DEVICE FOR ITS IMPLEMENTATION

AEROMECHANICAL METHOD OF MEASUREMENT OF AIR-SPEED PARAMETERS OF FLIGHT TRAJECTORY AND DEVICE FOR ITS IMPLEMENTATION

机译:航空弹道空速参数的气动测量方法及其实现

摘要

FIELD: physics, measurement.;SUBSTANCE: invention is related to the field of measuring equipment and may find application, in particular, in measurement of air-speed parameters of airplane flight trajectory, in particular, such as velocity head, angle of attack, coefficient of aerodynamic lift, airplane mass, position of airplane center of gravity and so on. Device for measurement of air-speed parameters of flight trajectory consists of pressure difference sensors group, group of functional transducers, amplifiers, group of indicators. Device operation consists in processing of voltages of output signals from pressure difference sensor, which are installed in appropriate specially selected points of airplane aerodynamic surface. Measured signals from pressure difference sensors are transformed with the help of device functional transducers, and by preset functional dependences values of output voltages of functional transducers are calculated, which are proportional to desired air-speed parameters of flight trajectory.;EFFECT: higher accuracy of measurement.;2 cl, 4 dwg
机译:技术领域本发明涉及测量设备领域,并且尤其可以在飞机飞行轨迹的空速参数的测量中找到应用,例如速度头,攻角,空气动力升力系数,飞机质量,飞机重心位置等。飞行轨迹的空速参数测量装置包括压差传感器组,功能传感器组,放大器,指示器组。设备操作包括处理来自压差传感器的输出信号的电压,该压力差传感器安装在飞机空气动力学表面的特别选定的适当位置。来自压力差传感器的测量信号在设备功能传感器的帮助下进行转换,并通过预设功能相关性来计算功能传感器的输出电压值,这些值与所需的飞行轨迹空速参数成比例;效果:更高的精度测量值; 2 cl,4 dwg

著录项

  • 公开/公告号RU2336533C2

    专利类型

  • 公开/公告日2008-10-20

    原文格式PDF

  • 申请/专利权人 ZHIVETIN VLADIMIR BORISOVICH;

    申请/专利号RU20060136161

  • 发明设计人 ZHIVETIN VLADIMIR BORISOVICH;

    申请日2006-10-13

  • 分类号G01P5/14;B64C13/16;

  • 国家 RU

  • 入库时间 2022-08-21 19:50:31

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