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Kinematic sensor for aerodynamic angle and true airspeed

机译:运动学传感器,用于空气动力学角度和真实空速

摘要

The utility model relates to the field of instrumentation, in particular to devices for measuring the magnitude (module) and direction angle (aerodynamic angle) of the true airspeed vector of an aircraft, in particular an airplane. The kinematic sensor of the aerodynamic angle and true airspeed contains a board with receivers of parameters of the incident air flow. Two combined pairs of piezoelectric emitters-receivers of ultrasonic vibrations mounted orthogonally to each other at an angle Θ = 45 ° to the axis of the board, relative to which the value of the aerodynamic angle is measured, are installed on the outer surface of the circuit board, streamlined by the incoming air stream. Emitters emit ultrasonic vibrations in the direction of the incoming air flow and against the direction of the incoming flow. The receivers of ultrasonic vibrations through the elements of the measuring circuit are connected to the inputs of the frequency subtraction circuits, the outputs of which are connected to the input of the calculator, the output of which is the digital outputs by the aerodynamic angle α and the true air speed V, determined in accordance with the algorithm M де L is the distance between the piezoelectric emitters and ultrasonic receivers fluctuations; Δƒ = ƒ-ƒ 'and Δƒ = ƒ-ƒ'; ƒƒ 'and ƒ, ƒ' are the frequencies of ultrasonic vibrations perceived by the pairs of receivers in opposite directions. The technical result in the implementation of the claimed solution is to simplify the design and increase the accuracy of the measurement by reducing the number of receivers for recording the parameters of the incoming air flow, reducing the number of measuring channels and simplifying a measuring circuit and a device for processing information and generating output signals and, as a result, ensuring competitiveness of application on le atelnyh devices, including aircraft of various classes and purposes, the kinematic sensor aerodynamic angle and true airspeed implementing kinematic measuring method. 6 ill.
机译:本实用新型涉及仪器领域,尤其涉及一种用于测量飞机,特别是飞机的真实空速矢量的大小(模数)和方向角(空气动力角)的装置。空气动力学角度和真实空速的运动学传感器包含一块带有接收入射气流参数的接收器的板。两对超声振动的压电发射器和接收器组合成两对,它们彼此正交安装,与板的轴线成θ= 45°角,相对于该板的空气动力学角度值进行测量,电路板,由进入的气流简化。发射器沿进入气流的方向并与进入气流的方向相反地发出超声波振动。通过测量电路元件的超声波振动的接收器连接到频率减法电路的输入,频率减法电路的输出连接到计算器的输入,计算器的输出是空气动力角α和f的数字输出。根据算法MдL确定的真实风速V是压电发射器和超声接收器波动之间的距离; Δƒ=ƒ-ƒ'和Δƒ=ƒ-ƒ'; ƒ'和ƒ,ƒ'是成对的接收器在相反方向上感知到的超声振动的频率。实施要求保护的解决方案的技术结果是,通过减少用于记录进入气流参数的接收器的数量,减少测量通道的数量并简化测量电路,简化了设计并提高了测量的准确性。一种用于处理信息并生成输出信号的设备,从而确保在各种设备和用途的航空器,运动传感器空气动力学角度和实际空速实现运动学测量方法等应用中具有竞争力。 6病了。

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