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Control device of the stop for large masses are provided with a high speed

机译:大质量挡块的控制装置具有高速

摘要

1,208,820. Controlling braking electrically. SOC. ALASACIENNE DE CONSTRUCTIONS ATOMIQUES DE TELECOMMUNICATIONS ET D'ELECTRONIQUE "ALCATEL". May 31, 1968 [June 2, 1967], No.26368/68. Heading G1N. An arrangement for stopping an aircraft arriving at the end of a runway at a speed higher than that corresponding to the stopping distance comprises a net 3 and two restraining straps 1, 2 which are retarded by brakes 4, 5 in dependence on control signals derived from measurements of the strap speed and the length of strap unwound. As shown in Fig. 5, the slider of a potentiometer 27 having a desired non-linear characteristic is moved in dependence on the length of strap 2 unwound and a tachometer 28 generates a voltage proportional to the speed of the strap. The output of a difference amplifier 30 is fed to servomechanisms 14, 15 to control the brakes. The voltage applied to the potentiometer 27 is set in accordance with the arrival speed of the aircraft. Initially, relays 19, 25 are in their rest positions R and a voltage source 20, the voltage of which corresponds to the highest anticipated arrival speed, is connected through an operational amplifier 22 to the potentiometer 27. When an aircraft arrives at the net and the straps have started to unwind, relay 19 is energized so that a capacitor 23 in the feedback circuit of amplifier 22 is charged from a voltage source 26 whereby the voltage applied to the potentiometer 27 decreases. When the output of a difference amplifier 29 becomes slightly positive, relay 25 is energized thereby disconnecting the source 26 so that the voltage fed to the potentiometer 27 remains constant from then on at a value appropriate to the arrival speed of the aircraft. Each strap may have its own control circuit, the brakes being controlled independently or by the average of the outputs of the control circuits. By comparing the lengths of the straps unwound, action may be taken to correct the direction of travel of the aircraft. A plurality of arrangements may be used having different characteristics.
机译:1,208,820。电动控制制动。 SOC。阿拉斯加国家建筑原子能公司和“阿尔卡特”电子公司。 1968年5月31日[1967年6月2日],编号26368/68。标题G1N。用于使飞机以比对应于停止距离的速度更高的速度停止到达跑道末端的飞机的装置包括网3和两个约束带1、2,所述约束带1、2由制动器4、5根据从中得出的控制信号而减速。皮带速度和皮带长度的测量方法。如图5所示,具有所需非线性特性的电位计27的滑块根据解绕的带子2的长度而移动,并且转速表28产生与带子的速度成比例的电压。差动放大器30的输出被馈送到伺服机构14、15以控制制动器。根据飞行器的到达速度来设置施加到电位计27的电压。最初,继电器19、25处于其静止位置R,并且电压源20(其电压对应于最高预期到达速度)通过运算放大器22连接到电位计27。当带子开始松开时,继电器19通电,放大器22反馈电路中的电容器23从电压源26充电,从而降低了施加到电位计27的电压。当差动放大器29的输出略微为正时,继电器25通电,从而断开电源26,从而从那时起,馈入电位计27的电压保持恒定,其值适合于飞机的到达速度。每个皮带可以具有其自己的控制电路,制动器可以独立控制,也可以通过控制电路的平均输出来控制。通过比较解开的带子的长度,可以采取措施来校正飞机的行进方向。可以使用具有不同特性的多种布置。

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