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Fail safe attaching parachute model airplane

机译:故障安全附加降落伞模型飞机

摘要

PURPOSE:To prevent disabled control by providing two receivers and two batteries connecting to them respectively. CONSTITUTION:When either a receiver 1 or 2 is faulty, for example, the receiver 1 receives a command to return. In this case, the direction lope is for left turning only, the aircraft flies on a desired sky point by controlling the turning radius properly and the altitude is controlled so that the aircraft is not damaged even on landing or falling by using a left turning servo motor 4 and a right elevating angle servo motor 6 and the craft is recovered by stopping the engine by an engine stop servo motor 5. When the receiver 1 is faulty, the receiver 2 controls a left elevating angle servo motor 7, a right turning servo motor 8 and an engine rotation number control servo motor 9 to recover the aircraft. When any of batteries 11, 12, 13 and 14 is worn out, the aircraft is recovered by applying the similar control. Thus, disabled control is prevented even when a trouble takes place to a part of the controller.
机译:目的:通过分别提供两个接收器和两个电池来防止禁用控制。章程:例如,当接收器1或2出现故障时,接收器1会收到一条返回命令。在这种情况下,方向坡度仅用于左转,通过适当控制转弯半径,飞机可以在所需的天空点上飞行,并且可以控制高度,从而即使使用左转舵机降落也不会损坏飞机电动机4和直角伺服电动机6,并且通过发动机停止伺服电动机5使发动机停止运转,从而回收船舶。当接收器1发生故障时,接收器2控制左仰角伺服电动机7,右转向伺服器7。电动机8和发动机转数控制伺服电动机9以恢复飞机。当电池11、12、13和14中的任何一个磨损时,可以通过应用类似的控制来恢复飞机。因此,即使在控制器的一部分发生故障时,也可以防止无效控制。

著录项

  • 公开/公告号JP2561536B2

    专利类型

  • 公开/公告日1996-12-11

    原文格式PDF

  • 申请/专利权人 CATERPILLAR MITSUBISHI LTD;

    申请/专利号JP19890131433

  • 发明设计人 ABE TOSHIRO;

    申请日1989-05-26

  • 分类号H04Q9/00;A63H30/04;B64C19/00;

  • 国家 JP

  • 入库时间 2022-08-22 03:29:31

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