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Development of a Cyclogyro-Based Flying Robot With Variable Attack Angle Mechanisms

机译:基于细胞学的具有可变迎角机制的飞行机器人的研制

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This paper presents an experimental study on the development of a cyclogyro-based flying robot with a new variable angle of attack mechanism. A cyclogyro is a flying machine supported in the air by power-driven rotors that rotate about a horizontal axis, like the paddle-wheels of a steamboat. Machines of this type have been designed by some companies but there has been no record of any successful flights. Our design starts with a new variable angle of attack mechanism with an eccentric (rotational) point in addition to a rotational point connecting to a motor. The main feature of the mechanism with the eccentric rotational point is the ability to change attack of angles in accordance with the wing positions (as determined by the rotational angles of the cyclogyro) without actuators. The design parameters (wing span, the number of wings, and eccentric distance) of the flying robot are determined through a series of experiments. Experimental results show that the cyclogyro-based flying robot with the new variable angle of attack mechanism is capable of generating sufficient lift force for flying.
机译:本文提出了一种具有新型可变迎角机构的基于陀螺仪的飞行机器人开发的实验研究。摆线陀螺仪是一种飞行器,它由绕着水平轴旋转的动力转子支撑在空中,就像汽船的桨轮一样。一些公司已经设计了这种类型的机器,但是没有任何成功飞行的记录。我们的设计从新的可变攻角机构开始,该机构具有连接到电动机的旋转点以及偏心(旋转)点。具有偏心旋转点的机构的主要特征是无需执行器即可根据机翼位置(由旋翼陀螺的旋转角度确定)改变角度迎角的能力。飞行机器人的设计参数(机翼跨度,机翼数和偏心距)是通过一系列实验确定的。实验结果表明,具有新型可变迎角机构的基于陀螺仪的飞行机器人能够产生足够的升力进行飞行。

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