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DEVELOPMENT OF MEASURING SYSTEM OF GRAVITY CENTER IN UNBALANCED MODELS

机译:不平衡模型中重力中心测量系统的发展

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The rotor system is core part in the unmanned helicopter, and it is important to the aviation performance, vibration and noise. In the system, rotor blade is usually manufactured manually because of its complex shape, materials, and production volume. Static balancing of the rotor blade should be controlled precisely in order to ensure the stability during the flight. But the cross section of the rotor blade is not symmetrical and very unbalance. In the industrial applications, there are many unbalanced models such as rotor blade in helicopter, small-sized precision motor, and rotating fans. In the real products, the centre of gravity does not usually accord with desired gravity centre. If the deviation of the gravity centre is large between them, it can be a major cause of vibration and noise due to the oscillating loads in the blades. Therefore the gravity centre in the rotation parts should be controlled properly to improve the static and dynamic balancing of the parts. In this research, the rotor blade of unmanned helicopter has been selected as unbalanced model to obtain the high quality of static balancing in the manufacturing process. It is more convenient to measure the static balancing than dynamic balancing, because the rotor blade has long length compared to its width. In order to achieve the purpose, a measuring system has been proposed. In the measuring system, basic principle is three point weighting method, which is one of the Multiple-point Weighting Method. And circle fitting was used for compensation of measured errors. Before measuring the centre of gravity, 3-dimensional measuring equipment was used for measuring the length and width of rotor blades. Because the resolution level of the electrical voltage obtained from the load cells is low, amplifier was used and the signal is inverted into the electro signal through the data acquisition board and transferred to the personal computer, then voltage is measured by using the measuring programme of gravity centre. From the results, the proposed measuring system gives reliable and precise data of gravity centre for the blade of unmanned helicopter.
机译:转子系统是无人驾驶直升机的芯部,对航空性能,振动和噪声非常重要。在该系统中,由于其复杂的形状,材料和生产体积,转子叶片通常是手动制造的。应精确地控制转子叶片的静态平衡,以确保飞行期间的稳定性。但转子叶片的横截面不对称,非常不平衡。在工业应用中,在直升机,小尺寸精密电机和旋转风扇中,有许多不平衡模型,如转子叶片。在真实产品中,重心通常不符合所需的重力中心。如果重心之间的偏差在它们之间大,则由于叶片中的振荡负载,它可以是振动和噪声的主要原因。因此,应适当地控制旋转部件中的重力中心以改善部件的静态和动态平衡。在该研究中,已经选择了无人直升机的转子叶片作为不平衡模型,以获得制造过程中的高质量静态平衡。测量比动态平衡的静态平衡更方便,因为转子叶片与其宽度相比长。为了达到目的,已经提出了一种测量系统。在测量系统中,基本原理是三点加权方法,是多点加权方法之一。和圆形配件用于补偿测量误差。在测量重心的焦点之前,使用3维测量设备来测量转子叶片的长度和宽度。因为从负载电池获得的电压的分辨率水平为低电平,所以使用放大器,并且信号通过数据采集板反转到电力信号中并传输到个人计算机,然后通过使用测量程序来测量电压重力中心。从结果中,所提出的测量系统为无人直升机叶片提供了可靠和精确的重心数据。

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