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Semi-active control of a sandwich beam partially filled with magnetorheological elastomer

机译:部分填充磁流变弹性体的夹层梁的半主动控制

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The paper deals with the semi-active control of vibrations of structural elements. Elastomer composites with ferromagnetic particles that act as magnetorheological fluids are used. The damping coefficient and the shear modulus of the elastomer increases when it is exposed to an electro-magnetic field. The control of this process in time allows us to reduce vibrations more effectively than if the elastomer is permanently exposed to a magnetic field. First the analytical solution for the vibrations of a sandwich beam filled with an elastomer is given. Then the control problem is defined and applied to the analytical formula. The numerical solution of the minimization problem results in a periodic perfectly rectangular control function if free vibrations are considered. Such a temporarily acting magnetic field is more efficient than a constantly acting one. The surplus reaches 20-50% or more, depending on the filling ratio of the elastomer. The resulting control was verified experimentally in the vibrations of a cantilever sandwich beam. The proposed semi-active control can be directly applied to engineering vibrating structural elements, for example helicopter rotors, aircraft wings, pads under machines, and vehicles.
机译:本文涉及结构元件振动的半主动控制。使用具有充当磁流变流体的铁磁颗粒的弹性体复合材料。当弹性体暴露于电磁场时,其阻尼系数和剪切模量会增加。与弹性体永久暴露在磁场中相比,及时控制此过程可使我们更有效地减少振动。首先,给出了填充弹性体的夹层梁振动的解析解。然后定义控制问题并将其应用于解析公式。如果考虑自由振动,则最小化问题的数值解会导致周期的完美矩形控制函数。这种暂时作用的磁场比持续作用的磁场更有效。剩余量达到20-50%或更多,具体取决于弹性体的填充率。通过悬臂夹层梁的振动实验验证了所得的控制。所提出的半主动控制可直接应用于工程振动结构元件,例如直升机旋翼,飞机机翼,机器下方的垫块和车辆。

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