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Relieving the effect of static load errors in nonlinear vibration isolation mounts through stiffness asymmetries

机译:通过刚度不对称减轻非线性隔振支座中静载荷误差的影响

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摘要

High Static Low Dynamic Stiffness (HSLDS) mounts consist of nonlinear springs that support a high static load with low static displacement, whilst maintaining locally low stiffness near equilibrium, to give a low natural frequency and consequently good isolation properties. Recent analysis has investigated such devices when the force-displacement relationship is an odd function about the equilibrium position, and analysed the consequences of different shapes of these functions. However many devices that have the HSLDS characteristic do not meet the assumptions of this analysis, in that the force-displacement relationship is generally asymmetric about equilibrium. Furthermore, even devices that do meet this assumption may be subject to significant adjustment error, particularly in the context of air vehicles where manoeuvres such as banked turns can cause an apparent variation in gravitational acceleration, and a consequent variation in the weight of the payload. This change in static load moves the payload away from its intended region of low stiffness. The current paper provides analysis of these situations, and shows that the performance of a mount with a symmetric stiffness-displacement relationship is highly sensitive to errors in the static loading. It is then shown that a mount with an asymmetric stiffness-displacement function can offer significant performance advantages when there are adjustment errors in the loading of the mount. (C) 2014 Elsevier Ltd. All rights reserved.
机译:高静态低动态刚度(HSLDS)支座由非线性弹簧组成,该弹簧可支撑高静态载荷且静态位移低,同时在平衡时保持局部较低的刚度,从而具有较低的固有频率,因此具有良好的隔离性能。最近的分析已经研究了当力-位移关系是关于平衡位置的奇数函数时的此类装置,并分析了这些函数的不同形状的后果。但是,许多具有HSLDS特性的设备不能满足此分析的假设,因为力-位移关系通常关于平衡是不对称的。此外,即使确实满足该假设的设备也可能遭受明显的调整误差,特别是在飞行器中,例如倾斜转弯等操纵会引起重力加速度的明显变化,以及随之而来的有效载荷重量变化。静载荷的这种变化使有效载荷远离其低刚度的预期区域。当前论文提供了对这些情况的分析,并表明具有对称刚度-位移关系的底座的性能对静态载荷的误差高度敏感。然后表明,当在支架的加载中存在调节误差时,具有不对称刚度-位移功能的支架可以提供明显的性能优势。 (C)2014 Elsevier Ltd.保留所有权利。

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