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《Vehicle System Dynamics: International Journal of Vehicle Mechanics and Mobility》2012,50(5):721-736
This work introduces a new concept in designing semi-active engine mounts. Engine mounts are under continuous development to provide better and more cost-effective engine vibration control. Passive engine mounts do not provide satisfactory solution. Available semi-active and active mounts provide better solutions but they are more complex and expensive. The variable stiffness engine mount (VSEM) is a semi-active engine mount with a simple ON–OFF control strategy. However, unlike available semi-active engine mounts that work based on damping change, the VSEM works based on the static stiffness change by using a new fast response force controlled variable spring. The VSEM is an improved version of the vibration mount introduced by the authors in their previous work. The results showed significant performance improvements over a passive rubber mount. The VSEM also provides better vibration control than a hydromount at idle speed. Low hysteresis and the ability to be modelled by a linear model in low-frequency are the advantages of the VSEM over the vibration isolator introduced earlier and available hydromounts. These specifications facilitate the use of VSEM in the automotive industry, however, further evaluation and developments are needed for this purpose. 相似文献
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预应力混凝土大跨连续梁桥隔震设计 总被引:2,自引:0,他引:2
大跨预应力混凝土连续梁桥由于质量庞大,地震作用往往成为控制该类结构设计的主要因素.理论分析表明,处于地震高烈度地区桥梁的地震反应对结构参数变动十分敏感.加大构件截面或增加固定墩数量虽可提高结构的抗震能力,但同时也会使结构的地震反应迅速增加.反而使结构抗震能力需求缺口进一步扩大,因此按常规抗震设计思路进行抗震设计往往无法达到抗震设防目标.选用具有隔震和耗能双重功能的摩擦摆支座对桥梁进行减隔震设计,可大幅降低墩底内力,并使主梁相对于墩顶的位移控制在可接受范围内,满足结构的抗震需求.通过对摩擦摆支座滑动曲面半径和摩擦面滑动摩擦系数等参数的优化分析,得出了减隔震装置参数选取的基本原则. 相似文献
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简单介绍了冲击试验机的发展概况,重点讨论了双波冲击机的优越性及其在橡胶减振器等船舶设备冲击试验中应用的可行性。利用现有双波冲击机中正波和负波发生系统的数学模型,数值仿真了冲击机的输出波形特征。分析了双波冲击机的试验条件,计算了冲击机在空载工况下的冲击响应谱。仿真结果表明,双波冲击机的冲击响应谱在允许误差范围内,冲击机输出波形符合标准,可以用于冲击试验。 相似文献
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The objective of the whole-spacecraft vibration isolation (WSVI) system is to reduce the launch-induced dynamic loads and the quality control cost of the satellite and its components, and to increase the launch reliability by insertion of isolators between the satellite and the launch vehicle. A niche hybrid genetic algorithm (NHGA) is proposed to optimize stiffness and damping of the isolators. Through the comparison of the frequency response analysis results, it shows that the optimized WSVI system more effectively reduces spacecraft axial / lateral response due to the broadband structure-born launch environment. At the same time, the case of the whole-spacecraft vibration isolation optimization design demonstrates the efficiency and validity of the genetic algorithm. 相似文献