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在汽车的设计计算和定型试验中,汽车的质心高度是一个重要的参数。本文介绍了质量反应法对汽车质心高度测试的应用情况,从测试的技术准备,测试方法,数据处理,计算举例等方面,论述了汽车质心高度的测试与应用。 相似文献
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电控空气悬架能够根据客车行驶工况进行车身高度自适应调节,从而能够显著提升客车行驶稳定性以及燃油经济性,车高调节控制设计具有重要意义。文章利用模糊PID控制算法对车身高度调节进行控制策略设计,有效缓解了客车电控空气悬架车高调节过程中存在的空气弹簧的“过充”“过放”及“振荡”等问题,分析客车电控空气悬架车高调节具体过程,建立包括车身、储气罐、电磁阀以及空气弹簧等在内的车高调节系统数学模型,最后完成了客车电控空气悬架车高调节模糊自适应PID控制策略设计及性能仿真验证。研究结果表明,所运用的模糊自适应PID控制策略能够完成客车电控空气悬架车身高度的准确调节。 相似文献
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龙华松花江特大桥主桥为65 5×100 65m的预应力混凝土半刚构-连续箱梁桥,施工采用悬臂浇筑法。本文介绍了主桥箱梁的构造特点、施工流程及高程控制中立模标高的确定和施工监控中测点的布置情况。 相似文献
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韩朝霞 《铁道标准设计通讯》2016,(4):17-20
受盾构结构空间狭小限制及施工误差影响,盾构中浮置板轨道结构高度不足问题在施工过程中普遍出现。为了研究此问题对浮置板受力和隔振效果的影响,本文针对目前此问题的常用处理措施,利用有限元软件建模分析这些措施对浮置板受力和隔振效果的影响。最终得出降低道床板厚度、减小隔振器纵向间距会增大浮置板1阶固有频率、降低浮置板的低频隔振效率,尤其道床板厚度的降低对浮置板隔振效果影响较大;隔振器纵横向间距减小会减小道床板内的拉、压应力,隔振器刚度增大会增大道床板内的应力。除此之外,目前的常用处理措施也会影响道床基底排水、浮置板施工及后期养护维修。 相似文献
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汽车座椅高度调节器核心构件优化设计 总被引:1,自引:0,他引:1
汽车座椅安全性设计的主要目标就是尽可能避免座椅结构损坏和功能失效情况的发生.高调器作为汽车座椅的部件之一,其功能的好坏直接影响安全性.文章主要根据某款轿车驾驶员座椅在高度调节过程中失效的原因进行分析,设计一种解决高调失效的有效结构设计方案,该方案重新设计了高调器核心件内部销柱的结构.对重新设计的高调器进行疲劳耐久试验,试验结果表明,改进后的高调器可有效解决高调失效的问题,提高了汽车座椅的安全性. 相似文献
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汽车质心高度测量过程中,引起测量误差的因素较多,为了弄清误差来源,提高测量数据的可信度,在特定假设条件成立的前提下,文章运用质量反应法对质心高度计算公式进行了推导,得到了通用公式。当前后轮静力半径相等时,该公式可以简化为国标给定公式。通过实车测量,并对质心高度按2种公式分别计算,比较2次计算结果的偏差,结果显示,在测量前置、前驱等前后轮静力半径不同的车辆时,更适合采用通用公式计算质心高度。 相似文献
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Impacts on asphalt mixture's high temperature performance with PR series additives added by means of rutting test and Repeated Shear Test (Constant Height) (RSCH) were investigated The analytic results of the two tests show that (1) rutting test is not suitable for the high temperature performance evaluation of asphalt mixture with PR series additives added for the reason of the conflict between dynamic stability and rut depth; (2) the results of RSCH,such as K1,K2,N and γ,show very well consistency which is suitable
for the high temperature performance evaluation of asphalt mixture with PR series additives
added The results of RSCH show that asphalt mixture with PR PLAST S (PRS)
added has the best performance,the PR FLEX MODULE (PRM) one is the next and t
he original one is the worst for the high temperature anti?shear performance 相似文献
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An optimization technique was used to generate a wing-in-ground-effect (WIG) configuration which can achieve the maximum lift
and satisfy the height stability criteria within the design constraints. For the analysis of the aerodynamic coefficients,
the vortex lattice method (VLM) was applied with the inviscid and potential flow approximations. The sequential quadratic
programming (SQP) method, which is a nonlinear optimization method, was employed as an optimization tool. The lift and moment
coefficients, including the stability analysis computed by VLM, were compared with the experimental results of a medium-sized
WIG, and a good correlation was found between them. In addition, the optimization tool was validated by finding the optimal
position of the side wing attached on the WIG craft. Then, various optimum examples are shown, with generation of the wing
section, the determination of the planform configuration, the aspect ratio, and the position of the tail wing within the design
constraints. It was shown that the present optimization tool can be used effectively for the optimal design of a WIG craft. 相似文献