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给出了一种利用有限元仿真软件求解航空分扭级和并车级齿轮在啮合过程中的最大接触应力和最大弯曲应力的变化情况的方法.通过不同应力计算标准计算出航空齿轮的最大接触应力与齿根处的最大弯曲应力,并与仿真结果进行比较.结果表明并车级齿轮在啮合过程中靠近轮齿端面和齿顶的地方均存在一定的边缘接触.由于边缘接触易引起应力集中,从而大大影... 相似文献
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Very high cycle fatigue (VHCF) tests were carried out to find the fatigue characteristics of a super-long life range by using
a cantilever type rotational bending fatigue test machine on three kinds of specimens in bearing steel which were quenched
and tempered in air (A: non-shot peened and B: shot peened after heat treatment) and under vacuum environment(C: non-shot
peened) in this study. S-N curves obtained from the VHCF tests of the B and C specimens tend to come down again in the super-long
life (109 cycles) range due to fish-eye type cracking, while most of the A and B specimens were fractured by surface defects such as
scratches and slip lines. This duplex S-N behavior of bearing steel has to be reviewed by the change of the fracture modes.
This paper was recommended for publication in revised form by Associate Editor Youngseog Lee
Chang-Min Suh received his B.S. and M.S. degrees in mechanical engineering from Busan Na-tional University in 1964 and 1968, respectively,
and received his Ph.D. degree from the University of Tokyo in 1981. He now is a professor at Kyungpook National University.
He has served as the Head of the Department of Mechanical Engineering at Kyungpook National University, a Visiting Professor
of Materials Science and Engineering in Univ. of California Berkeley, a Head of the Institute of Engineering Design Technology
Kyungpook Nat’l Univ, and a Head of the Technology Innovation Center designated by the Department of Commerce and Industry
of Korea. 相似文献
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《Wear》1996,193(2):242-247
En 24 steel spur gears in untreated and thermal-treated conditions with and without shot peening were tested in a back-to-back gear test rig. Surface finish at the pitch region and wear loss were monitored. Surface integrity studies and ferrographic analysis of wear debris enabled the interpretation of failure. The surface deterioration was less pronounced in the case of shot-peened gears and further they exhibited good steady-state wear characteristics compared to unpeened gears. 相似文献
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为了提高汽车后桥半轴疲劳寿命检验的效率以及检测的安全性,基于虚拟现实技术提出了一种台架试验与仿真相结合的复合分析检验方法.在一定量台架试验基础上,利用Pro/E参数化设计方法,对汽车后桥半轴进行三维实体建模,ANSYS WorKbench有限元疲劳分析模块对后桥半轴进行疲劳寿命预测分析,获得的结果与一定量台架检验的结果对比分析,得出预测结果与试验结果一致,验证了方法的正确性.这种复合的检验方法相对于单-的台架检验方法,减少了产品的试验样品数量,缩短了开发周期,提高了安全性,降低了开发成本,同时也为农用、工程车辆传动系冲击性能的研究提供了参考. 相似文献
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基于有限元法的汽车构件疲劳寿命分析 总被引:1,自引:0,他引:1
对汽车构件结构疲劳分析和寿命预测方法即静态疲劳分析方法和总寿命S-N预测方法进行了介绍。针对某种型号轿车的悬架,应用多体动力学软件ADAMS构建了悬架的虚拟样机,进行了动力学仿真分析。并应用MSC系列有限元分析和疲劳软件对下控制臂进行分析,计算了其应力特性和疲劳寿命。 相似文献
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通过对试验结果的分析,证明了一种特殊性能的添加剂加入润滑脂后,该润滑脂对于提高轴承的寿命、改善轴承的性能起到一定的促进作用。 相似文献
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通过研究轴承钢GCr15SiMn试片与渗碳钢G20Cr2Ni4A试片的接触疲劳寿命水平得知,渗碳钢G20Cr2Ni4A试片的各项寿命指标均高于轴承钢GCr15SiMn试片,且渗碳钢G20Cr2Ni4A试片的接触疲劳寿命是轴承钢GCr15SiMn试片接触疲劳寿命的3.75倍。 相似文献
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采用计算机辅助工程(CAE)技术来估计奔驰桥轮边减速器齿轮的疲劳寿命。首先运用UG对其行星轮、太阳轮、行星架进行建模并装配;其次在ADAMS中将Hertz接触理论嵌入仿真模型,在齿轮之间施加接触力,实现齿轮啮合的动态实时仿真,并得到其载荷谱;接着将实体简化模型导入MSC.Patran/nastran中进行有限元分析,获得模型的应力应变分布;最后,将载荷谱和应力应变分布导入MSC.Fatigue进行疲劳寿命计算。通过疲劳分析得到轮边减速器齿轮疲劳寿命的分布情况和最危险点的寿命值,该方法和结论对设计汽车的轮边减速器具有指导作用。 相似文献
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对16MnR焊接接头进行了控制应变幅条件下的疲劳试验,获得其疲劳特性参数以及恒应变幅载荷下的疲劳一寿命关系,建立了焊接接头低周疲劳寿命曲线方程。并将试验结果同局部应力应变法计算的结果进行了比较,为该焊接接头应变疲劳提供了理论依据。 相似文献
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