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Fatigue failure investigation on anti-vibration springs

机译:抗振弹簧疲劳失效研究

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Fatigue failure investigation on anti-vibration springs, involving both metal and rubber materials, is presented. Rubber-to-metal bonded springs are widely used in industry as anti-vibration components giving many years of service. Recently a need to improve time and cost efficiencies has caused an unexpected early fatigue failure of the component with no immediate explanation. The required total fatigue life was 1.25 million cycles but only 0.7 million cycles achieved. There was an urgent need to investigate the causes of the fatigue failure and to modify the component design accordingly to meet the customer requirement and the supply schedule. The investigation, based on the actual fatigue loads, is carried out on these failed and modified products using a method of continuum mechanics. To simplify the simulation, a non-linear quasi-static analysis is carried out and then the residual stresses are superimposed to obtain the effective stress range to predict the metal crack initiation. For the rubber parts a three-dimensional effective stress criterion is employed to predict the fatigue crack initiation. The fatigue failure is taken as visual crack observation (normally 1-2 mm). The fatigue crack initiation for the metal parts of the failed component is predicted at 225 K cycles under specified fatigue load against total metal broken at 700 K cycles from the test. For the modified part the minimum total fatigue life for the metal parts of the component, estimated conservatively, is 2.1 million cycles against 1.75 million cycles from the test without any crack observed. The rubber fatigue crack initiation is predicted at 90 K cycles against crack onset around 79 K cycles and crack length 40 mm at 145 K cycles from the test. From design point of view it is important to optimize the rubber profile under this very tight allowable space to provide the maximum support of the metal interleaves and at the same time to meet the minimum requirements of the manufacture process. It is shown that this approach can be employed at a design stage for both metal and rubber fatigue evaluations on anti-vibration springs.
机译:介绍了涉及金属和橡胶材料的抗振弹簧的疲劳失效研究。橡胶与金属的粘结弹簧作为防振组件已在工业中得到广泛使用,具有多年的使用寿命。最近,对改善时间和成本效率的需求已经导致组件的意外的早期疲劳失效,没有立即说明。所需的总疲劳寿命为125万次循环,但仅实现了70万次循环。迫切需要调查疲劳失效的原因,并相应地修改组件设计,以满足客户的需求和供货计划。基于实际疲劳载荷的调查,是使用连续力学方法对这些失效和修改后的产品进行的。为了简化模拟,先进行非线性准静态分析,然后叠加残余应力以获得有效应力范围,以预测金属裂纹的萌生。对于橡胶零件,采用三维有效应力准则来预测疲劳裂纹的萌生。疲劳破坏作为目视裂纹观察(通常为1-2mm)。在指定的疲劳载荷下,预计在225 K循环下失效部件的金属零件的疲劳裂纹萌生,相对于测试中在700 K循环下断裂的总金属而言。保守地估计,对于改性零件,部件金属零件的最小总疲劳寿命为210万次循环,而从测试开始的175万次循环中未观察到任何裂纹。相对于测试,橡胶疲劳裂纹萌生是在90 K周期时预测的,而裂纹在79 K周期左右发生,而裂纹长度在145 K周期为40 mm。从设计的角度来看,重要的是在这个非常狭窄的允许空间内优化橡胶轮廓,以最大程度地支撑金属夹层,同时满足制造工艺的最低要求。结果表明,该方法可以在设计阶段用于抗振弹簧的金属和橡胶疲劳评估。

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