首页> 外文期刊>SAE International Journal of Materials and Manufacturing >Accelerated Fatigue and Modal Parameter Identification of Lightweight Structures
【24h】

Accelerated Fatigue and Modal Parameter Identification of Lightweight Structures

机译:轻型结构的加速疲劳和模态参数识别

获取原文
获取原文并翻译 | 示例
           

摘要

Car components are exposed to the random/harmonic/impact excitation which can result in component failure due to vibration fatigue. The stress and strain loads do depend on local stress concentration effects and also on the global structural dynamics properties. Standardized fatigue testing is long-lasting, while the dynamic fatigue testing can be much faster; however, the dynamical changes due to fatigue are usually not taken into account and therefore the identified fatigue and structural parameters can be biased. In detail: damage accumulation results in structural changes (stiffness, damping) which are hard to measure in real time; further, structural changes change the dynamics of the loaded system and without taking this changes into account the fatigue load in the stress concentration zone can change significantly (even if the excitation remains the same). This research presents a new approach for accelerated vibration testing of real structures. The new approach bases on phase locked harmonic excitation and can be used for identification of natural frequencies and damping while the damage due to vibration is being accumulated. At the same time a real-time control loop takes into account the structural changes and adequately changes the excitation to preserve the constant amplitude of the stress at the fatigue zone of the tested structure. An example of a real aluminum (A-S8U3) part excited close to the 4th natural frequency is presented. Due to high testing frequency the 1 × 10~6 cycles are reached in approx. 20 minutes. The presented measurements show the change of natural frequency and damping during the test, while the stress amplitude at the fatigue zone is kept constant.
机译:汽车零部件会受到随机/谐波/冲击的激励,这可能会由于振动疲劳而导致零部件失效。应力和应变载荷确实取决于局部应力集中效应,还取决于整体结构动力学特性。标准化的疲劳测试可以长期持续,而动态疲劳测试可以更快。但是,通常不会考虑由于疲劳引起的动态变化,因此可以对确定的疲劳和结构参数进行偏置。详细地说:损伤的积累导致结构变化(刚度,阻尼),这些变化很难实时测量;此外,结构变化会改变加载系统的动力学,并且在不考虑此变化的情况下,应力集中区域中的疲劳载荷会发生显着变化(即使激励保持不变)。这项研究提出了一种用于真实结构的加速振动测试的新方法。新方法基于锁相谐波激励,可用于识别固有频率和阻尼,同时积累由于振动引起的损坏。同时,实时控制回路会考虑结构变化,并充分改变激励,以保持被测结构疲劳区域应力的恒定幅度。给出了一个真实的铝(A-S8U3)零件的示例,该零件被激发接近第4个固有频率。由于测试频率高,大约需要1×10〜6个周期。 20分钟。给出的测量结果显示了测试期间固有频率和阻尼的变化,而疲劳区的应力幅度保持恒定。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号