振动疲劳寿命分析在主镜支撑结构设计中的应用

通过随机振动峰值应力响应考核空间相机在随机振动环境下主镜支撑结构的可靠性存在一定的局限性。本文针对主镜支撑结构在随机振动试验中出现断裂的现象,采用振动疲劳寿命分析对结构的可靠性进行考察,提出了应用数值仿真技术预测结构随机振动疲劳寿命的方法。根据有限元和随机振动疲劳相关理论,采用振动疲劳分析软件对某空间相机支撑环柔节进行了随机振动疲劳分析,计算了疲劳寿命的大小及分布。比较仿真和随机振动试验结果表明,采用振动疲劳寿命评价随机振动环境下结构的可靠性是合理的,利用数值仿真技术预测结构的随机振动疲劳寿命是可行的。     

空间光学遥感器主镜加工过程中疲劳寿命研究

针对空间光学遥感器主镜镜面加工过程中,磨盘与主镜间磨削动作往复运行引起的主镜柔性支撑结构疲劳寿命问题,通过建立主镜组件的有限元模型,利用MSC.Fatigue软件按应力-寿命(S-N)法对主镜组件进行了疲劳寿命分析,确定了支撑结构的薄弱部位,并对仿真过程进行了误差分析,讨论了影响仿真结果的各个因素.对比热真空试验和动力学试验前后主镜镜面面型数据,验证了支撑结构加工、设计参量的合理性.通过疲劳寿命仿真分析,可以有效预示光学结构在加工过程中的疲劳情况,为空间光学遥感器结构的设计、加工提供理论依据和参考.     

空间光学遥感器主镜加工过程中疲劳寿命研究

针对空间光学遥感器主镜镜面加工过程中,磨盘与主镜间磨削动作往复运行引起的主镜柔性支撑结构疲劳寿命问题,通过建立主镜组件的有限元模型,利用MSC.Fatigue软件按应力-寿命(S-N)法对主镜组件进行了疲劳寿命分析,确定了支撑结构的薄弱部位,并对仿真过程进行了误差分析,讨论了影响仿真结果的各个因素.对比热真空试验和动力学试验前后主镜镜面面型数据,验证了支撑结构加工、设计参量的合理性.通过疲劳寿命仿真分析,可以有效预示光学结构在加工过程中的疲劳情况,为空间光学遥感器结构的设计、加工提供理论依据和参考.     

空间相机反射镜组件的随机振动疲劳分析

针对空间相机反射镜组件在随机振动试验中出现的疲劳破坏问题,为了保证结构的安全,应用有限元方法预测结构随机振动疲劳寿命。首先建立了反射镜组件有限元模型,然后进行了模态和频率响应分析,最后利用MSC.Fatigue软件结合材料S-N曲线和载荷谱进行了随机振动疲劳分析。通过分析得到反射镜组件的疲劳寿命最小为80235s,其位置在柔性支撑结构的十字筋处。结果表明,反射镜组件的疲劳寿命远大于试验的所需时间,满足设计要求,可以对材料的选取和结构的优化设计做出快速响应,为结构随机振动疲劳寿命的研究提供参考和依据。     

温度对超薄铜膜疲劳性能影响的分子动力学模拟

用嵌入原子势的分子动力学方法模拟了温度对超薄铜膜疲劳性能的影响. 通过模拟, 首先给出了超薄铜膜的总能及应力随循环周次的变化曲线; 根据叠加经验式得出的叠加量随循环周次变化曲线, 判断出各种恒定温度下超薄铜膜的疲劳寿命. 由 200–400 K温度范围内超薄铜膜的疲劳寿命-温度变化曲线, 可以发现存在两个温度区域: 在约370 K以下, 超薄铜膜的疲劳寿命随温度升高缓慢增加, 而在约370 K以上增加较快. 建立了模型并用位错演化机制解释了超薄铜膜疲劳寿命的温度依赖关系. 关键词： 分子动力学 疲劳 温度效应 位错     

基于能量法的激光熔覆构件疲劳寿命评估研究北大核心CSCD

激光熔覆零件疲劳寿命评估一直是制约激光熔覆技术在工程中推广应用的一个重要因素,现有研究多为试验研究,缺乏理论分析。为量化评估激光熔覆试件的疲劳寿命,并确定熔覆过程的最优速度参数,采用能量法,综合考虑相变及熔覆过程能量变化规律,建立了激光熔覆构件疲劳寿命评估模型,模型计算结果和试验结果基本吻合。评估模型计算结果表明采用同步送粉法,激光功率、光斑直径及送粉速率一定的情况下,V是180mm/min时为最优参数。     

测试薄膜弯曲疲劳寿命的简易实验

基于悬臂梁振动和纯弯曲理论,提出测试薄膜弯曲疲劳寿命的简易实验方法.将待检测的薄膜沉积在一定尺寸的金属片上作为试样,外力驱动试样作悬臂梁一阶弯曲受迫振动,通过光学显微镜观察其表面的薄膜是否开裂或剥落,确定薄膜的疲劳寿命,理论计算获得应力分布.以CoCrMo为基体材料研究了TiO2薄膜的疲劳特性.     

内压、弯扭耦合载荷下连续管疲劳寿命评估

针对连续管在作业中易出现疲劳失效等问题,进行了连续管在内压、弯扭耦合加载下疲劳寿命评估。首先分析了耦合加载下连续管低周疲劳失效机理,基于Brown-Miller疲劳寿命模型建立了连续管疲劳寿命数值计算模型,开展了内压和弯曲加载下连续管疲劳实验,实验结果证实该数值模型是可行的。计算了内压和弯曲耦合加载下连续管低周疲劳寿命,以及内压和弯扭耦合加载下连续管低周疲劳寿命。计算结果表明,连续管最大塑性应变和疲劳敏感区出现在轴向拉伸面和压缩面,与现场连续管失效情况是一致的。通过计算得到了连续管安全服役的临界扭矩值和内压值。     

制导光缆中光纤寿命预期

介绍了光纤寿命预期的疲劳实验方法和筛选实验方法。采用这两种方法，利用电子万能材料试验机和光纤筛选复绕机对室温下光纤进行了疲劳性能实验。实验得出，在张力小于850g的情况下，制导光纤的寿命可以达到10年以上；光纤的韦伯参数md和疲劳参数nd的大小影响光纤寿命。实验表明，当光纤的使用状态受力较大时，或使用贮存状态相差较大时，宜选用动态方法进行寿命预期；当贮存和使用状态受力变化不大时，宜选用筛选复绕方法预期光纤寿命。制导光纤寿命模型宜选用动态疲劳模型，通信光纤可选用筛选实验模型。实验还表明，提高光纤的抗疲劳因子nd和减小光缆中光纤的应变，可以更好地保持光缆中光纤的使用寿命和可靠性。     

实用NbTi/Cu超导股线、绞线拉伸及疲劳性能研究

对NbTi/Cu超导股线、绞线开展了一系列常温力学特性实验研究,包括准静态加卸载、芯丝裂纹扩展及轴向疲劳。实验发现:超导股线加载过程具有明显的阶段性,经过初始加卸载循环"锻炼"后,残余应变不随卸载应力增加而增加;疲劳前期芯丝内部无裂纹,疲劳后期裂纹呈指数型增长直至最终破坏;绞线杨氏模量、疲劳寿命均与扭转节距有关。疲劳过程中,采用循环周期内耗散能定性评估材料内部损伤程度。     

Damage monitor and life prediction of carbon fiber-reinforced ceramic-matrix composites at room and elevated temperatures using hysteresis dissipated energy-based damage parameter

In this paper, the damage monitor and life prediction of carbon fiber-reinforced ceramic-matrix composites (C/SiC CMCs) have been investigated using the hysteresis dissipated energy-based damage parameter. The evolution of the interface shear stress, hysteresis dissipated energy, hysteresis dissipated energy-based damage parameter and the broken fibers fraction vs. cycle number, the fatigue life S?N curves of unidirectional, cross-ply and 2.5D C/SiC composites at room temperature and 800 °C in air atmosphere have been analyzed. For unidirectional C/SiC, the hysteresis dissipated energy and hysteresis dissipated energy-based damage parameter first increase and then decrease with cycle number, and the fatigue limit stress decreases from 88% tensile strength at room temperature to 20% of the tensile strength at 800 °C in air atmosphere; for cross-ply C/SiC, the hysteresis dissipated energy and hysteresis dissipated energy-based damage parameter decrease with increasing applied cycles, and the fatigue limit stress decreases from 85% tensile strength at room temperature to 22% tensile strength at 800 °C in air; and for 2.5D C/SiC, the hysteresis dissipated energy and hysteresis dissipated energy-based damage parameter increases with cycle number, and the fatigue limit stress decreases from 70% tensile strength at room temperature to 25% tensile strength at 800 °C in air.     

An energy-equilibrium model for complex stress effect on fatigue crack initiation

Based on Tanaka and Mura’s fatigue model and Griffith theory for fracture,an energy-equilibrium model was proposed to explain the complex stress effect on fatigue behavior.When the summation of the elastic strain energy release and the stored strain energy of accumulated dislocations reach the surface energy of a crack,the fatigue crack will initiate in materials.According to this model,for multiaxial stress condition,the orientation of the crack initiation and the initiation life can be deduced from the energy equilibrium equation.For the uniaxial fatigue loading with mean stress,the relation between the maximum stress or the minimum stress and the stress amplitude is in agreement with an ellipse equation on the constant life diagram.If the ratio of the mean stress to stress amplitude is less than a critical value-0.17,and the stress amplitude keeps constant,the fatigue crack initiation life will decrease with the increase of the compress mean stress.In this model,the mean stress does not cause damage accumulation with the fatigue cycles in crack initiation.For this reason,the loading sequence of different load levels would induce the cumulative damage to deviate from the Palmgren-Miner cumulative damage rule.The procedure of estimating the damage under random loading is also discussed.     

柔性有机场效应晶体管研究进展

柔性有机场效应晶体管具有可折叠、质量轻、低成本等优点,在柔性显示、柔性传感器、柔性射频标签和柔性集成电路等方面显示了广阔的应用前景.本文在介绍柔性有机场效应 晶体管最新研究进展的基础上, 总结了柔性有机场效应晶体管的器件结构和柔性有机场效应晶体管所使用的衬底材料、 栅绝缘层材料、有源层材料及电极材料, 阐述了柔性有机场效应晶体管的制备工艺, 并讨论了不同的弯曲方式对柔性有机场效应晶体管性能的影响, 最后总结和展望了柔性有机场效应晶体管的应用领域. 关键词： 柔性 晶体管 有机/聚合物 溶液加工     

大数值孔径多组分玻璃柔性光纤的制备及影响因素分析

大数值孔径多组分玻璃柔性光纤在医用光纤内窥镜中具有广阔的应用前景.采用La2O3 -Nb2O5 -SiO2-B2O3-RO玻璃系统作纤芯,用自制相匹配的低折射率玻璃材料作包层拉制的柔性光纤的数值孔径为0.8725,光的接受角为122°,扩大了医用光纤内窥镜的观察范围,满足了医疗仪器观察诊断的特殊需要.给出了La2O3 ...     

High‐mobility flexible thin‐film transistors with a low‐temperature zirconium‐doped indium oxide channel layer

Thin film transistors (TFTs) with zirconium‐doped indium oxide (ZrInO) channel layer were successfully fabricated on a flexible PEN substrate with process temperature of only 150 °C. The flexible ZrInO TFT exhibited excellent electrical performance with a saturation mobility of as high as 22.6 cm² V^–1 s^–1, a sub‐threshold swing of 0.39 V/decade and an on/off current ratio of 2.5 × 10⁷. The threshold voltage shifts were 1.89 V and ?1.56 V for the unpassivated flexible ZrInO TFT under positive and negative gate bias stress, respectively. In addition, the flexible ZrInO TFT was able to maintain the relatively stable performance at bending curvatures larger than 20 mm, but the off current increased apparently after bent at 10 mm. Detailed studies showed that Zr had an effect of suppress the free carrier generation without seriously distorting the In₂O₃ lattice. (© 2016 WILEY‐VCH Verlag GmbH &Co. KGaA, Weinheim)     

Effects of loading condition on very-high-cycle fatigue behaviour and dominant variable analysis

The specimens of a high carbon chromium steel were quenched and tempered at 150°C,180°C and 300°C.Such specimens were tested via rotating bending and a push-pull type of axial loading to investigate the influences of loading condition on the behaviour of very-high-cycle fatigue(VHCF).Experimental results show the different influences of inclusion size on the fatigue life for the two loading conditions.Predominant factors and mechanism for the fine-granular-area(FGA)of crack origin were discussed.In addition,a reliability analysis based on a modified Tanaka-Mura model was carried out to evaluate the sensitivity of inclusion size,stress,and KFGA to the life of VHCF crack initiation.     

柔性基周期性厚度梯度薄膜的应变效应

可控的表面微结构在柔性电子、仿生器件和能源材料等方面均具有重要的应用价值.本文采用编织铜网作为掩模板,利用磁控溅射技术在柔性聚二甲基硅氧烷(PDMS)基底上制备具有周期分布的厚度梯度金属银薄膜,研究了薄膜在单轴压缩/拉伸过程中的形貌演化规律.实验发现,在单轴机械载荷作用下,银薄膜表面将形成相互垂直的条纹褶皱和多重裂纹.膜厚的梯度变化调制了薄膜的面内应力分布,导致褶皱在膜厚较小处率先形成,并逐渐扩展到膜厚较大区域,而裂纹则基本限定在膜厚较小区域.基于应力理论和有限元计算,对周期性厚度梯度薄膜的褶皱和裂纹的形貌特征、演化行为和物理机制进行了深入分析.该研究将有助于加深对非均匀薄膜体系的应变效应的理解,并有望通过梯度薄膜的结构设计在柔性电子等领域获得应用.     

界面合金化控制柔性Al/PI薄膜应力的研究

针对航天器用MEMS热控百叶窗存在的柔性薄膜应力问题, 开展界面合金化控制薄膜应力技术研究. 通过给柔性Al/PI薄膜体系添加中间层Sn, 使其合金化, 使晶格产生膨胀畸变, 来引入相反的应力与已经存在的本征压应力相抗衡, 可获得低表观应力的薄膜. 用SEM和EDS剖面分析验证了Sn原子发生了明显的扩散现象, 形成了Al-Sn合金层. 这种方法可作为控制薄膜应力的一种新的技术手段.     

Quasi-variational principles of single flexible body dynamics and their applications

The reasons for studying single flexible body dynamics are that on one hand, it is the basis of flexible multi-body dynamics. If the theory of the single flexible body dynamics has been deeply studied, the theory of flexible multi-body dynamics will be researched easily. On the other hand, it has its unique and important applications. Quasi-variational principle of non-conservative single flexible body dynamics is established under the cross-link of particle rigid body mechanics and deformable body mechanics. Taking the interceptor as an example, this paper has explained the physical meaning of the quasi-stationary value condition of the quasi-variational principle in non-conservative single flexible body dynamics. Taking the launch of rocket as an example, it has illustrated the features of “one force for two effects” in a single flexible body dynamics. With an example of the extending flexible beam coupled with the spacecraft attitude, it has shown the transition from the single flexible body dynamics to the flexible multi-body dynamics. Finally, a number of related problems are discussed. Supported by the National Natural Science Foundation of China (Grant No. 10272034), the Doctoral Education Foundation (Grant No. 20060217020), and the Natural Science Foundation of Harbin Engineering University (Grant No. HEUF04003)