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Jing HU, Pengfei LIU, Bernhard STEINAUER
《结构与土木工程前沿(英文)》 2017年 第11卷 第3期 页码 329-337 doi: 10.1007/s11709-017-0407-9
关键词: asphalt mixture microstructure morphology digital image processing fatigue damage
Estimation of fatigue damage of airplane landing gear
LIU Ke-ge, YAN Chu-liang, ZHANG Shu-ming
《机械工程前沿(英文)》 2006年 第1卷 第4期 页码 424-428 doi: 10.1007/s11465-006-0051-x
杨晓华,姚卫星,段成美
《中国工程科学》 2003年 第5卷 第4期 页码 81-87
著名的Miner-Palmgren线性累积损伤理论的提出已有70余年,但由于疲劳问题的复杂性,迄今为止还没有一个模型的工程应用价值能与该理论媲美。疲劳累积损伤理论仍在发展与完善中。文章根据疲劳损伤与疲劳累积损伤理论的特点,将确定性疲劳累积损伤理论分成两大类,即线性累积损伤理论和非线性累积损伤理论,并将主要的非线性累积损伤理论分成五类:a. 基于损伤曲线法的非线性累积损伤理论;b. 基于材料物理性能退化概念的非线性累积损伤理论;c. 基于连续损伤力学概念的非线性累积损伤理论;d. 考虑载荷间相互作用效应的非线性累积损伤理论;e. 基于能量法的非线性累积损伤理论。文章分析了每一类模型中有代表性模型的物理背景,回答了模型在疲劳累积损伤理论中存在的主要问题,简要评述了模型的优缺点,讨论了确定性疲劳累积损伤理论的几个关键问题。
Contact fatigue life prediction of a bevel gear under spectrum loading
Pan JIA, Huaiju LIU, Caichao ZHU, Wei WU, Guocheng LU
《机械工程前沿(英文)》 2020年 第15卷 第1期 页码 123-132 doi: 10.1007/s11465-019-0556-8
关键词: bevel gear rolling contact fatigue (RCF) multiaxial fatigue criterion load spectrum damage accumulation rule
李靖宇,田常录
《中国工程科学》 2006年 第8卷 第2期 页码 51-54
船舶事故分析表明,疲劳破坏是其结构破坏的主要形式。由于船体中节点的多样性以及节点荷载的复杂性,使得船体结构的疲劳校核计算也相当复杂,所以工程中提出了一些简化方法。介绍了船体结构疲劳强度校核的基本原理,疲劳载荷和疲劳累积损伤计算方法;编写了船体结构疲劳强度校核程序,并用其评估了大型油轮(VLCC)在典型节点处的疲劳寿命。
Cracking evolution behaviors of lightweight materials based on
Y. Luo, S. C. Wu, Y. N. Hu, Y. N. Fu
《机械工程前沿(英文)》 2018年 第13卷 第4期 页码 461-481 doi: 10.1007/s11465-018-0481-2
Damage accumulation and failure behaviors are crucial concerns during the design and service of a critical component, leading researchers and engineers to thoroughly identifying the crack evolution. Third-generation synchrotron radiation X-ray computed microtomography can be used to detect the inner damage evolution of a large-density material or component. This paper provides a brief review of studying the crack initiation and propagation inside lightweight materials with advanced synchrotron three-dimensional (3D) X-ray imaging, such as aluminum materials. Various damage modes under both static and dynamic loading are elucidated for pure aluminum, aluminum alloy matrix, aluminum alloy metal matrix composite, and aluminum alloy welded joint. For aluminum alloy matrix, metallurgical defects (porosity, void, inclusion, precipitate, etc.) or artificial defects (notch, scratch, pit, etc.) strongly affect the crack initiation and propagation. For aluminum alloy metal matrix composites, the fracture occurs either from the particle debonding or voids at the particle/matrix interface, and the void evolution is closely related with fatigued cycles. For the hybrid laser welded aluminum alloy, fatigue cracks usually initiate from gas pores located at the surface or sub-surface and gradually propagate to a quarter ellipse or a typical semi-ellipse profile.
关键词: fatigue crack initiation and growth fatigue damage mechanism damage tolerance defect characterization laser welded aluminum alloys
Jia XU,Zhen-yu ZHOU,Zhong-yu PIAO
《机械工程前沿(英文)》 2016年 第11卷 第3期 页码 227-232 doi: 10.1007/s11465-016-0395-9
The accumulated damage process of rolling contact fatigue (RCF) of plasma-sprayed coatings was investigated. The influences of surface roughness, loading condition, and stress cycle frequency on the accumulated damage status of the coatings were discussed. A ball-on-disc machine was employed to conduct RCF experiments. Acoustic emission (AE) technique was introduced to monitor the RCF process of the coatings. AE signal characteristics were investigated to reveal the accumulated damage process. Result showed that the polished coating would resist the asperity contact and remit accumulated damage. The RCF lifetime would then extend. Heavy load would aggravate the accumulated damage status and induce surface fracture. Wear became the main failure mode that reduced the RCF lifetime. Frequent stress cycle would aggravate the accumulated damage status and induce interface fracture. Fatigue then became the main failure mode that also reduced the RCF lifetime.
关键词: accumulated damage spray coating rolling contact fatigue acoustic emission
Review of the damage mechanism in wind turbine gearbox bearings under rolling contact fatigue
Yun-Shuai SU, Shu-Rong YU, Shu-Xin LI, Yan-Ni HE
《机械工程前沿(英文)》 2019年 第14卷 第4期 页码 434-441 doi: 10.1007/s11465-018-0474-1
关键词: rolling contact fatigue (RCF) white etching area (WEA) white etching crack (WEC) adiabatic shear band (ASB)
A dimensional analysis on asphalt binder fracture and fatigue cracking
Qian ZHAO, Zhoujing YE
《结构与土木工程前沿(英文)》 2018年 第12卷 第2期 页码 201-206 doi: 10.1007/s11709-017-0402-1
Hierarchical approach for fatigue cracking performance evaluation in asphalt pavements
Ibrahim ONIFADE, Yared DINEGDAE, Björn BIRGISSON
《结构与土木工程前沿(英文)》 2017年 第11卷 第3期 页码 257-269 doi: 10.1007/s11709-017-0410-1
关键词: fatigue cracking energy based crack initiation mechanistic approach pavement analysis
Assessment of fatigue life of remanufactured impeller based on FEA
Lei XU,Huajun CAO,Hailong LIU,Yubo ZHANG
《机械工程前沿(英文)》 2016年 第11卷 第3期 页码 219-226 doi: 10.1007/s11465-016-0394-x
Predicting the fatigue life of remanufactured centrifugal compressor impellers is a critical problem. In this paper, the S-N curve data were obtained by combining experimentation and theory deduction. The load spectrum was compiled by the rain-flow counting method based on the comprehensive consideration of the centrifugal force, residual stress, and aerodynamic loads in the repair region. A fatigue life simulation model was built, and fatigue life was analyzed based on the fatigue cumulative damage rule. Although incapable of providing a high-precision prediction, the simulation results were useful for the analysis of fatigue life impact factors and fatigue fracture areas. Results showed that the load amplitude greatly affected fatigue life, the impeller was protected from running at over-speed, and the predicted fatigue life was satisfied within the next service cycle safely at the rated speed.
关键词: remanufactured impeller fatigue life impeller failures finite element analysis (FEA)
詹俞,李国芬,王宏畅
《中国工程科学》 2013年 第15卷 第8期 页码 75-78
结合南京长江第四大桥钢桥面铺装实体工程,开展铺装层混合料20 ℃疲劳性能试验。为了使试验结果能够更真实地反映主桥铺装的实际情况,直接采用主桥铺装使用的混合料成型试件,其中,带钢板复合梁试件为施工现场摊铺、碾压成型。室内试验对铺装结构单层采用劈裂疲劳试验,选择0.2、0.3、0.4、0.5、0.6这5个等级的应力水平,对组合结构采用带钢板复合梁疲劳试验,荷载水平为6 kN、7 kN、8 kN,并通过回归分析得到疲劳方程。
Enhancing fatigue life of cylinder-crown integrated structure by optimizing dimension
Weiwei ZHANG,Xiaosong WANG,Zhongren WANG,Shijian YUAN
《机械工程前沿(英文)》 2015年 第10卷 第1期 页码 102-110 doi: 10.1007/s11465-015-0329-y
Cylinder-crown integrated hydraulic press (CCIHP) is a new press structure. The hemispherical hydraulic cylinder also functions as a main portion of crown, which has lower weight and higher section modulus compared with the conventional hydraulic cylinder and press crown. As a result, the material strength capacity is better utilized. During the engineering design of cylinder-crown integrated structure, in order to increase the fatigue life, structural optimization on the basis of the adaptive macro genetic algorithms (AMGA) is first conducted to both reduce weight and decrease peak stress. It is shown that the magnitude of the maximum principal stress is decreased by 28.6%, and simultaneously the total weight is reduced by 4.4%. Subsequently, strain-controlled fatigue test is carried out, and the stress-strain hysteresis loops and cyclic hardening curve are obtained. Based on linear fit, the fatigue properties are calculated and used for the fatigue life prediction. It is shown that the predicted fatigue life is significantly increased from 157000 to 1070000 cycles after structural optimization. Finally, according to the optimization design, a 6300 kN CCIHP has been manufactured, and priority application has been also suggested.
关键词: cylinder-crown integrated hydraulic press (CCIHP) adaptive macro genetic algorithms (AMGA) strain-controlled fatigue test
穆志韬
《中国工程科学》 2002年 第4卷 第3期 页码 68-72
依据海军现役飞机的腐蚀环境特点及结构件腐蚀损伤深度拟合规律,采用应力场强法和局部应力应变法分别对疲劳缺口系数Kf及疲劳寿命计算模型进行了分析,提出了一种腐蚀环境下飞机结构疲劳寿命的评定方法。该方法以室温大气环境下的寿命评定结论为依据,考虑了结构件腐蚀损伤后潮湿空气、盐雾、盐雾+SO2等环境介质对疲劳寿命的影响,并结合国产某型飞机机翼前梁缘条腐蚀损伤部位的疲劳寿命及剩余寿命估算实例进行了分析。
标题 作者 时间 类型 操作
A study on fatigue damage of asphalt mixture under different compaction using 3D-microstructural characteristics
Jing HU, Pengfei LIU, Bernhard STEINAUER
期刊论文
Contact fatigue life prediction of a bevel gear under spectrum loading
Pan JIA, Huaiju LIU, Caichao ZHU, Wei WU, Guocheng LU
期刊论文
Cracking evolution behaviors of lightweight materials based on
Y. Luo, S. C. Wu, Y. N. Hu, Y. N. Fu
期刊论文
Accumulated damage process of thermal sprayed coating under rolling contact by acoustic emission technique
Jia XU,Zhen-yu ZHOU,Zhong-yu PIAO
期刊论文
Review of the damage mechanism in wind turbine gearbox bearings under rolling contact fatigue
Yun-Shuai SU, Shu-Rong YU, Shu-Xin LI, Yan-Ni HE
期刊论文
Hierarchical approach for fatigue cracking performance evaluation in asphalt pavements
Ibrahim ONIFADE, Yared DINEGDAE, Björn BIRGISSON
期刊论文
Assessment of fatigue life of remanufactured impeller based on FEA
Lei XU,Huajun CAO,Hailong LIU,Yubo ZHANG
期刊论文
Enhancing fatigue life of cylinder-crown integrated structure by optimizing dimension
Weiwei ZHANG,Xiaosong WANG,Zhongren WANG,Shijian YUAN
期刊论文