Ying Yan
,
Wan-Peng Deng
,
Zhan-Feng Gao
,
Jing Zhu
,
Zhong-Jun Wang
,
Xiao-Wu Li
金属学报(英文版)
doi:10.1007/s40195-016-0373-6
To explore the coupled effect of temperature T and strain rate ε˙ε˙ on the deformation features of AZ31 Mg alloy, mechanical behaviors and microstructural evolutions as well as surface deformation and damage features were systematically examined under uniaxial tension at T spanning from 298 to 523 K and ε˙ε˙ from 10-4 to 10-2 s-1. The increase in T or the decrease in ε˙ε˙ leads to the marked decrease in flow stress, the appearance of a stress quasi-plateau after an initially rapid strain hardening, and even to the occurrence of successive strain softening. Correspondingly, the plastic deformation modes of AZ31 Mg alloy transform from the predominant twinning and a limited amount of dislocation slip into the enhanced non-basal slip and the dynamic recrystallization (DRX) together with the weakened twinning. Meanwhile, the cracking modes also change from along grain boundaries (GBs) and at twin boundaries (TBs) or the end of twins into nearby GBs where the DRX has occurred. The appearance of a stress quasi-plateau, the formation of large-sized cracks nearby GBs, and the occurrence of continuous strain softening, are intimately related to the enhancement of the non-basal slip and the DRX.
关键词:
AZ31
,
Mg
,
alloy
,
Uniaxial
,
tension
,
Temperature
,
Strain
,
rate
,
Deformation
,
Damage
,
Twinning
E.Bayraktar
,
F.Montembault
,
C.Bathias
材料科学技术（英文）
The study of microstructural network and damage mechanism of polymer and rubber, although deceptively simple, involves a complex interplay between material properties and service conditions. So, the study of the texture, deformation and the failure of rubber specimens are of considerable practical interest. In fact, the occurrence of defects such as the initiation and the growth of cavitations in rubber specimens in working conditions is an important problem. These deal with the improvement of microstructure (for delaying instability) in order to obtain a higher service capacity. The scope of the present paper is, therefore, to evaluate principal mechanisms, in-situ observation of damage at mesoscopic, microscopic and macroscopic levels by using X-ray computed tomography (CT) installed in the ITMA research centre for confirming the behaviour of natural rubber (NR) and styrene butyl rubber (SBR) specimens used in automotive and aeronautical fields.
关键词:
X-ray computed tomography
,
null
,
null
,
null
鲍永杰
,
曹波
,
李兰柱
,
高航
宇航材料工艺
采用研制的(Φ)4mm金刚石磨料刀具,研究SiCp/Al复合材料磨削制孔过程中工艺参数对轴向力和孔质量的影响规律.结果表明:刀具转速高于6 000 r/min、进给速度为5mm/min时,可以获得较好的制孔质量.
关键词:
铝基复合材料
,
钻孔
,
轴向力
,
缺陷
侯军涛
,
乔生儒
,
张程煜
,
张跃冰
新型炭材料
doi:10.1016/S1872-5805(08)60046-3
3D-C/SiC复合材料试样在空气介质中600℃、900℃和1300℃热曝露不同时间后,采用三点弯曲法测试了以室温弯曲弹性模量表征的损伤变化规律,并进行了SEM和EDS分析.结果表明:3D-C/SiC在热曝露15 h后,损伤变化可分为急剧上升(阶段Ⅰ)和平稳上升(阶段Ⅱ)两个阶段.阶段Ⅰ归因于炭纤维和炭层界面在空气中的直接氧化,阶段Ⅱ由复合材料内部氧的扩散所致.在复合材料制备过程的冷却阶段,因基体和炭纤维热膨胀系数不同所产生的基体微裂纹提供了氧化反应的表面与氧扩散的途径.在同一热曝露时间下,损伤随温度的上升而减少的原由可能是由于高温下裂纹收缩导致氧化表面减少,并降低氧向复合材料内扩散所致.
关键词:
3D-C/SiC
,
热曝露
,
损伤
,
弯曲性能
沈自才
,
姜海富
,
徐坤博
,
丁义刚
,
刘宇明
宇航材料工艺
doi:10.3969/j.issn.1007-2330.2016.02.001
基于航天材料在轨将遭遇多种空间环境的作用且不同空间环境对航天材料的损伤存在一定的关联性,本文首先对航天材料的空间环境及效应进行了介绍,接着对真空、温度、微重力、等离子体、粒子辐射、太阳电磁辐射、空间大气、空间碎片及微流星体、空间污染、空间动力学、腐蚀及空间生物等环境对航天材料的损伤机制及不同损伤机制之间的关联性进行了研究,最后对需要进一步研究和关注的方向进行了讨论并给出了发展建议.
关键词:
航天材料
,
空间环境
,
损伤
,
机制
刘礼平
,
戚春亮
,
王瑞峰
,
徐建新
,
周志强
宇航材料工艺
doi:10.12044/j.issn.1007-2330.2017.02.007
波音787飞机的机身蒙皮采用全复合材料,对于复合材料机身蒙皮的修理,波音787结构维修手册给出了明确的修理方案,其中包括复合材料机身蒙皮的钛合金板铆接修理.然而,对维修方案背后的理论依据,即强度、刚度等力学特性要求没有叙述.基于此,本文对复合材料机身蒙皮的钛合金板铆接修理建立了两种维修的三维有限元模型,分析了这两种维修方案母板、补片和填平板的应力大小和应力分布特性.研究表明:复合材料机身蒙皮大的穿透型裂纹钛合金板铆接修理能够满足静强度要求,两种维修方案的钛合金补片破坏源发生在不同位置.
关键词:
复合材料
,
机身蒙皮
,
损伤
,
修理
