刘持栋
,
成来飞
,
梅辉
,
栾新刚
,
周俊
无机材料学报
doi:10.3724/SP.J.1077.2008.00729
采用应力比为0.1, 频率为3Hz的正弦波分别在室温和1300℃水氧环境对2D C/SiC复合材料进行了拉-拉疲劳试验．结果表明, 若取循环基数为105, 室温和高温水氧环境下的疲劳极限分别为244.8MPa和93.3MPa, 高温下的水氧腐蚀是材料失效的主要原因．根据疲劳断口特征分析得出以下结论: 在高温水氧环境下, 足够大的外载荷将会显著削弱SiO2层的封填裂纹效果, 导致氧化性气氛通过外力拉开的微裂纹扩散进入材料内部．外载荷越大, 气体在材料内部的扩散越快, 复合材料的疲劳寿命越短．
关键词:
2D C/SiC复合材料
,
fatigue
,
high temperature
,
oxidation
陈敏
,
朱贵文
,
周伟华
,
沈韩
,
李景德
无机材料学报
doi:10.3724/SP.J.1077.2007.00461
用铁电微分回线谱分析方法研究了Ba 0.99 Sr 0.01 TiO 3陶瓷的极化疲劳效应, 该方法可将线性和非线性电导、非铁电极化电容、以及纯铁电极化信号完全分开. 实验给出各效应对应的微分谱线型参数在疲劳过程中的变化规律, 并据此分出样品中分别由180°畴和90°畴提供的极化, 发现在同等作用下, 180°畴提供的极化更快出现疲劳.
关键词:
铁电性
,
fatigue
,
differential hysteresis loop
,
BST
张红霞
,
裴飞飞
,
闫志峰
,
王凯
,
王文先
,
刘晓晴
,
吴广贺
,
李咏梅
稀有金属材料与工程
采用红外热像法测量AZ31B镁合金板材在疲劳过程中表面温度场的变化,结果表明,当疲劳载荷大于疲劳强度时,镁合金试样表面的温度变化经历5个阶段:温度上升阶段、温度下降阶段、稳定阶段、断裂前的温升阶段和断裂后温度下降阶段.通过疲劳过程中镁合金试样表面的温度变化规律,基于不同的理论提出了2种预测疲劳寿命的方法:由试验过程中试样表面温升(△TM)特征确定其疲劳寿命,△TM-Nf曲线拟合结果表明,△TM=3.89℃为温升极限值,即△TM＞3.89℃时,试样会发生断裂,与实测疲劳试样的温升值(3.68℃)相比,误差为5.7％;利用能量法提出了镁合金疲劳寿命的计算公式,用能量法和传统试验方法分别绘制S-N曲线,结果具有很好的一致性,用2种方法分别计算了循环次数为1x107时的疲劳强度△σeφ=99.3 MPa、△σesN=99.8 MPa,误差为0.5％.采用红外热像法估算疲劳寿命具有简单、省时等优势.
关键词:
AZ31B镁合金
,
疲劳
,
红外热像法
,
疲劳寿命预测
,
能量法
文磊
,
王亚明
,
金莹
,
孙冬柏
稀有金属材料与工程
在2024铝合金表面制备纳米化-微弧氧化复合涂层,该复合涂层由底层纳米晶层及顶层陶瓷涂层构成.采用XRD、TEM和SEM研究了复合涂层的微观组织结构,并研究了表面处理对铝合金基体疲劳寿命的影响规律.顶层陶瓷涂层厚度分别为5和10 μm的复合涂层试样的疲劳寿命分别提高了21.9％和23.2％,疲劳性能的改善是基体合金靠近涂层区域的纳米晶结构及残余压应力共同作用的结果;当顶层陶瓷涂层厚度增加到15μm时,由于涂层表面较大的孔径及涂层内部存在的微裂纹,导致疲劳寿命降低.
关键词:
铝合金
,
疲劳
,
微弧氧化
,
表面机械研磨处理
J.H.Yang1
,
2)
,
S.X.Li1)and C.X.Ma2) 1) State Key Laboratoryfor Fatigueand Fracture of Materials
,
Instituteof Metal Research
,
The Chinese Academy of Sciences
,
72 Wenhua Road
,
Shenyang 110015
,
China 2) Department of Materials Physics
,
Northeastern University
,
Shenyang 110006
,
China
金属学报(英文版)
The dislocation evolution wassimulated by using positiveand negative parallelstraightedgedislocationsrandomly distributing on the primary slip planes astheinitialconditions. Thevein and wallstructuresof dynamicequilibrium have been obtained. Abig dipolestructure wasfound inthesimulation.
关键词:
computersimulation
,
null
,
null
,
null
STOLOFF
,
N.S. and ALVEN
,
D.A.(Department of Materials Engineering Rensselaer Polytechnic Institute Troy
,
New York
,
12180-3590
,
USA)
金属学报(英文版)
This paper reviews recent research on embrittlement of iron aluminides brought about by exposure to moisture or hydrogen. The tensile and fatigue crack growth behavior of several Fe-Al alloys, ranging in aluminum content from 16 to 35a%, is described. It will be shown that tensile ductility and fatigue crack growth behavior are dependent on type and degree of long range order, grain structure, temperature and environment. Environments studied include vacuum,oxygen, hydrogen gas, electrolytically charged hydrogen and moist air. All cases of embrittlement are ultimately traceable to the interaction of hydrogen with the lattice.
关键词:
: aluminides
,
null
,
null
,
null
,
null
Author J.H. Lee 1)
,
K.B. Yoon2)
,
Y.J. Kim3)and U.B. Baek4) 1) Engineering Research Department
,
Korea Institute of Nuclear Safety
,
P.O. Box 114
,
Yoosung
,
Taejon 305600
,
Korea2) Department of Mechanical Engineering
,
Chung Ang University
,
221 Huksuk
,
Dongjak
,
Seoul 156756
,
Korea3) Department of Mechanical Engineering
,
Sungkyunkwan University
,
300 Chunchun
,
Jangan
,
Suwon 440746
,
Korea4) Failure Prevention Research Center
,
Korea Research Institute of Standards and Science
,
P.O. Box 102
,
Yoosung
,
Taejon 305600
,
KoreaManuscript received 18 October 1998
金属学报(英文版)
Most of the assessment equations for Ct which is a wellknown fracture parameter characterizing high temperature crack growth rates, have limited applicability to constant load conditions after sudden loading. However, crack growth due to creep can also occur under load varying conditions when load rising time is so long that accumulated creep deformation near the crack tip is not negligible.In this paper, the estimation equation of the Ctparameter which can be applied to the case of slow load rising, i.e., (Ct)r, is explained. And the correlation between (Ct)r at the end of the load increasing period and Ct at the beginning of the succeeding load hold period is discussed. Finite element analyses of several cases with various loading conditions were performed and results were presented to show the effectiveness of the proposed Ct estimation scheme. The general applicability of the equation is also discussed.
关键词:
creep
,
null
,
null
,
null
,
null
,
null
