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J4  2012, Vol. 46 Issue (5): 948-953    DOI: 10.3785/j.issn.1008-973X.2012.05.028
能源工程     
基于应变相对变化量的机体疲劳裂纹识别方法
张鹏伟1,2,刘震涛1,李建锋2,李京鲁2,俞小莉1
1. 浙江大学 能源工程学系,浙江 杭州 310027; 2. 潍柴动力股份有限公司,山东 潍坊 261001
Fatigue crack identification method based on relative
change of strain in engine block
ZHANG Peng-wei1,2, LIU Zhen-tao1, LI Jian-feng2, LI Jing-lu2, YU Xiao-li1
1. The Department of Energy Engineering, Zhejiang University, Hangzhou 310027,China;
2. Weichai Power Company, Limited, Weifang 261001, China
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摘要:

针对发动机机体疲劳试验中微裂纹诊断困难的现象,提出一种基于应变相对变化量的裂纹识别方法.建立机体的仿真模型,对可能出现裂纹的部位进行假象裂纹设制,并计算出现裂纹前后的应变值,得出结构出现裂纹前后应变的相对变化量,通过对应变相对变化量差分,求得差分曲线的有效零值点及有效极值点,由有效极值点与有效零值点确定位置指标,最终对裂纹部位进行定位.仿真计算结果表明:该方法对裂纹诊断具有敏感性,对裂纹的识别精度高,能够对给定应变测点连线上何处出现裂纹进行识别,定位最大误差为2.25%.

Abstract:

Crack identification is very difficultin the fatigue testof engine block, and a method for crack identification was put forward based on the differential of relative strain variation. Corresponding simulation model of block was established to simulate block fatigue test according to the block structure, loading mode and material, and three cracks were pre-produced on the simulation model,where cracks were possible to occur, meanwhile the corresponding strain were calculated from both undamaged and damaged block.The relative change of the strain and the differential curve can be obtained easily,so valid zero and extreme points of differential curve were easily found. According to zero and extreme points, the crack position can be indentified accurately, and the maximum error was only 2.25%. The simulation results indicates that the method is sensitive to crack and have a great significance to damage identification for block fatigue test.

出版日期: 2012-05-01
:     
通讯作者: 俞小莉,女,教授,博导.     E-mail: yuxl@zju.edu.cn
作者简介: 张鹏伟(1979-),男,博士生,主要从事内燃机结构可靠性研究.E-mail: zhangpengwei@zju.edu.cn
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引用本文:

张鹏伟,刘震涛,李建锋,李京鲁,俞小莉. 基于应变相对变化量的机体疲劳裂纹识别方法[J]. J4, 2012, 46(5): 948-953.

ZHANG Peng-wei, LIU Zhen-tao, LI Jian-feng, LI Jing-lu, YU Xiao-li. Fatigue crack identification method based on relative
change of strain in engine block. J4, 2012, 46(5): 948-953.

链接本文:

http://www.zjujournals.com/eng/CN/10.3785/j.issn.1008-973X.2012.05.028        http://www.zjujournals.com/eng/CN/Y2012/V46/I5/948

[1] BRANCO C M, INFANTE V, MARTINS R F. A failure analysis study of wet liners in maritime diesel engines [J]. Engineering Failure Analysis, 2002, 9(4): 403-421.
[2] CHO S S, SHIN C S, LEE C S. Assessment of an engine cylinder headblock joint using finite element analysis [J]. International Journal of Automotive Technology, 2010, 11(1): 75-80.
[3] 孙耀国,杜海明,周迅,等. 基于有限元的柴油机机体疲劳寿命仿真[J]. 内燃机工程,2009,30(4): 48-51.
SUN Yaoguo, DU Haiming, ZHOU Xun. Simulation of Fatigue life of diesel engine cylinder block based on finite element analysis [J]. Chinese Internal Combustion Engine Engineering, 2009, 30(4): 48-51.
[4] 陈学罡,李慧远,田雨苗. 发动机气缸体疲劳试验研究[J]. 汽车工艺与材料,2006,(3): 6-9.
CHEN Xuegang, LI Huiyuan, TIAN Yumiao. Research on fatigue test of engine cylinder block [J]. Automobile Technology & Material, 2006, (3): 6-9.
[5] 张晓艳,王生武,吴昌华. 16V240ZJ柴油机机体疲劳寿命评价方法的研究[J]. 内燃机与配件,2010,(4): 15-18.
ZHANG Xiaoyan, WANG Shengwu, WU Changhua. Study on method of fatigue life evaluation of 16V240ZJ diesel engine cylinder block [J]. Internal Combustion Engine & Parts, 2010, (4): 15-18.
[6] 崔建国,李明,陈希成. 基于声发射技术飞机关键零部件健康监测方法[J]. 仪器仪表学报, 2008, 29(10): 2126-2129.
CUI Jianguo, LI Ming, CHEN Xicheng. Health monitoring of airplane key components based on acoustic emission[J]. Chinese Journal of Scientific Instrument. 2008, 29(10):2126-2129.
[7] 王柏生, 倪一清, 高赞明. 青马大桥桥板结构损伤位置识别的数值模拟[J]. 土木工程学报, 2001, 34(3): 67-73.
WANG Baisheng, NI Yiqing, GAO Zanming. Numerical study of damage localization for tsing ma bridge deck [J]. China Civil Engineering Journal, 2001, 34(3): 67-73.
[8] CORNWELL P, DOEBLING S W, FARRAR C R. Application of the strain energy damage detection method to platelike structures [J]. Journal of Sound and Vibration, 1999, 233(3): 545-546.
[9] LI Y Y, CHENG L, YAM L H. Identification of damage locations for platelike structures using damage sensitive indices: strain modal approach \
[J\]. Computers & Structures, 2002, 25(14): 1785-1802.
[10] 李德葆, 诸葛鸿程, 王波. 实验应变模态分析原理和方法[M]. 北京:科学出版社,2001:66-68.

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