Optimisation of the fatigue resistance of 2024-T351 aluminium alloys by controlled shot peening - methodology, results and analysis

被引:112
作者
Rodopoulos, CA
Curtis, SA
de los Rios, ER
SolisRomero, J
机构
[1] Sheffield Hallam Univ, Mat Engn Res Inst, Sheffield S1 1WB, S Yorkshire, England
[2] Univ Sheffield, Dept Engn Mech, Struct Integrit Res Inst, Sheffield S1 3JD, S Yorkshire, England
[3] Inst Technol Tlalnepantla, Mexico City 54070, DF, Mexico
基金
英国工程与自然科学研究理事会;
关键词
controlled shot peening; fatigue life; residual stresses; surface roughness;
D O I
10.1016/j.ijfatigue.2004.01.003
中图分类号
TH [机械、仪表工业];
学科分类号
0802 [机械工程];
摘要
A methodology dedicated to the optimisation of the fatigue properties of aluminium alloys by controlled shot peening is presented. Selection of the peening conditions is made out of the use of the Design of Experiment and the Effects Neutralisation Model. Both techniques allowed the optimisation both in terms of life and crack growth rates. Experimental determination and further analysis of the residual stress relaxation patterns revealed that at high stress levels, low cycle fatigue, life improvement is predominantly due to slow crack growth rates, while in high cycle fatigue the extension of life is attributed to a prolonged period of crack arrest. (C) 2004 Elsevier Ltd. All rights reserved.
引用
收藏
页码:849 / 856
页数:8
相关论文
共 24 条
[1]
*AIRB IND ENG DIR, 1996, 10011 AITM END DIR, P1
[2]
*ASTM, 1985, ANN BOOK ASTM STAND, P642
[3]
Baragetti S, 1997, INT J MATER PROD TEC, V12, P83
[4]
BOYER HE, 1997, METALS HDB
[5]
Callister W.D., 1991, MAT SCI ENG INTRO, P1
[6]
Analysis of the effects of controlled shot peening on fatigue damage of high strength aluminium alloys [J].
Curtis, S ;
de los Rios, ER ;
Rodopoulos, CA ;
Levers, A .
INTERNATIONAL JOURNAL OF FATIGUE, 2003, 25 (01) :59-66
[7]
Predicting the interfaces between fatigue crack growth regimes in 7150-T651 aluminium alloy using the fatigue damage map [J].
Curtis, SA ;
Romero, JS ;
de los Rios, ER ;
Rodopoulos, CA ;
Levers, A .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2003, 344 (1-2) :79-85
[8]
Modelling fatigue crack growth in shot-peened components of Al 2024-T351 [J].
De Los Rios, ER ;
Trull, M ;
Levers, A .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2000, 23 (08) :709-716
[9]
DELOSRIOS ER, 1999, P CEAS FOR CHURCH CO, P261
[10]
DORR T, 1999, INT C SHOT PEEN, V7, P153