Room and high temperature fatigue behaviour of the A354 and C355 (Al-Si-Cu-Mg) alloys: Role of microstructure and heat treatment

被引:56
作者
Ceschini, Lorella [1 ,2 ]
Morri, Alessandro [1 ,2 ]
Toschi, Stefania [1 ]
Seifeddine, Salem [3 ]
机构
[1] Univ Bologna, Alma Mater Studiorum, Dept Ind Engn DIN, Viale Risorgimento 4, I-40136 Bologna, Italy
[2] Univ Bologna, Alma Mater Studiorum, Ind Res Ctr Adv Mech & Mat CIRI MAM, Viale Risorgimento 4, I-40136 Bologna, Italy
[3] Jonkoping Univ, Sch Engn, Dept Mat & Mfg, Gjuterigatan 5, S-55111 Jonkoping, Sweden
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 2016年 / 653卷
关键词
Casting aluminium alloys; A354; C355; Overaging; High temperature fatigue; MECHANICAL-PROPERTIES; PRECIPITATION BEHAVIOR; TENSILE PROPERTIES; FRACTURE-BEHAVIOR; GRAIN-REFINEMENT; CAST; STRENGTH; PHASE; FE; DEFORMATION;
D O I
10.1016/j.msea.2015.12.015
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Al-Si-Mg alloys are widely used in the automotive industry for the production of engine components. Due to the new stringent emissions standards, these components undergo higher temperatures than in the past; as a result, alloys with higher thermal stability, such as the Al-Si-Cu-Mg, are currently under investigation. The present paper aims at widening the knowledge on the relationship between room temperature (RT) and high temperature fatigue behaviour of A354 and 055 alloys and their microstructural features, in particular, secondary dendrite arm spacing (SDAS) and intermetallic compounds. Samples for fatigue characterization were hot isostatic pressed, aiming to avoid the effect of solidification defects. The results of microstructural analyses and rotating bending fatigue tests highlighted that (i) SDAS influences room temperature fatigue behaviour of the peak-aged A354 and 055 alloys, while its effect on the overaged alloys at high temperature is negligible; (ii) fatigue cracks nucleated mostly from large intermetallic compounds; (iii) at room temperature, 055 alloy is characterized by higher fatigue strength (151 and 135 MPa for fine and coarse SDAS, respectively) in comparison to A354 alloy (133 and 113 MPa); after overaging and testing at high temperature, the behaviour of the two alloys is comparable. A good correlation between ultimate tensile strength and fatigue resistance was found, independent of microstructure and aging condition. (C) 2015 Elsevier B.V. All rights reserved.
引用
收藏
页码:129 / 138
页数:10
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