{"title":"Influence of Grinding on Residual Stress Measurements of Shot Peened Aluminium Alloy AA7075","authors":"S. Žagar, R. Sturm","doi":"10.5545/SV-JME.2019.6083","DOIUrl":null,"url":null,"abstract":"Aluminium alloys series 7xxx containing zinc, magnesium and copper, as the main alloy elements, are characterised by high ultimate tensile strength (UTS) between 350 MPa and 650 MPa, depending on the state of the alloy. For comparison, the extruded profiles from 6xxx alloys after heat treatment show the UTS at levels of 160 MPa to 340 MPa. Due to its high specific strength, formability, corrosion resistance, resistance to stress corrosion cracking, lightweight and wide application, the aluminium alloy 7075 is widely used in automotive and aerospace industries [1] to [4]. However, these alloys generally have poor ductility and low fracture strength in the as-cast condition, and extensive processing, which includes a combination of heat treatment and hot-cold working, is required to improve the mechanical properties [5]. González et al. [6] investigated different shot peening treatments with conventional and severe parameters, which were performed on an aluminium 6063 alloy in order to assess the differences induced in the microstructure of the surface layer and to evaluate their effects on fatigue behaviour. The obtained results evidence the notable influence of shot peening parameters on the surface layer microstructure, which simultaneously influence fatigue behaviour. Jamalian and Field [7] carried out a microstructural analysis of an AZ31 Mg alloy, which revealed a direct relation between the thickness of the ultra-fine grained layer and severe shot peening parameters, with each of them having a distinct effect on grain size. Furthermore, microhardness tests demonstrated how pressure and shot size control fine grains at the surface. Tensile test results revealed that the best mechanical properties were obtained by maximum shot size and pressure at minimum processing time. Nam et al. [8] investigated the effects of four peening parameters on microhardness and residual stress of AA 2124-T851. To verify the validity of the optimal conditions obtained from experimental results, metallurgical analyses of the shot-peened aluminium alloy were conducted with respect to hardness, residual stress, surface morphology, X-ray diffraction (XRD) analysis and surface roughness. They concluded that shot peening induces plastic deformation, increases surface hardness and introduces significant levels of compressive residual stress. Under optimal peening conditions, the average microhardness and compressive residual stress are ~13 % higher than that of the unpeened sample. Žagar and Grum [9] studied two types of aluminium alloys, EN AW 2007 and EN AW 6082, treated by shot peening, in which the surfaces of the metals were subjected to cold deformation Influence of Grinding on Residual Stress Measurements of Shot Peened Aluminium Alloy AA7075 Žagar, S. – Šturm, R. Sebastjan Žagar* – Roman Šturm University of Ljubljana, Faculty of Mechanical Engineering, Slovenia","PeriodicalId":135907,"journal":{"name":"Strojniški vestnik – Journal of Mechanical Engineering","volume":"12 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-07-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Strojniški vestnik – Journal of Mechanical Engineering","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.5545/SV-JME.2019.6083","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 2
Abstract
Aluminium alloys series 7xxx containing zinc, magnesium and copper, as the main alloy elements, are characterised by high ultimate tensile strength (UTS) between 350 MPa and 650 MPa, depending on the state of the alloy. For comparison, the extruded profiles from 6xxx alloys after heat treatment show the UTS at levels of 160 MPa to 340 MPa. Due to its high specific strength, formability, corrosion resistance, resistance to stress corrosion cracking, lightweight and wide application, the aluminium alloy 7075 is widely used in automotive and aerospace industries [1] to [4]. However, these alloys generally have poor ductility and low fracture strength in the as-cast condition, and extensive processing, which includes a combination of heat treatment and hot-cold working, is required to improve the mechanical properties [5]. González et al. [6] investigated different shot peening treatments with conventional and severe parameters, which were performed on an aluminium 6063 alloy in order to assess the differences induced in the microstructure of the surface layer and to evaluate their effects on fatigue behaviour. The obtained results evidence the notable influence of shot peening parameters on the surface layer microstructure, which simultaneously influence fatigue behaviour. Jamalian and Field [7] carried out a microstructural analysis of an AZ31 Mg alloy, which revealed a direct relation between the thickness of the ultra-fine grained layer and severe shot peening parameters, with each of them having a distinct effect on grain size. Furthermore, microhardness tests demonstrated how pressure and shot size control fine grains at the surface. Tensile test results revealed that the best mechanical properties were obtained by maximum shot size and pressure at minimum processing time. Nam et al. [8] investigated the effects of four peening parameters on microhardness and residual stress of AA 2124-T851. To verify the validity of the optimal conditions obtained from experimental results, metallurgical analyses of the shot-peened aluminium alloy were conducted with respect to hardness, residual stress, surface morphology, X-ray diffraction (XRD) analysis and surface roughness. They concluded that shot peening induces plastic deformation, increases surface hardness and introduces significant levels of compressive residual stress. Under optimal peening conditions, the average microhardness and compressive residual stress are ~13 % higher than that of the unpeened sample. Žagar and Grum [9] studied two types of aluminium alloys, EN AW 2007 and EN AW 6082, treated by shot peening, in which the surfaces of the metals were subjected to cold deformation Influence of Grinding on Residual Stress Measurements of Shot Peened Aluminium Alloy AA7075 Žagar, S. – Šturm, R. Sebastjan Žagar* – Roman Šturm University of Ljubljana, Faculty of Mechanical Engineering, Slovenia
7xxx系列铝合金含有锌、镁和铜作为主要合金元素,其特点是根据合金的状态,具有350兆帕至650兆帕之间的高极限抗拉强度(UTS)。相比之下,6xxx合金经过热处理后的挤压型材显示出160 MPa至340 MPa的UTS水平。7075铝合金由于具有高比强度、可成形性、耐腐蚀、抗应力腐蚀开裂、重量轻、应用广泛等优点,广泛应用于汽车和航空航天工业[1]~[4]。然而,这些合金在铸态下通常具有较差的延展性和较低的断裂强度,需要进行广泛的加工,包括热处理和热冷加工相结合,以提高其力学性能[5]。González等人[6]研究了6063铝合金在常规和严格参数下的不同喷丸强化处理,以评估表层微观组织的差异,并评估其对疲劳行为的影响。结果表明,喷丸强化参数对合金表层组织有显著影响,同时也影响合金的疲劳行为。Jamalian和Field[7]对AZ31镁合金进行了显微组织分析,发现超细晶层厚度与强喷丸参数之间存在直接关系,且每种参数对晶粒尺寸都有不同的影响。此外,显微硬度测试证明了压力和射丸尺寸如何控制表面的细晶粒。拉伸试验结果表明,在最短的加工时间内,最大的射丸尺寸和压力可获得最佳的力学性能。Nam等[8]研究了四种喷丸参数对AA 2124-T851显微硬度和残余应力的影响。为了验证实验结果得出的最佳工艺条件的有效性,对喷丸铝合金进行了硬度、残余应力、表面形貌、x射线衍射(XRD)分析和表面粗糙度等金相分析。他们得出结论,喷丸强化引起塑性变形,增加表面硬度,并引入显著水平的残余压应力。在最佳喷丸条件下,试样的平均显微硬度和残余压应力比未喷丸试样高约13%。Žagar和Grum[9]研究了两种类型的铝合金,EN AW 2007和EN AW 6082,经过喷丸处理,金属表面受到冷变形磨削对喷丸铝合金AA7075残余应力测量的影响Žagar, S. - Šturm, R. sebasjan Žagar* - Roman Šturm卢雅那大学,机械工程学院,斯洛文尼亚