冷轧与拉伸复合预变形对2519A铝合金板材应力腐蚀的影响(英文)

采用10-6s-1慢应变拉伸测试手段研究冷轧与拉伸复合预变形对2519A铝合金抗应力腐蚀开裂性能的影响。冷轧7%后再垂直拉伸3%的合金板材抗拉强度和应力腐蚀指数分别为481MPa和0.0429,与冷轧4%后再平行拉伸3%以及冷轧7%后再平行拉伸3%的合金板材相比表现出了更好的力学性能和抗应力腐蚀开裂性能。这主要是由于冷轧7%后再垂直拉伸3%在合金板材中生成了密度更高且分布更均匀的位错组织,使时效后合金板材晶内析出相细小、密集,晶界析出相不连续,晶界无沉淀析出带且较窄。     

T9I6形变热处理工艺对2519A铝合金组织、力学性能及抗弹性能的影响(英文)

借助金相显微镜、透射电镜、拉伸测试、抗弹性能测试等手段研究T9I6新型形变热处理对2519A铝合金组织、力学性能和抗弹性能的影响。经T9I6工艺处理的2519A铝合金,其屈服强度、抗拉强度、伸长率分别达到501 MPa、540 MPa、14%。30 mm厚的2519A-T9I6铝合金板材的极限穿透速度达715 m/s。弹坑侧壁组织随着弹孔深度的变化而变化。T9I6热处理工艺中的断续时效阶段是2519A铝合金性能提升的关键。低温下的时效使得GP区变得密集,从而使得后续相的析出也变得更为密集、细小。     

时效工艺对2519铝合金热轧板材抗应力腐蚀敏感性的影响

以腐蚀的强度指标(Kσ)和腐蚀的伸长率指标(Kδ)评定合金的抗应力腐蚀敏感性, 研究了2519铝合金热轧板材在T6、T7和T8状态下的抗应力腐蚀敏感性.试验结果表明,2519铝合金热轧板材的抗应力腐蚀敏感性按T8>T7>T6 排序,而它们的力学性能按T6>T8>T7的顺序排列.另外,测试了室温下T6、T7 和T8状态2519铝合金试样的恒电位极化曲线,发现可以以合金的极化电阻定性地描述合金的抗应力腐蚀敏感性,且当合金的极化电阻越大时,合金的抗应力腐蚀敏感性越好.     

高温预析出和固溶温度对7A52合金应力腐蚀开裂的影响

通过对高温预析出处理的7A52合金在T61和自然时效状态的强度、硬度、电阻率和应力腐蚀开裂（SCC）的测试,对比分析了高温预析出对7A52合金自然时效和T61时效状态下应力腐蚀性能的影响。研究结果表明：高温预析出可以提高自然时效和人工时效状态7A52合金的抗应力腐蚀性能,同时强度和伸长率有所增加;对于T61时效状态的7A52合金可保持其拉伸强度在500MPa,伸长率在13．O％。475℃固溶处理后T61状态下的7A52合金,不论是否经高温预析出处理合金抗应力腐蚀性能都优于经480℃固溶处理的T61状态下的7A52合金的抗应力腐蚀性能。     

2519铝合金热轧板材抗应力腐蚀敏感性研究

以腐蚀强度指标Kσ和腐蚀伸长率指标Kδ评定合金的抗应力腐蚀敏感性，研究了2519铝合金热轧板材在T6、17和T8三种时效状态下的抗应力腐蚀敏感性。结果表明，2519铝合金热轧板材的抗应力腐蚀敏感性由高到低按118、17、T6工艺排序，而它们的力学性能按T6、T8、17的顺序排列。另外，测试了三种工艺状态下2519铝合金试样的恒电位极化曲线，发现合金的极化电阻越大时，其抗应力腐蚀敏感性越好。     

热处理制度对2519铝合金板材力学性能和应力腐蚀敏感性的影响

选用3种不同的热处理工艺对2519铝合金板材进行处理，采用测定试样在腐蚀前后力学性能的变化即腐蚀的力学性能指标Kσ和Kδ来评定2519铝合金的应力腐蚀敏感性。结果表明：2519铝合金板材经先高温后低温的双级时效处理(180℃，3h 145℃，24h)后力学性能最好，抗应力腐蚀性能最差；而经形变热处理(20℃，100h 冷加工15％ 145℃，21h)后的力学性能较好，抗应力腐蚀性能最好；过时效状态(180℃，30h)下力学性能最差，抗应力腐蚀性能适中。     

最终形变热处理对7097铝合金锻件组织与性能的影响

采用力学性能测试、剥落腐蚀试验、光学显微镜、扫描电镜以及透射电镜等对最终形变热处理后的7097铝合金锻件的力学性能各向异性和抗腐蚀性能进行了研究.结果表明:合金的综合性能随着预变形程度的增加先升高后降低.采用3％预拉伸在保持与未进行预拉伸的三级时效态7097铝合金拉伸性能相近的同时,合金抗应力和抗剥落腐蚀性能提升,其中...     

Sc及回归再时效处理对7075铝合金抗应力腐蚀性能的影响

采用铸锭冶金法制备了常规和含0.23%Sc的两种7075铝合金,使用光学显微镜和扫描电镜分析了合金的微观组织,并采用拉伸试验、慢应变速率拉伸试验研究了两种合金在T6、T73和回归再时效(RRA)3种时效状态下的力学性能和抗应力腐蚀性能。结果表明,在相同时效状态下,Sc明显细化了7075合金晶粒,合金的力学性能,尤其是抗应力腐蚀性能得到明显提高。相对于T6处理而言,T73处理使两种合金的强度下降,抗应力腐蚀性能增加,RRA处理使合金在保持T6状态力学性能的同时,具有接近于T73状态的抗应力腐蚀性能。     

T916形变热处理工艺对2519A铝合金组织、力学性能及抗弹性能的影响

借助金相显微镜、透射电镜、拉伸测试、抗弹性能测试等手段研究T916新型形变热处理对2519A铝合金组织、力学性能和抗弹性能的影响。经T916工艺处理的2519A铝合金,其屈服强度、抗拉强度、伸长率分别达到501MPa、540MPa、14％。30mm厚的2519A-T916铝合金板材的极限穿透速度达715m／s。弹坑侧壁组织随着弹孔深度的变化而变化。T916热处理工艺中的断续时效阶段是2519A铝合金性能提升的关键。低温下的时效使得GP区变得密集,从而使得后续相的析出也变得更为密集、细小。     

高温预析出对Al-Zn-Mg铝合金组织、力学性能和应力腐蚀性能的影响

研究了近固溶度高温预析出工艺对抗应力腐蚀性能较差的中强可焊7A52和仿7039合金的组织、时效硬化和应力腐蚀性能的影响.显微组织观察、力学性能分析及应力腐蚀性能测试结果表明:近固溶度高温预析出处理可使合金在晶界形成不连续的析出相;在保持合金强度、塑性的同时,预析出可提高抗应力腐蚀性能,但预析出温度过低,合金强度呈下降趋势;固溶后于400℃预析出处理在峰值时效状态下可使7A52铝合金强度和抗应力腐蚀性能得到最佳组合,抗应力腐蚀性能达到三级时效后的效果.     

Mechanical properties of hot rolled 2519 aluminum alloy plate

1　INTRODUCTIONThemainadvantageof 2 5 19aluminumalloyisitsspecificstrengthandthereforeitisconsideredasagoodchoiceforaviationandshippingindustry .How ever,theseapplicationsmayberestrictedby poorcharacteristicssuchasresistancetostresscorrosioncracking ,strengthandplasticity .Thesecharacteris ticsdependintensivelyonthedistributionofthesec ondphaseparticleandthesizeandshapeofgrainsthataredeterminedby proces sing andheattreat ment.Stresscorrosioncrackingisthetypeofattackinwhichatensileandacorr…     

新型Al-Zn-Mg-Cu合金型材回归再时效处理的组织与性能

采用拉伸、硬度、电导率测试和透射电镜分析等方法研究了不同回归处理工艺对Al-Zn-Mg-Cu合金型材组织与性能的影响。结果表明,采用120℃×24 h+180℃×45 min+120℃×24 h回归再时效处理后,合金的抗拉强度、屈服强度、伸长率和电导率分别为613.5 MPa、599 MPa、11.1%和39.2%IASC。与T6态相比,合金在抗拉强度和伸长率相当的情况下,屈服强度和电导率显著提高,合金的抗应力腐蚀性能明显改善。合金晶内为细小的η’相和η相,晶界沉淀相断续分布,伴有较窄的晶界无析出带。     

Retrogression and re-aging treatment of Al-9.99%Zn-1.72%Cu-2.5%Mg-0.13%Zr aluminum alloy

1 Introduction The 7000 series aluminum alloys have been widely used as aircraft structure material because of their high strength/density ratio. This series of alloys provide high strength in the T6 condition but are prone to stress corrosion cracking(SC…     

多级热处理工艺对铝合金AA7049性能的影响(英文)

T6态高强7xxx系列铝合金对应力腐蚀开裂敏感。采用回归和再时效热处理(RRA)可以提高其抗应力腐蚀开裂性能而不降低其强度性能。研究了多级热处理工艺对7049铝合金性能和组织的影响。通过电导率测量、DSC分析和TEM组织观察,考察合金在不同热处理态的组织变化。DSC分析表明,RRA处理会导致合金的显微组织发生显著变化,RRA处理态合金的组织与T6和T73态合金的组织明显不同。RRA处理可以使合金保持在T6态的强度且获得T73态的热力学稳定性能。     

Stress-corrosion cracking susceptibility of various product forms of aluminum alloy 2519

Aluminum alloy 2519 is the main structural alloy for the Advanced Amphibious Assault Vehicle (AAAV). A potential drawback to the use of 2519, particularly for an amphibious vehicle, is its susceptibility to corrosion. General corrosion, which is largely in the form of pitting, may reduce the effective life of the system, while stress-corrosion cracking (SCC) of any high strength aluminum alloy can lead to catastrophic failure. Therefore, an evaluation of the SCC susceptibility of various 2519 product forms was performed. Plate, extrusions, ring roll forgings, and weldments all exhibited excellent SCC resistance as measured by a series of standard ASTM tests. Multi-axis hand forgings were the only product forms that exhibited SCC susceptibility, and this susceptibility was remedied via the use of a specifically designed heat treatment. While all product forms passed the prescribed SCC tests, each exhibited a significant reduction in strength after simultaneous exposure to both stress and the saline corrosion environment. Such behavior was not apparent when the exposure was limited to the corrosion media alone. That is, while resistant to SCC, the load-bearing capacities of all products tested are somewhat degraded during concurrent exposure to stress and corrosive media by a mechanism that includes pitting. This article will discuss the effort that was conducted by the National Center for Excellence in Metalworking Technology (NCEMT) to evaluate the SCC susceptibility of 2519 in various product forms and tempers.     

Study of the SCC Behavior of 7075 Aluminum Alloy After One-Step Aging at 163 °C

For the past many years, 7075 aluminum alloys have been widely used especially in those applications for which high mechanical performances are required. It is well known that the alloy in the T6 condition is characterized by the highest ultimate and yield strengths, but, at the same time, by poor stress corrosion cracking (SCC) resistance. For this reason, in the aeronautic applications, new heat treatments have been introduced to produce T7X conditions, which are characterized by lower mechanical strength, but very good SCC behavior, when compared with the T6 condition. The aim of this study is to study the tensile properties and the SCC behavior of 7075 thick plates when submitted to a single-step aging by varying the aging times. The tests were carried out according to the standards and the data obtained from the SCC tests were analyzed quantitatively using an image analysis software. The results show that, when compared with the T7X conditions, the single-step aging performed in the laboratory can produce acceptable tensile and SCC properties.     

时效时间对7150铝合金组织和性能的影响

通过维氏硬度测试、电导率测试和拉伸、晶间腐蚀等测试方法,研究了预时效、回归及再时效三个阶段中的时效时间对7150铝合金组织和性能的影响,借助透射电镜观察时效处理各阶段合金的微观组织演变。结果表明:120℃×20 h欠时效作为预时效工艺,比120℃×24 h峰时效的晶内析出相更细小,高温回归时更利于回溶。在190℃短时回归5、15和30 min中,15 min回溶效果最好,硬度最低,再经120℃×24 h再时效后合金抗拉强度Rm、屈服强度RP0.2、伸长率A分别为622 MPa、573 MPa、10.8%,显微硬度为204 HV,力学性能与120℃×24 h单级峰时效时相近。经120℃×20 h+190℃×15 min+120℃×24 h处理后7150铝合金综合性能好,耐晶间腐蚀性能佳。     

Effect of secondary aging on microstructure and properties of cast Al-Cu-Mg alloy

To obtain better comprehensive properties of cast Al-Cu-Mg alloys, the secondary aging (T6I6) process (including initial aging, interrupted aging and re-aging stages) was optimized by an orthogonal method. The microstructures of the optimized Al-Cu-Mg alloy were observed by means of scanning electron microscopy and transmission electron microscopy, and the properties were investigated by hardness measurements, tensile tests, exfoliation corrosion tests, and intergranular corrosion tests. Results show that the S phase and θ′ phase simultaneously exist in the T6I6 treated alloy. Appropriately increasing the temperature of the interrupted aging in the T6I6 process can improve the mechanical properties and corrosion resistance of Al-Cu-Mg alloy. The optimal comprehensive properties (tensile strength of 443.6 MPa, hardness of 161.6 HV) of the alloy are obtained by initial aging at 180 °C for 2 h, interrupted aging at 90 °C for 30 min, and re-aging at 170 °C for 4 h.