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1.
A novel non-keyhole friction stir welding technique was proposed to weld the butt joint of 6061-T6 aluminum alloy with the thickness of 6 mm. A sound joint was obtained by this technique, simultaneously eliminating the flash, shoulder mark and keyhole defects. The sleeve directly affected zone (SDAZ) and the sleeve indirectly affected zone (SIAZ) were divided into the joint according to the plunging position of the hollow sleeve. The lack of root penetration defect was avoided when the plunging depth of the hollow sleeve was only 4.2 mm, because the hollow part inside the sleeve improved the material flow below the sleeve. An S-shaped line was left at the SIAZ, and the height of it had the minimum value of 1.47 mm at 20 mm/min. Whether the failure location of the joint was in SIAZ/SDAZ or the heat-affected zone (HAZ) depended on the height and bonding strength of the S-shaped line. The joint fracture location changed from the SIAZ/SDAZ at 35 mm/min to the HAZ at 20 and 30 mm/min. The maximum tensile strength of 224.3 MPa was obtained at 30 mm/min which was 73.7% of that of the base material. The fracture surface morphology exhibited the typical ductile fracture.  相似文献   
2.
Four tools with different pin centerline deviations were fabricated to friction stir weld (FSW) thick plates of Al-Mg-Zn-Cu alloys. The results show that, compared with the pin without pin centerline deviation, the applying of pin centerline deviation is favorable to improve the flowability of plastic material, enlarging the size of nugget zone, refining the grains and reprecipitated phase particles, enhancing the degrees of dynamic recrystallization and quantity of high angle grain boundaries owing to higher temperature and bigger eccentric force, resulting in the increase of strain hardening. Especially for the used pin with a centerline deviation of 0.2 mm, the highest average hardness and best metallurgical properties of thick FSW joints are produced, and which are consistent with the microstructure evolution and recrystallization behavior. Moreover, the fracture mode of the joints produced by the pins with centerline deviation from 0 mm to 0.3 mm changes gradually from a brittle fracture in the nugget zone (NZ) to a ductile failure in the HAZ.  相似文献   
3.
基于断裂力学理论对铝合金型材对搭接搅拌摩擦焊接头中Hook缺陷进行安全评定,并通过疲劳试验进行验证。金相显示Hook缺陷的本质是搭接面在搅拌头剧烈搅拌作用下向上迁移的结果,显现为裂纹的形式。将Hook缺陷归一化为延伸到焊缝内部的单边裂纹,裂纹扩展速率线性拟合得出应力强度因子幅度门槛值ΔKth为2.509 MPa·m1/2。依据裂纹扩展条件,得到评定Hook缺陷疲劳扩展的缺陷尺寸-应力幅关系曲线。疲劳试验结果与理论Hook缺陷临界扩展应力幅值有一定的误差,误差平均值为9.4%,整体趋势与理论曲线吻合度较好,可以将该理论公式应用到Hook缺陷疲劳扩展临界应力幅的预测中,对不同工作应力幅下接头中Hook缺陷进行安全评定。  相似文献   
4.
张翠翠  吴化  于晓丰 《表面技术》2021,50(5):315-320
目的 利用搅拌摩擦加工技术制备纳米SiC铝基复合材料,研究经过纳米粒子的添加和FSP作用后,其耐腐蚀性能的变化及原因.方法 室温条件下,在3.5%NaCl溶液中,通过电化学阻抗谱和动电位极化曲线对试样的耐腐蚀性能进行检测分析.利用电子背散射衍射技术和透射电镜对3种试样的显微组织进行表征,研究耐腐蚀性能的变化机理.结果 经搅拌摩擦加工后,样品的阻抗值明显提高,动电位极化曲线测试结果显示,母材、FSP试样和复合材料试样的自腐蚀电位分别为–1.517、–1.338、–1.339 V,而腐蚀电流密度分别为0.48、0.11、0.12 mA/cm2.FSP加工试样的晶粒由平均晶粒尺寸为8.7μm左右的等轴晶粒构成,并且大部分析出相因高温作用发生溶解,而纳米SiC粒子的加入,使晶粒尺寸进一步降低至4.1μm左右.结论 所制备Al6061/SiC复合材料的耐腐蚀性能相较于母材明显改善,但弱于FSP试样.SiC和基体之间电位差的存在构成腐蚀微电池,降低材料的耐腐蚀性能,而晶界数量的增加造成点阵空位等缺陷增加,导致电荷转移的阻力增加,耐腐蚀性能得到改善.  相似文献   
5.
为提高搅拌摩擦焊焊接成功率,基于相关工程经验和热传导理论,提出了一种在确定被焊工件厚度情况下保证焊接成功所需要的搅拌头最小轴肩直径的方法。讨论搅拌针直径和长度等参数的选取方法,以稳态焊接时搅拌头摩擦产热量等于工件内固塑分界面的散热量为基础,推导被焊工件厚度与所需搅拌头最小轴肩直径的关系方程,并探讨该方程相关参数的取值范围。以6061铝合金为例,通过该方程绘制工件厚度与搅拌头轴肩直径的关系图,其结果符合实际情况。  相似文献   
6.
《Ceramics International》2022,48(4):4710-4721
In this study, AA5083 sheets were reinforced with four different hybrid nanoparticles by friction stir processing (FSP) for the development of surface nanocomposites used in advanced engineering applications. The present research focused on improving the properties and tribological behaviour of AA5083 alloy surfaces, including novel hybrid nanoparticles and the intermetallic phase formed during FSP. A tribometer tester with a constant normal load was used to examine the tribological performance of the hybrid composites. After the wear test, a surface profiler inspector was used to analyse the morphology and surface roughness of the examined materials. The Vickers micro-hardness of the base metal and the manufactured composites were measured. During FSP, a new intermetallic phase of AlV3 was successfully formed at 300–400 °C in the hybrid nanocomposites containing VC particles. The reinforcements resulted in additional grain refining than FSP. The AA5083/Ta2C–Al2O3 exhibited the greatest grain refinement, a sixty-fold reduction in grain size compared to that of the base alloy. The results revealed that the hybrid nanocomposites containing VC particles demonstrated the most significant microhardness values inside the stirred zone as a result of the presence of the AlV3 phase, which was increased by 25–30%. Moreover, the mechanical properties were significantly improved for all manufactured nanocomposites. The tensile strength was increased by 28% through the hybridisation of AA5083 using a hybrid of VC-GNPs. The dispersion of Ta2C-GNPs and VC-GNPs in the matrix led to excellent interfacial adhesion, resulting in an enhancement in the mechanical properties. The AA5083/VC-GNPs surface composite outperformed other manufactured composites regarding wear resistance. In addition, due to GNPs soft nature, it reduced the coefficient of friction (COF) of the manufactured composites by 20–25% compared to other reinforcements.  相似文献   
7.
张文琼  方亮  谢天 《润滑与密封》2021,46(8):108-114
搅拌法制备SiC颗粒增强铝基复合材料时铺粉工艺对材料性能影响很大,影响SiC颗粒能否均匀地嵌入基体中。研究黏接剂、SiC颗粒粒径、颗粒铺粉厚度等对搅拌摩擦制备SiC颗粒增强铝基复合材料的影响。以焊缝宏观质量、SiC颗粒体积分数与硬度、基体组织及颗粒、复合材料不同深度维氏硬度、复合区面积(宏观)为表征参量对制备的复合材料进行表征,并得出最佳的铺粉工艺。结果表明:相比于α-氰基丙烯酸乙酯,聚乙烯醇作为黏接剂时,复合材料中SiC颗粒的分布更加均匀;嵌入基体的SiC颗粒体积分数随着SiC粉末粒径的增加而增加,而基体中SiC颗粒体积分数相同情况下,SiC颗粒的粒径越小对基体材料硬度的提高越明显;复合材料中SiC颗粒增强区面积会随着铺粉厚度的增加而增加,但增加铺粉厚度会使得SiC颗粒增强区硬度、体积分数的变化梯度增加。  相似文献   
8.
为了提高机箱焊缝的致密性,减少硫酸阳极化后机箱焊缝露白、槽液残留等问题,文中从铝合金机箱的结构特点入手,详细介绍了机箱搅拌摩擦焊结构和焊接夹具的设计要点、焊接和热处理的工艺参数等。通过样件的试生产和试验验证,模拟样件焊接接头的抗拉强度超过母材的80%,焊缝可实现180°无裂纹、无断裂的正向弯曲。同时,箱体结构也通过了产品的试验验证。该硫酸阳极化机箱搅拌摩擦焊的焊接结构设计及工艺,对此类产品的制造具有一定的指导意义。  相似文献   
9.
In this paper, cenosphere particles embedded in AA2014 aluminium matrix are used to fabricate syntactic foam by stir casting method. The particle size is about 100?µm and foam density is about 1990?kg?m?3. Compression tests at strain rate 0.001/s are performed on foam samples to characterise their mechanical properties which are then used in numerical analysis on commercial finite element analysis software ABAQUS/CAE with isotropic elastic-plastic material model. Experimental and numerical results show good conformity in deformation behaviour with elastic and plateau zones showing average deviations less than 5% and 20%, respectively. Foams showed high yield stress and energy absorption capabilities that can be useful in making blast and impact resistant structures.  相似文献   
10.
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