Alloy 7050(合金7050)研究综述
Alloy 7050 合金7050 - This research work is focused on modeling and analysis of connecting rod stress, deformation, fatigue strength, and life prediction for Toyota Hilux diesel engine made by four candidate materials (aluminum alloy 7068T6, aluminum alloy 7050 T765, carbon steel C-40 and forged steel 4340). [1] The purpose of this research is to predict fracture loci and fracture forming limit diagrams (FFLDs) considering strain rate for aluminum alloy 7050-T7451. [2] Applying the finite element software, the contact model of ultrasonic rolling process was built to simulate the ultrasonic rolling process of aluminum alloy 7050-T7451, and the distribution of equivalent plastic strain and residual stress distribution were analyzed effectively. [3] This paper describes a local blind-prediction challenge for a series of coupons manufactured from Aluminium Alloy 7050-T7451 plate simulating a combat aircraft wing root shear restraint (or shear tie post) subject to a combined aerodynamic buffet and manoeuvre load spectrum. [4] Graphene reinforced aluminium alloy 7050 based metal matrix composites are manufactured using stir mixing followed by squeeze casting technique wear property tests were carried out with pin-on-disc tribometer using dry sliding method on both the developed composites and the Al alloy 7050 to evaluate the properties of the composites. [5] This research article focuses on the development and characterization of Aluminum alloy 7050 matrix composites reinforced with Graphene nanoparticles. [6]本研究工作的重点是对四种候选材料（铝合金 7068T6、铝合金 7050 T765、碳钢 C-40 和锻钢）制造的丰田 Hilux 柴油发动机的连杆应力、变形、疲劳强度和寿命预测进行建模和分析。 4340）。 [1] 本研究的目的是根据铝合金 7050-T7451 的应变率预测断裂轨迹和断裂形成极限图 (FFLD)。 [2] 应用有限元软件，建立超声轧制接触模型，模拟7050-T7451铝合金的超声轧制过程，有效分析了等效塑性应变分布和残余应力分布。 [3] 本文描述了一系列由铝合金 7050-T7451 板制造的试样的局部盲预测挑战，模拟战斗机机翼根部剪切约束（或剪切系杆）受到组合空气动力学抖振和机动载荷谱的影响。 [4] 石墨烯增强铝合金 7050 基金属基复合材料是通过搅拌混合和挤压铸造技术制造的的复合材料。 [5] 本研究文章重点关注石墨烯纳米粒子增强铝合金 7050 基复合材料的开发和表征。 [6]
Aluminum Alloy 7050 铝合金7050
This research work is focused on modeling and analysis of connecting rod stress, deformation, fatigue strength, and life prediction for Toyota Hilux diesel engine made by four candidate materials (aluminum alloy 7068T6, aluminum alloy 7050 T765, carbon steel C-40 and forged steel 4340). [1] The purpose of this research is to predict fracture loci and fracture forming limit diagrams (FFLDs) considering strain rate for aluminum alloy 7050-T7451. [2] Applying the finite element software, the contact model of ultrasonic rolling process was built to simulate the ultrasonic rolling process of aluminum alloy 7050-T7451, and the distribution of equivalent plastic strain and residual stress distribution were analyzed effectively. [3] This research article focuses on the development and characterization of Aluminum alloy 7050 matrix composites reinforced with Graphene nanoparticles. [4]本研究工作的重点是对四种候选材料（铝合金 7068T6、铝合金 7050 T765、碳钢 C-40 和锻钢）制造的丰田 Hilux 柴油发动机的连杆应力、变形、疲劳强度和寿命预测进行建模和分析。 4340）。 [1] 本研究的目的是根据铝合金 7050-T7451 的应变率预测断裂轨迹和断裂形成极限图 (FFLD)。 [2] 应用有限元软件，建立超声轧制接触模型，模拟7050-T7451铝合金的超声轧制过程，有效分析了等效塑性应变分布和残余应力分布。 [3] 本研究文章重点关注石墨烯纳米粒子增强铝合金 7050 基复合材料的开发和表征。 [4]
Aluminium Alloy 7050 铝合金7050
This paper describes a local blind-prediction challenge for a series of coupons manufactured from Aluminium Alloy 7050-T7451 plate simulating a combat aircraft wing root shear restraint (or shear tie post) subject to a combined aerodynamic buffet and manoeuvre load spectrum. [1] Graphene reinforced aluminium alloy 7050 based metal matrix composites are manufactured using stir mixing followed by squeeze casting technique wear property tests were carried out with pin-on-disc tribometer using dry sliding method on both the developed composites and the Al alloy 7050 to evaluate the properties of the composites. [2]本文描述了一系列由铝合金 7050-T7451 板制造的试样的局部盲预测挑战，模拟战斗机机翼根部剪切约束（或剪切系杆）受到组合空气动力学抖振和机动载荷谱的影响。 [1] 石墨烯增强铝合金 7050 基金属基复合材料是通过搅拌混合和挤压铸造技术制造的的复合材料。 [2]