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1)  aluminum alloy 7050-T7451
铝合金7050-T7451
1.
Then the orthogonal cutting force tests were conducted to obtain the tangential force and normal force in order to investigate the average friction coefficient on the rake face in machining aluminum alloy 7050-T7451.
基于对传统的剪切角模型的分析,借助快速落刀试验及直角切削力试验,获得了航空铝合金7050-T7451在切削加工中的剪切角以及前刀面的平均摩擦因数。
2)  7050-T7451 aluminum alloy
7050-T7451铝合金
3)  7050 Al alloy
7050铝合金
1.
Small angle x-ray scattering study on microstructure and mechanical property evolutions of equal-channel angular pressed 7050 Al alloy;
7050铝合金等通道转角挤压过程中显微结构和力学性能演化的小角x射线散射研究
2.
Feather crystals are often existed in conventional DC casting 7050 Al alloy ingots.
常规DC铸造7050铝合金铸锭常常含有羽毛晶组织缺陷。
4)  7050 aluminum alloy
7050铝合金
1.
Modeling of Semi-continuous Casting Process for 7050 Aluminum Alloy Ingot;
7050铝合金大铸锭半连续铸造过程数值模拟
2.
Change of the microstructure of 7050 aluminum alloy ingot during homogenization annealing;
7050铝合金铸锭均匀化过程中相的转变
3.
Grain Refinement of 7050 Aluminum Alloy;
7050铝合金晶粒细化的研究
5)  7050 aluminium alloy
7050铝合金
1.
In this paper, the process of free forging and die forging for 7050 aluminium alloy was simulated on the platform of DEFORM-3D, and the microstructure module was applied to simulate the law of the microstructure evolution.
本文在DEFORM-3D平台上对7050铝合金大锻件自由锻工艺及模锻工艺进行了模拟,并利用微观组织模块对锻造过程中微观组织演变进行了模拟。
2.
The effect of melt ultrasonic treatment(400 W) on the pores,microstructure and as-cast component distribution of 7050 aluminium alloy was studied by metalloscopy,Archimedes\' method,scanning electron microscopy and electron probe micro analysis.
采用光学显微镜、阿基米德法、扫描电镜及电子探针等手段研究了熔体经400 W超声处理对7050铝合金铸锭中的气孔、密度、显微组织及成分分布等的影响。
3.
The effect of alternating magnetic field frequency on the meniscus,microstructure and element distribution of the static formed ingots of minitype square billet of 7050 aluminium alloy.
研究了在交变磁场作用下磁场频率变化对7050铝合金小型方坯静态成型铸坯熔体的弯液面、显微组织以及元素分布的影响。
6)  7050 aviation aluminum-alloy
7050航空铝合金
1.
To investigate the correlation between parameters of "single factor" constitutive model and temperature for 7050 aviation aluminum-alloy,theoretic analyses and material experiments were employed.
从理论和实验两方面研究7050航空铝合金“单因素”本构模型中参数与温度的相关性。
补充资料:氟碳涂层铝合金装饰板制成的铝合金幕墙建筑物


氟碳涂层铝合金装饰板制成的铝合金幕墙建筑物


J氟碳涂层铝合金装饰板制成的铝合金幕墙建筑物
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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