1) titanium alloy shell
钛合金壳体
1.
Manual argon arc welding technology of TC4 titanium alloy shell;
TC4钛合金壳体的手工氩弧焊工艺
2) aluminum-titanium-alloy grid-shell
铝钛合金网壳
1.
The oval glass hall of Shanghai Science & Technology City consists of only aluminum-titanium-alloy grid-shell, which has pure installation system, and glass skin plates.
上海科技城卵球形玻璃大厅由纯安装体系的铝钛合金网壳与玻璃面板组成 ,在空间定位、杆件安装、节点固定和玻璃安装过程中 ,采取高精度测量控制手段 ,合理的安装顺序及防止产生附加应力的措施 ,确保了安装的顺利进行。
3) titanium alloy cabin
钛合金舱体
1.
This paper discusses the reason and harm of incomplete penetration rounded welded root of titanium alloy cabin with lock bottom structure in air-to-air missile,and presents several solutions of this problem.
对空空导弹钛合金舱体插接锁底结构圆周焊缝根部未焊透的产生原因和危害进行了讨论,提出了几套解决和防止根部未焊透缺陷的工艺方案。
4) aluminum alloy shell
铝合金壳体
1.
The paper briefly introduces the characters of warm extrusion and emphases on application advantages for parts of aluminum alloy shells and influencing factors on technological process.
简要介绍了温挤压技术的特点,重点介绍了该技术在铝合金壳体类零件上的应用优势和影响工艺过程中的各种因素,温挤压技术已成功推广应用于铝合金壳体类零件成形的批量生产之中,使生产成本降低25%,生产效率提高70%。
2.
The difficulty of aluminum alloy shell workpiece with empennages was analyzed during plasticity forming,and its forming process and die designing was introduced.
分析了带尾翼铝合金壳体零件在塑性成形过程中的难点,介绍了壳体零件的成形工艺与模具设计的方法。
5) tungsten alloy shell
钨合金壳体
1.
Normal penetration of a tungsten alloy shell into a concrete target was performed and the strain history of the critical section of the shell was obtained with the aid of an onboard recording system.
通过自行设计的弹载存储测试系统 ,进行了钨合金壳体垂直侵彻混凝土靶板的实验 ,获得了钨合金壳体危险截面处的应变—时间历程。
2.
The mic rostructure of received shells was e xamined and analyzed,revealing that the formation of adiabatic shear band at critical section is the mainl y failure behavior of tungsten alloy shell,and matrix rupture at the tip o f internal hollow also results in the damage of the shell.
进行了钨合金壳体垂直侵彻45钢靶板的实验,成功地获得钨合金壳体侵彻钢靶板时变形破坏演变的完整过程。
补充资料:Ti-55高温钛合金显微组织
Ti-55高温钛合金显微组织
丫‘“合‘{丫:黔
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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