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弯曲冲凸一次成形模
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作者 康建召 康灿 《机械工人(热加工)》 2002年第9期63-63,共1页
图1所示支承件的材料为纯铜带,厚1.0mm。从结构上分析,该件有两道弯曲和一个凸台,如果弯曲和冲凸分别由单独的模具完成。
关键词 弯曲 冲凸 成形模 冲压
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小直径冲凸冲模设计
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作者 齐凤凯 《模具制造》 2004年第8期41-42,共2页
根据零件的结构特点,介绍了一种用于小直径冲凸成形的新型模具结构,并叙述该模具的工作过程。
关键词 冲凸 卸料装置 导向装置 冲模 设计 冲压
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壳体盖板级进模设计
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作者 姜伯军 《模具制造》 2018年第8期12-15,共4页
通过针对壳体盖板拉伸件的结构特点分析,对成形工艺过程和各工序间排列方案进行比较以及对所需设计、加工的级进模全部成形工艺及工序排列的过程和排样方案进行了确定。同时介绍了该级进模的主要工作零件及模具的总装结构设计。
关键词 拉伸工艺 工序分析 冲凸成形 冲孔 翻边 模具总装结构
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Injection and Extraction Techniques in Circular Accelerators
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作者 唐靖宇 《Chinese Physics C》 SCIE CAS CSCD 北大核心 2008年第z1期256-258,共3页
Injection and extraction are usually the key systems in circular accelerators.They play important roles in transferring the beam from one stage acceleration to the other or to experimental stations.It is also in the i... Injection and extraction are usually the key systems in circular accelerators.They play important roles in transferring the beam from one stage acceleration to the other or to experimental stations.It is also in the injection and extraction regions where beam losses happen mostly.Due to the tight space and to reduce the perturbation to the circulating orbit,the devices are usually designed to meet special requirements such as compactness,small stray field,fast rise time or fall time,etc.Usual injection and extraction devices include septum magnets,kicker magnets, electrostatic deflectors,slow bump magnets and strippers.In spite of different accelerators and specification for the injection and extraction devices,many techniques are shared in the design and manufacturing.This paper gives a general review on the techniques employed in the major circular accelerators in China. 展开更多
关键词 injection extraction technique SEPTUM kicker slow bump electrostatic deflector STRIPPER
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Shock control bump optimization for a low sweep supercritical wing 被引量:4
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作者 DENG Feng QIN Ning +2 位作者 LIU XueQiang YU XiongQing ZHAO Ning 《Science China(Technological Sciences)》 SCIE EI CAS 2013年第10期2385-2390,共6页
Shock control bumps are a promising technique in reducing wave drag of civil transport aircraft flying at transonic speeds.This paper investigates the optimization of 3D shock control bumps on a supercritical wing wit... Shock control bumps are a promising technique in reducing wave drag of civil transport aircraft flying at transonic speeds.This paper investigates the optimization of 3D shock control bumps on a supercritical wing with a sweep angle of 16°at the1/4 chord.A similar supercritical wing with a higher sweep angle of 24.5°at the 1/4 chord has been adopted as a baseline for the study.Numerical results show that the drag coefficient of the low sweep wing with the optimized 3D shock control bumps is reduced below that for the high sweep wing,indicating shock control bumps can be used as an effective means to reduce the wave drag caused by reducing the wing sweep angle.From the point of view of the wing structure design,lower sweep angle will also bring the benefits of weight reduction,resulting in further fuel reduction. 展开更多
关键词 supercritical wing low sweep angle shock control bump aerodynamic shape optimization computational fluiddynamics
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