航天推进技术研究院主办
YU Kang,XIE Ronghua,CHEN Xiaojiang.Study on electron beam welding process for surface tension tank[J].Journal of Rocket Propulsion,2015,41(05):89-94.
表面张力贮箱电子束焊接工艺研究
- Title:
- Study on electron beam welding process for surface tension tank
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 对球形表面张力贮箱装配精度与表面张力贮箱焊缝熔深及形貌之间的关系进行了研究,得到了电子束焊接工艺规范。该规范为:采用虚焦电子束焊接工艺,聚焦束流虚焦30 mA,焊缝锁底部位宽度0.7 mm,焊接束流23 mA,焊接速度1 200 mm/min,焊接熔深2.4~3.3 mm。采用该规范焊接的表面张力贮箱通过了振动、液压、声发射等试验考核,表面张力贮箱满足设计要求,并通过了地面热试车考核。
- Abstract:
- The electron beam welding process specifications were obtained by studying the relationship of surface tension tank assembly precision, weld penetration and morphology. The specifications are: with the virtual focus electron beam welding process, when the virtual focus beam is upper than 30 mA, the seam width of lock bottom portion is 0.7 mm; when the welding beam is 23 mA, welding speed is 1200 mm/min and the weld penetration was 2.4~3.3 mm. The surface tension tank made according to the electron beam welding process specifications passed the assessment of vibration, hydraulic and acoustic emission tests, met the design requirements, and also passed the ground hot fire test.
参考文献/References:
[1]陈志坚, 孟庆平, 李建. 表面张力贮箱推进剂管理装置的计算[J]. 上海航天,2001(5):23-32.
[2]李治, 沈赤兵, 周进. 通道式表面张力贮箱通道的计算和确定[J]. 推进技术, 2003, 24(3): 244-246.
[3]DOMINICK S, TEGART J. Orbital test results of a vaned liquid acquisition device, AIAA 94-3027[R]. USA: AIAA, 1994.
[4]HOPKINS M A, DOLVIN D J, PAUL D B, et al. Structure technology for future aerospace system, AIAA-1998-1869 [R]. USA: AIAA,1998.
[5]DAROOKA D K, JENSEN D W. Advanced space stru- cture concepts and their development, AIAA-2001-1257 [R]. USA: AIAA, 2001.
[6]陈芙蓉, 霍立兴, 张玉凤. 电子束焊接技术在工业中的应用与发展[J]. 电子工艺技术. 2002, 23(2): 56-58.
[7]付鹏飞, 黄锐, 刘方军. TA12钛合金电子束焊接组织性能及残余应力分析[J]. 焊接学报, 2008, (2): 82-84.
[8]MLADENOV G, VUTOVA K, WOJCICKI S. Experi- mental investigation of the weld depth and thermal efficiency during electron beam welding[J]. Vacuum. 1998, 51(2): 231-233.
[9]杨彦涛, 王禹华, 张永洋. 氢对钛合金的影响[J]. 材料开发与应用, 2009, 1(24): 69-72.
[10]CHEN S C, HUANG J C. Comparison of post-weld microstructures and mechanical properties of electron and laser-beam welded 8090Al-Li alloy lates[J]. Mat- erials Transactions, 1999, 4(10): 1039-1078.
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备注/Memo
收稿日期:2015-04-02;修回日期:2015-05-28 作者简介:于康(1986—),男,工程师,研究领域为高能束焊接、扩散焊、钎焊等