航天推进技术研究院主办
[1]郭会民.15CrMoR+Incoloy825复合板的焊接工艺[J].火箭推进,2010,36(04):53-58.
Guo Huimin.Welding technology of 15CrMoR+Incoloy825 composite plate[J].Journal of Rocket Propulsion,2010,36(04):53-58.
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Guo Huimin.Welding technology of 15CrMoR+Incoloy825 composite plate[J].Journal of Rocket Propulsion,2010,36(04):53-58.
15CrMoR+Incoloy825复合板的焊接工艺
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
36
期数:
2010年04期
页码:
53-58
栏目:
工艺与材料
出版日期:
2010-08-15
- Title:
- Welding technology of 15CrMoR+Incoloy825 composite plate
- 文章编号:
- (2010)04-0053-06
- 分类号:
- V46
- 文献标志码:
- A
- 摘要:
- 通过大量的焊接工艺试验、分析及工艺评定试验验证，确定了15CrMoR+Incoloy825复合板焊接及在15CrMoR基体上堆焊Incoloy825复合层最佳的焊接工艺规范参数及焊接工艺方法。熔敷金属（包括堆焊金属）的力学性能、化学成分及复合层的耐腐蚀性能等各项技术指标均达到了设计要求。
- Abstract:
- Proper welding parameters for a 15CrMoR+Incoloy825 composite plate welding and Incoloy825 composite layer surfacing on 15CrMoR substrate were proposed based on extensive tests and analysis. Optimal standard parameters and methods were verified by welding assessment test. The mechanical properties and chemical composition of deposited metal (including surfacing metal) and corrosion resistance of composite layer met the design requirements.
参考文献/References:
[1]柯玉雄. 15CrMoR钢材的焊接[J]. 焊接技术, 2004, 33(3): 70. [2]郭会民, 赵仕哲, 李万万. 溶化极混合气体保护焊工艺研究与应用[J]. 火箭推进, 2007, 33(2): 57-62. [3]王辉. 钛合金张力贮箱焊接工艺改进[J]. 火箭推进, 2001, 27(5): 40-44. [4]丁新玲. 液体火箭发动机喷管延伸段制造新技术[J]. 航天制造技术, 2006, (6): 4-8+17. [5]周振丰, 张文钺. 焊接冶金与金属焊接性[M]. 北京: 机械工业出版社, 1990. [6]陈裕川. 低合金结构钢的焊接[M]. 北京: 机械工业出版社, 1992.
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备注/Memo
收稿日期：2010-０2-26；修回日期：2010-03-19。
作者简介： 郭会民（19６6—），男，高级工程师，研究领域为焊接工艺。
更新日期/Last Update:
1900-01-01