摘要
为解决淬火状态下30Cr3超高强度钢在真空电子束焊接时易产生冷裂纹、过热区脆化及热影响区软化等问题,在对材料性能分析的基础上,采取了提高真空度、提高加速电压、焊前预热、选择合适的焊接速度以及焊后回火处理等措施。结果表明,金相分析未发现缺陷,试样断口为塑性断裂,试片焊缝强度系数达0 96,产品爆破压力pb>27MPa。证明该方法可满足设计要求的焊接接头,为固体火箭发动机壳体的生产提供了新的工艺方法。
The tendency of cold crack, overheating area embrittlement and HAZ softening of 30Cr3 ultrahigh strength steel in quenching state after vacuum electron beam welding were introduced. A series of measures such as raising vacuum level, increasing acceleration voltage, preheating before welding, choosing suitable welding speed and tempering after welding were presented based on the material property analysis. The results show that no defect was found through metallographic analysis of weld joint. It also show that the fracture of sample is plastic one, the weld strength factor of the sample reaches as high as 0.96 and the bursting pressure of the product is more than 27 MPa. Thus, with the effective measures, qualified weld joint of 30Cr3 ultrahigh strength steel in quenching state can be manufactured, which will open a new way to the production of solid rocket motor case.
出处
《推进技术》
EI
CAS
CSCD
北大核心
2003年第5期478-480,共3页
Journal of Propulsion Technology
关键词
淬火硬化
电子束焊
真空焊
预热
回火
Cracks
Embrittlement
Preheating
Quenching
Rocket engines
Solid propellants
Steel
Strength of materials
Tempering
Vacuum welding