余槐, 袁鸿, 张国栋, 等. 3种典型航空齿轮钢电子束焊接头微观组织与力学性能[J]. 焊接, 2024(3):33 − 39, 46. DOI: 10.12073/j.hj.20230710001
引用本文: 余槐, 袁鸿, 张国栋, 等. 3种典型航空齿轮钢电子束焊接头微观组织与力学性能[J]. 焊接, 2024(3):33 − 39, 46. DOI: 10.12073/j.hj.20230710001
Yu Huai, Yuan Hong, Zhang Guodong, et al. Microstructure and mechanical properties of electron beam welded joints of three typical aviation gear steels[J]. Welding & Joining, 2024(3):33 − 39, 46. DOI: 10.12073/j.hj.20230710001
Citation: Yu Huai, Yuan Hong, Zhang Guodong, et al. Microstructure and mechanical properties of electron beam welded joints of three typical aviation gear steels[J]. Welding & Joining, 2024(3):33 − 39, 46. DOI: 10.12073/j.hj.20230710001

3种典型航空齿轮钢电子束焊接头微观组织与力学性能

Microstructure and mechanical properties of electron beam welded joints of three typical aviation gear steels

  • 摘要: 齿轮轴的高质量焊接是影响直升机功重比和服役性能的关键,论文探讨了电子束焊接过程对中国三代典型的齿轮钢材料(9310,16Cr3NiWMoVNbE和CSS-42L)的微观组织与力学性能的影响。结果表明,3种齿轮钢基体组织均为细小针状马氏体,而电子束焊缝则显著粗化,尤其9310焊缝晶粒长大明显,CSS-42L热影响区在电子束热作用下变化显著,从焊缝边界到母材可分为4种不同形貌的组织,呈现出极端不均匀的现象。9310和16Cr3NiWMoVNbE焊缝显微硬度明显高于基体,而CSS-42L焊缝显微硬度则显著低于基体;3种焊接接头显微硬度最低值均出现在热影响区,表明热影响区是整个结构最薄弱区域,力学性能测试结果也充分表明了这一结论。3种齿轮钢电子束焊接头拉伸断裂全部发生在热影响区,强度较基体稍有下降;断裂之前发生了明显的颈缩现象,塑性下降不显著。CSS-42L性能显著优于9310和16Cr3NiWMoVNbE,CSS-42L电子束焊接头强度也高出9310焊接接头强度50%,塑性更加显著,高出超过20%。研究结果为直升机传动系统制造提供科学依据。

     

    Abstract: High quality welding of gear shaft is critical to improving power-to-weight ratio and service performance of helicopter transmission systems. Effect of electron beam welding process on microstructure and mechanical performance of three gear steels (9310, 16Cr3NiWMoVNbE and CSS-42L) was deeply discussed. The results showed that microstructure of three gear steel was all tiny needle martensite, grain size of weld was obviously coarse after electron beam welding, especially grain size of 9310 weld was obviously coarse. Significant change appeared in heat affected zone of CSS-42L under the action of electron beam heat, four different kinds of microstructure formed from weld boundary to base metal, appearing extremely inconsistency phenomenon. Hardness of 9310 and 16Cr3NiWMoVNbE weld was higher than that of base metals, while hardness of CSS-42L weld was lower than that of base metal. The lowest hardness zone of three kinds of welded joints was all located in HAZ, indicating that HAZ was the weakest zone of welded joints, and it was supported by mechanical test results. Tensile fracture appeared in HAZ of three EBW joints. Tensile strength and torsional strength of welded joints were slightly lower than those of base metals. Obvious necking phenomenon occurred before fracture, so plasticity reduction was little. Mechanical properties of CSS-42L were all higher than those of 9310 and 16Cr3NiWMoVNbE. Strength of CSS-42L EBW joints was higher over 50% than that of 9310 EBW joints, and plasticity exceeded over 20% than those of two gear steel EBW joints. The results provided scientific support for manufacturing of helicopter transmission systems.

     

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