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材料研究学报  2026, Vol. 40 Issue (9): 677-684    DOI: 10.11901/1005.3093.2025.361
  研究论文 本期目录 | 过刊浏览 |
GH3536镍基高温合金电阻点焊电极的失效及其机理
胡峰1, 易润华1, 邓黎鹏1(), 徐康1, 高鹏飞1, 蒋志坚1, 徐忠2, 朱高东2, 谢思中2, 何毅涛2, 赵嘉成2
1.南昌航空大学材料科学与工程学院 南昌 330063
2.湖南南方通用航空发动机有限公司 株洲 412002
Failure Analysis of BeCoCu-alloy Electrodes for Resistance Spot Welding of GH3536 Nickel-based Superalloy Sheets
HU Feng1, YI Runhua1, DENG Lipeng1(), XU Kang1, GAO Pengfei1, JIANG Zhijian1, XU Zhong2, ZHU Gaodong2, XIE Sizhong2, HE Yitao2, ZHAO Jiacheng2
1.School of Materials Science and Engineering, Nanchang Hangkong University, Nanchang 330063, China
2.Hunan Southern General Aviation Engine Co., Ltd., Zhuzhou 412002, China
引用本文:

胡峰, 易润华, 邓黎鹏, 徐康, 高鹏飞, 蒋志坚, 徐忠, 朱高东, 谢思中, 何毅涛, 赵嘉成. GH3536镍基高温合金电阻点焊电极的失效及其机理[J]. 材料研究学报, 2026, 40(9): 677-684.
Feng HU, Runhua YI, Lipeng DENG, Kang XU, Pengfei GAO, Zhijian JIANG, Zhong XU, Gaodong ZHU, Sizhong XIE, Yitao HE, Jiacheng ZHAO. Failure Analysis of BeCoCu-alloy Electrodes for Resistance Spot Welding of GH3536 Nickel-based Superalloy Sheets[J]. Chinese Journal of Materials Research, 2026, 40(9): 677-684.

全文: PDF(12324 KB)   HTML
摘要: 

使用DZ-3×100型三相次级整流点焊机点焊1.3 mm厚的GH3536高温合金构件,研究了铍钴铜(BeCoCu)球面电极的失效并揭示其机理。结果表明,BeCoCu电极失效后其表面的合金层粘连,电极端面微观组织的尺寸明显增大,其服役寿命点数为220点;焊接时,合金试样中的Fe、Ni、Cr等元素向电极扩散生成(Fe, Ni)置换固溶体和Fe0.7Cr0.19Ni1.1、Cr0.19Fe0.7Ni0.11以及Cu0.81Ni0.19等脆性金属间化合物。电极的合金化使其表面产生微裂纹并脱落;电极的失效是强度较高的Cubic{100}<001>和{110}<100>织构转变为强度较低的Cubic<111>||ND织构,使试样的相对强度由4.12和5.62降低到3.05;在BeCoCu电极的服役过程中,大角度晶界的含量提高。以上因素的共同作用,使电极发生合金化而失效。

关键词 : 材料失效与保护,  失效分析,  电极寿命,  铍钴铜,  航空发动机,  电阻点焊    
Abstract:

The resistance spot welding of 1.3 mm-thick GH3536 nickel-based superalloy sheets was performed via DZ-X100 three-phase secondary rectifier spot welding machine with spherical electrodes made of BeCoCu-alloy, aiming to simulate the actual operating conditions in a production line, and to examine the applicability of the electrodes and their failure process after long term service. The results show that the useable number of times of the BeCoCu-alloy electrodes is approximately 220 times for spot welding. When the electrode fails, it can be observed that on the electrode end surface, metals-accumulation and -adhesion occur, the grains size increases, and pits appear due to erosion. These may be ascribed to that during welding, elements such as Fe, Ni, Cr etc. in the superalloy may diffuse inwards the electrode to form (Fe, Ni) substitution solid solution, as well as brittle intermetallic compounds such as Fe0.7Cr0.19Ni1.1, Cr0.19Fe0.7Ni0.11 and Cu0.81Ni0.19. Such alloying process may cause microcracks on the electrode surface, which is conductive to the occurrence of failure and spallation. The failure process involves the transformation of the alloy texture from stronger cubic {100}<001> and {110}<100> textures to weaker cubic<111>||ND texture, resulting in reduction of its relative strength from 4.12 and 5.62 to 3.05. Additionally, during the service process of BeCoCu electrode, the amount of high-angle grain boundary increases, which promotes alloying process of the electrode. These factors together lead to electrode failure.

Key words: materials failure and protection    failure analysis    electrode life    beryllium cobalt copper    aero-engine    resistance spot welding
收稿日期: 2025-12-03     
ZTFLH:  TG453.9  
基金资助:江西省自然科学基金(20252BAC250035)
通讯作者: 邓黎鹏,副教授,denglipeng@nchu.edu.cn,研究方向为钛合金、高温合金、铝合金等有色金属
Corresponding author: DENG Lipeng, Tel: 13870665644, E-mail: denglipeng@nchu.edu.cn
作者简介: 胡 峰,男,2002年生,硕士生
MaterialCrFeMoWCoPAlNiMnSiC
GH353621.7718.868.420.9080.9800.0110.164Bal.0.6960.2620.071
表1  GH3536合金的化学成分
图1  球面电极的示意图
图2  熔核直径与焊点个数的关系
图3  拉剪力与焊点个数的关系
图4  失效前后电极端面的微观形貌
图5  电极端面的SEM形貌
图6  电极端面的EDS分析
图7  失效后电极端面的XRD谱
图8  电极的反极图
图9  失效前后电极端面的PF和ODF
图10  电极失效前后的晶界图和取向差概率分布
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