焊接2024,Issue(1) :27-32.DOI:10.12073/j.hj.20220729001

30mm厚TC4钛合金电子束焊接头的高周疲劳与裂纹扩展速率

High cycle fatigue and crack growth rate of 30 mm thick TC4 titanium alloy electron beam welded joint

贾金龙 龙健 张林杰
焊接2024,Issue(1) :27-32.DOI:10.12073/j.hj.20220729001

30mm厚TC4钛合金电子束焊接头的高周疲劳与裂纹扩展速率

High cycle fatigue and crack growth rate of 30 mm thick TC4 titanium alloy electron beam welded joint

贾金龙 1龙健 2张林杰2
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作者信息

  • 1. 兰州工业学院,兰州 730050
  • 2. 西安交通大学,金属材料强度国家重点实验室,西安 710049
  • 折叠

摘要

文中对比研究了30mm厚TC4 钛合金电子束焊接头和母材的高周疲劳性能,发现接头的高周疲劳性能与母材非常接近.在文中试验条件下,电子束焊接头在循环周次为 2×106 时的高周疲劳强度为 474 Mpa,达到母材的 94.2%.观察电子束焊接头和母材的高周疲劳断口形貌,发现接头和母材的疲劳源均位于试样表面.疲劳裂纹扩展区都发现疲劳辉纹,相同载荷条件下,母材高周疲劳断口中辉纹的间距较小,约为 1.49 μm,电子束焊接头的相邻辉纹间距为 2.14 μm.在接头和母材的疲劳瞬断裂区还发现大量韧窝,呈现出典型的韧性断裂特征.文中还对比了母材、热影响区和焊缝区的疲劳裂纹扩展速率,发现热影响区的抗疲劳裂纹扩展性能最弱.分析认为,热影响区的高硬度是导致其抗疲劳裂纹扩展性能弱于其他区域的重要原因.

Abstract

High cycle fatigue properties of 30 mm thick TC4 titanium alloy electron beam welded joints and base material were compared and studied in this paper,it was found that high cycle fatigue performance of welded joints was very close to that of base material.Under the experimental conditions,high cycle fatigue strength of electron beam welded joints was 474 MPa when number of cycles was 2×106,reaching 94.2%of base material.By observing high cycle fatigue fracture morphology of welded joints and base material,it was found that fatigue sources were located on the samples'surface of welded joints and base material.Fatigue cracks were found in the fatigue crack growth area.Under the same load condition,spacing of scratches in the high cycle fatigue fracture of base material was smaller,about 1.49 μm,and spacing of the adjacent scratches of electron beam welded joints was 2.14 μm.A large number of dimples were found in the final tensile fracture area of welded joints and base material,showing characteristics of ductile fracture.Fatigue crack propagation rate of base material,heat affected zone and weld zone was also compared in this paper,and it was found that fatigue crack propagation resistance of heat affected zone was the weakest.It was concluded that high hardness of heat affected zone was an important reason for its weaker anti-fatigue crack growth performance than other areas.

关键词

钛合金/电子束焊接/高周疲劳/裂纹扩展速率

Key words

titanium alloy/electron beam welding/high cycle fatigue/crack growth rate

引用本文复制引用

基金项目

甘肃省高等教育教学成果培育项目(2021-JXCGPY131)

甘肃省一流本科课程研究项目(2022-XXKC-150)

陇原青年创新创业人才团队项目()

出版年

2024
焊接
机械科学研究院哈尔滨焊接研究所 中国机械工程学会焊接学会

焊接

CSTPCD
影响因子:0.318
ISSN:1001-1382
参考文献量10
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