Influence of Welding Sequence on the Distortion of TA15 Titanium Alloy Panel

DONG Wenchao; LU Shanping

doi:10.16080/j.issn1671-833x.2017.04.042

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Influence of Welding Sequence on the Distortion of TA15 Titanium Alloy Panel

更新时间：2025-10-30

- Influence of Welding Sequence on the Distortion of TA15 Titanium Alloy Panel
- Aeronautical Manufacturing Technology Vol. 60, Issue 4, Pages: 42-46(2017)
- 作者机构：
  
  中国科学院金属研究所沈阳材料科学国家（联合）实验室,沈阳,110016
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2017.04.042
  CLC：
- Published：2017
- 稿件说明：
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董文超，陆善平. 焊接顺序对TA15钛合金壁板焊接变形的影响[J]. 航空制造技术, 2017, 60(4): 42-46.

DONG Wenchao, LU Shanping. Influence of Welding Sequence on the Distortion of TA15 Titanium Alloy Panel. Aeronautical Manufacturing Technology, 2017, 60(4): 42-46.
董文超，陆善平. 焊接顺序对TA15钛合金壁板焊接变形的影响[J]. 航空制造技术, 2017, 60(4): 42-46. DOI： 10.16080/j.issn1671-833x.2017.04.042.

DONG Wenchao, LU Shanping. Influence of Welding Sequence on the Distortion of TA15 Titanium Alloy Panel. Aeronautical Manufacturing Technology, 2017, 60(4): 42-46. DOI： 10.16080/j.issn1671-833x.2017.04.042.

摘要

建立了TA15钛合金壁板焊接有限元模型，利用热弹塑性有限元法分析了焊接顺序对壁板变形的影响。通过对比焊缝截面宏观形貌和残余应力，建立了TIG穿透焊焊接工艺的双椭球热源模型，进而模拟了五种焊接顺序下壁板变形情况。结果表明：按从一侧开始的顺序进行焊接时，下壁板中部边缘凸起，变形量较大；采用对称施焊，可有效地控制壁板变形量。

Abstract

A welding finite element model for TA15 titanium alloy panel structure is developed. The influence of welding sequence on the panel distortion is investigated by using thermo-elastic-plastic finite element method. The double ellipsoid heat source models which are suitable for the site TIG penetration welding process are established through comparing the weld cross-section and the residual stress of calculation and experiment. Furthermore

the distortion behaviors of the panel structure in different welding sequences are simulated. The results show that the distortion of the middle part of thin plate is severewhen the welding starts from one side

and the maximum distortion is 3.9mm. The distortion of the thin plates is improved effectively by using the symmetrical welding sequence.

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