金属热处理 ›› 2025, Vol. 50 ›› Issue (10): 252-255.DOI: 10.13251/j.issn.0254-6051.2025.10.041

• 工艺研究 • 上一篇    下一篇

去应力退火对Ti-4Al-5Mo-5V-6Cr-1Nb钛合金力学性能和残余应力的影响

胡生双1, 史利利1, 赵虎1, 杜垚鑫1, 张颖云1, 徐勇2   

  1. 1.中航西安飞机工业集团股份有限公司, 陕西 西安 710089;
    2.南昌航空大学 民航学院, 江西 南昌 330063
  • 收稿日期:2025-04-21 修回日期:2025-08-13 出版日期:2025-10-25 发布日期:2025-11-04
  • 通讯作者: 徐 勇,E-mail: xuyong@nchu.edu.cn
  • 作者简介:胡生双(1989—),男,高级工程师,主要研究方向为钛合金和铝合金工艺,E-mail: hushengshuang2000@163.com。
  • 基金资助:
    国家重点研发计划(ZX20210486);国家自然科学基金(52174308)

Effect of stress relief annealing on mechanical properties and residual stress of Ti-4Al-5Mo-5V-6Cr-1Nb titanium alloy

Hu Shengshuang1, Shi Lili1, Zhao Hu1, Du Yaoxin1, Zhang Yingyun1, Xu Yong2   

  1. 1. Avic Xi'an Aircraft Industry Group Co., Ltd., Xi'an Shaanxi 710089, China;
    2. Civil Aviation Academy, Nanchang Hangkong University, Nanchang Jiangxi 330063, China
  • Received:2025-04-21 Revised:2025-08-13 Online:2025-10-25 Published:2025-11-04

摘要: 研究了480和500 ℃去应力退火对Ti-4Al-5Mo-5V-6Cr-1Nb钛合金力学性能、残余应力及微观组织的影响规律。结果表明,去应力退火对强度影响较小,去应力退火后抗拉强度保持在1310 MPa左右,屈服强度保持在1250 MPa左右。较未退火,480 ℃去应力退火后断面收缩率降低17.8%,断裂韧度降低8.8%。去应力退火温度升高至500 ℃时,断面收缩率和断裂韧度与未经去应力退火时基本保持一致。去应力退火后的显微组织变化不大,晶界α相平直,晶内α相呈交织网状分布。去应力退火前后合金的拉伸断裂机制均为韧窝和准解理的混合断裂机制,480 ℃应力退火时的纤维区明显比未经去应力退火和500 ℃去应力退火的纤维区面积小。500 ℃×1 h去应力退火可基本消除合金残余应力。综合考虑残余应力、强度、塑性和断裂韧度,应选500 ℃×1 h去应力退火工艺为宜。

关键词: 去应力退火, 钛合金, 力学性能, 显微组织, 残余应力

Abstract: Effect of stress relief annealing at 480 ℃ and 500 ℃ on mechanical properties, residual stress and microstructure of Ti-4Al-5Mo-5V-6Cr-1Nb titanium alloy was investigated. The results show that stress relief annealing has a relatively small effect on strength. After stress relief annealing, the tensile strength remains around 1310 MPa and the yield strength remains around 1250 MPa. After stress relief annealing at 480 ℃, the percentage reduction of area is reduced by 17.8% and the fracture toughness is reduced by 8.8%. When the stress relief annealing temperature increases to 500 ℃, the percentage reduction of area and fracture toughness are basically the same as those without stress relief annealing. The microstructure changes a little after stress relief annealing, with straight α phases at grain boundaries and interlaced network distribution of α phases within the grains. The tensile fracture mechanism of the alloy before and after stress relief annealing is a mixed fracture mechanism of ductile dimples and quasi cleavage. The fiber zone area after stress relief annealing at 480 ℃ is significantly smaller than that without stress relief annealing and at 500 ℃. Stress relief annealing at 500 ℃ for 1 h can effectively eliminate residual stress of the alloy. Considering the comprehensive residual stress, strength, plasticity, and fracture toughness, the stress relief annealing process at 500 ℃ for 1 h should be selected.

Key words: stress relief annealing, titanium alloy, mechanical properties, microstructure, residual stress

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