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2026, 08, v.33 61-69
高频感应加热TB8包边成形工艺
基金项目(Foundation): 国家自然科学基金资助项目(52205326;52375345)
邮箱(Email): donghongrui@nuaa.edu.cn;
DOI:
发布时间: 2026-08-21
出版时间: 2026-08-21
网络发布时间: 2026-08-21
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摘要:

为实现TB8钛合金长包边零件的高效精密成形,提出一种结合预成形与高频感应快速应力松弛的复合成形工艺。通过建立电磁-热-力多场耦合有限元模型,系统模拟了不同感应热源移动速度下的温度分布、应力松弛与回弹行为,并开展了包边试验件成形验证。研究结果表明,随着感应热源移动速度的提高,成形件两侧回弹误差逐渐增大。当移动速度为0.7 mm·s-1时,左右两侧最大回弹误差分别为0.48和0.23 mm,满足零件成形误差±0.5 mm的设计要求,显著提高了成形精度与效率,证实了预成形/高频感应加热复合成形工艺在TB8钛合金包边快速精密成形中的可行性与有效性。

Abstract:

To achieve efficient and precise forming of TB8 titanium alloy long-edge components, a composite forming process combining pre-forming and high-frequency induction rapid stress relaxation was proposed. An electromagnetic-thermal-mechanical multi-fields coupling finite element model was established to systematically simulate the temperature distribution, stress relaxation and rebound behavior with different induction heat source moving speeds. Forming validation was conducted on edge test specimens. The research results indicate that as the induction heat source moving speed increases, the rebound errors on both sides of the formed part gradually increase. When the moving speed is 0.7 mm·s-1, the maximum rebound errors on the left and right sides are 0.48 and 0.23 mm, respectively, meeting the design requirement of ±0.5 mm forming error of components, significantly improving the forming accuracy and efficiency, thereby confirming the feasibility and effectiveness of the combined preforming/high-frequency induction heating process for the rapid and precise forming of TB8 titanium alloy edges.

参考文献

[1] 黄珺,吴明忠,洪海华.钛合金包铁在复合材料桨叶上的应用研究[J].直升机技术,2014,(4):29-34.HUANG Jun,WU Mingzhong,HONG Haihua.Research of titanium alloy leading edge protection on the composite blade [J].Helicopter Technique,2014,(4):29-34.

[2] 陈一哲,付舒程,王辉,等.薄壁双曲率金属包边冲压起皱机理及控制方法[J].塑性工程学报,2022,29(11):42-52.CHEN Yizhe,FU Shucheng,WANG Hui,et al.Wrinkle mechanism and control method of thin-wall bi-curve metal shield in stamping[J].Journal of Plasticity Engineering,2022,29(11):42-52.

[3] 王正峰,李志峰.复合材料桨叶前缘包铁研制及使用现状[J].直升机技术,2018,(2):68-72.WANG Zhengfeng,LI Zhifeng.Development and application actuality of composite material blade leading edge protection[J].Helicopter Technique,2018,(2):68-72.

[4] 周希文.钛合金桨叶前缘包铁精确成形与表面处理工艺研究[D].南京:南京航空航天大学,2014.ZHOU Xiwen.Research on precision forming and surface treatment of titanium leading edge[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2014.

[5] GOLUBEV V I,MEDISON V V,PASTUKHOV D S,et al.Influence of thermal oxidation on the properties of titanium alloys[J].IOP Conference Series:Materials Science and Engineering,2020,966(1):012134.

[6] TANG J J,LIANG C,XU C G,et al.Effect of process parameters on properties of titanium alloy during thermal simulation deformation[J].Advanced Materials Research,2022,1173:101-106.

[7] 王克环,常澍芃,丁锐,等.钛合金薄壁构件快速加热冷模热冲压成形技术进展[J].塑性工程学报,2024,31(1):15-25.WANG Kehuan,CHANG Shupeng,DING Rui,et al.Progress on cold-die hot stamping with rapid heating technology for thin-walled titanium alloy components[J].Journal of Plasticity Engineering,2024,31(1):15-25.

[8] 刘奇,李保永,秦中环,等.TA15钛合金异形曲面钣金件热压成形工艺[J].航天制造技术,2017,(4):6-9.LIU Qi,LI Baoyong,QIN Zhonghuan,et al.Hot-press forming technology of TA15 Titanium alloy profiled surface sheet metal parts[J].Aerospace Manufacturing Technology,2017,(4):6-9.

[9] LI H,CHEN S F,ZHANG S H,et al.Deformation characteristics,formability and springback control of titanium alloy sheet at room temperature:A review[J].Materials,2022,15(16):5586.

[10] 解文龙,马彦,陈帅峰,等.应变速率对钛合金板材室温回弹行为的影响[J].兵器装备工程学报,2023,44(10):52-56.XIE Wenlong,MA Yan,CHEN Shuaifeng,et al.Effect of strain rate on springback behavior of titanium alloy sheet at room temperature[J].Journal of Ordnance Equipment Engineering,2023,44(10):52-56.

[11] FAN R,WU Y,CHEN M,et al.Determining the hot forming limits of titanium alloy sheet under different strain paths by constant equivalent strain rate hot gas bulging tests[J].Journal of Materials Processing Technology,2023,319:118067.

[12] IMRAN S M,LI C,LANG L,et al.An analysis of the hot forming characteristics of diffusion-bonded TC4 alloy using processing maps[J].The International Journal of Advanced Manufacturing Technology,2023,127(7):3239-3253.

[13] 史文祥,章文亮,陈明和,等.TB8钛合金复杂外形桨叶前缘蒙皮多步热成形工艺研究[J].航空制造技术,2021,64(8):84-91.SHI Wenxiang,ZHANG Wenliang,CHEN Minghe,et al.Research on multi-step hot forming process of TB8 titanium alloy leading edge skin of complex shape blade[J].Aeronautical Manufacturing Technology,2021,64(8):84-91.

[14] 牛涛,张艳苓,陈福龙,等.一种直升机桨叶包边成形方法:中国,202110024330.4[P].2021-06-08.

[15] 刘坡,宗影影,郭斌,等.钛合金高温短时蠕变与应力松弛的关系研究[J].材料研究学报,2014,28(5):339-345.LIU Po,ZONG Yingying,GUO Bin,et al.Relation between short-term creep and stress relaxation of titanium alloy at high temperature[J].Chinese Journal of Materials Research,2014,28(5):339-345.

[16] 林遵东,吕枫,韩玉杰,等.TA32钛合金板成形性能与电磁辅助弯曲成形实验研究[J].锻压技术,2021,46(1):104-109.LIN Zundong,LÜ Feng,HAN Yujie,et al.Experimental study on formability and electromagnetic-assisted bending for TA32 titanium alloy sheets[J].Forging & Stamping Technology,2021,46(1):104-109.

[17] 李细锋,陈鑫,朱富慧,等.一种钛合金薄板电辅助分段渐进成形装置及方法:中国,201811561155.7[P].2019-04-16.

[18] 牛涛,张艳苓,陈福龙,等.一种直升机桨叶包边分段分步成形方法:中国,202110024687.2[P].2022-12-16.

[19] WANG H,CHEN M H,XIE L S.Study on stress removal behavior of TB8 titanium alloy by high frequency induction heating.[C]//The 12th International Academic Conference for Graduates.Nanjing,2024:27-32.

[20] 姚红红,邹德宁,周雨晴,等.固溶温度对06Cr25Ni2奥氏体耐热钢微观组织和力学性能的影响[J].上海金属,2017,39(6):22-25.YAO Honghong,ZOU Dening,ZHOU Yuqing,et al.Effect of solution temperature on microstructure and mechanical properties of 06Cr25Ni20 austenitic heat-resistant steel [J].Shanghai Metals,2017,39(6):22-25.

基本信息:

中图分类号:V261;TG306

引用信息:

[1]凌子涵,陈明和,董红瑞,等.高频感应加热TB8包边成形工艺[J].塑性工程学报,2026,33(08):61-69.

基金信息:

国家自然科学基金资助项目(52205326;52375345)

发布时间:

2026-08-21

出版时间:

2026-08-21

网络发布时间:

2026-08-21

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