YANG Sanqiang, WANG Lei, LI Maowei, GAO Zhanjiao, HAN Jianchao, QI Junfeng. Study on Residual Stress Relief and Shape Accuracy Retention of Titanium Alloy Parts[J]. Development and Application of Materials, 2024, 39(4): 76-82.
Citation: YANG Sanqiang, WANG Lei, LI Maowei, GAO Zhanjiao, HAN Jianchao, QI Junfeng. Study on Residual Stress Relief and Shape Accuracy Retention of Titanium Alloy Parts[J]. Development and Application of Materials, 2024, 39(4): 76-82.

Study on Residual Stress Relief and Shape Accuracy Retention of Titanium Alloy Parts

More Information
  • Received Date: September 01, 2023
  • Available Online: September 11, 2024
  • Residual stress relief tests are carried out on typical TC4 R state titanium alloy commonly used in spacecraft structural products by vacuum stress relief annealing, cryogenic treatment, and high and low temperature cyclic heat treatment. X-ray diffraction method is used to measure residual stress in the specimens, and the average residual stress relief rates inside and in the surface of the treated specimens are calculated. Finally, the shape accuracies of the treated specimens are tested, and the effectiveness of various heat treatment methods in maintaining shape accuracy is verified. The results show that the vacuum stress relief annealing is the most effective, followed by cryogenic treatment, and that the effectiveness of high and low temperature cyclic heat treatment is the lowest. The average residual stress relief rate is strongly positively correlated with the shape accuracy retention. Of all the specimens treated by different methods, the average residual stress relief rates in the internal/surface of specimens treated with the combination of vacuum stress relief annealing, cryogenic treatment, and high and low temperature cycle heat treatment in queue are the highest, and their shape accuracy retention the best, those of the specimens treated with cryogenic treatment and high and low temperature cycle heat treatment come in second, and those of the specimens only treated with high and low temperature cyclic heat treatment rank last.
  • [1]
    马聪.火星探测遥感相机支撑结构设计[D].长春:中国科学院大学(中国科学院长春光学精密机械与物理研究所), 2018.
    [2]
    祁俊峰,季禹曈,张天驰,等.面向航天器多分支钛合金支承结构的SLM成型工艺[J].新技术新工艺, 2018(6):1-5.
    [3]
    吴宏宇,王春洁,丁宗茂,等.着陆姿态不确定下的着陆器缓冲机构优化设计[J].宇航学报, 2018, 39(12):1323-1331.
    [4]
    姜建堂,孟金奎,董亚波,等.大型复杂构件制造过程残余应力演化与调控[J].宇航学报, 2020, 41(6):676-685.
    [5]
    米谷茂.残余应力的产生和对策[M].朱荆璞,邵会孟,译.北京:机械工业出版社, 1983.
    [6]
    何伟,杜小平,马红征,等. TC4钛合金相变温度的测定与分析[J].理化检验(物理分册), 2014, 50(7):461-464.
    [7]
    黎文献,龚浩然,柏振海,等.金属材料的深冷处理[J].材料导报, 2000, 14(3):16-18.
    [8]
    康超,曾卫东,张尧武,等.真空去应力退火对TC21钛合金残余应力的影响[J].热加工工艺, 2011, 40(16):154-156.
  • Related Articles

    [1]SUN Jianjun, WANG Desheng, WANG Pengyun. Effect of Heat Treatment on Microstructure and Properties of AlZn4SiPb Alloy[J]. Development and Application of Materials, 2022, 37(5): 22-27.
    [2]WANG Renfu, YAO Zhiying, DENG Wanping, NIU Jicheng, YE Fan. Research Progress on Stress Reduction Heat Treatment of Low Alloy Steel[J]. Development and Application of Materials, 2021, 36(3): 86-94.
    [3]XIE Bin, ZHOU Haitao, DUAN Haiyang. Effect of Heat Treatment Process on Particle Size and Uniformity of SnO2 Atomized Powder[J]. Development and Application of Materials, 2021, 36(3): 7-11.
    [4]DENG Wanping, NIU Jicheng, WANG Renfu. Effect of Stress Relieving Heat Treatment on Microstructure and Properties of 10CrNi5MoV Steel after Plastic Deformation[J]. Development and Application of Materials, 2019, 34(3): 46-51,62. DOI: 10.19515/j.cnki.1003-1545.2019.03.008
    [5]WANG Peng, LÜ Jialong, LI Zhihao, HU Changfei, WANG Bing. Experimental Study on Nondestructive Examination for Metal Enhanced Rubber Composite[J]. Development and Application of Materials, 2018, 33(3): 56-61. DOI: 10.19515/j.cnki.1003-1545.2018.03.009
    [6]SUN Lin-lin, LI Hong, ZHOU Hong-tao, ZHANG Lei, LENG Ai-ping. XRF Test Method for Elements Analysis of Middle-low Alloy Steel[J]. Development and Application of Materials, 2015, 30(6): 86-89. DOI: 10.19515/j.cnki.1003-1545.2015.06.017
    [7]ZHAO Rong-bing. Application of X-ray Diffraction Peak Separation Technology on Field HeatTreatment Two-phase Analysis of Ferromagnetic NiMnGa Intelligent Alloy[J]. Development and Application of Materials, 2012, 27(2): 18-23,27. DOI: 10.19515/j.cnki.1003-1545.2012.02.005
    [8]DAI Li-ping, PENG Qiao. Preparation of the Ru15Ir15SnxTi70-x/Ti Anode by Sol-gel Process and Performance Investigation[J]. Development and Application of Materials, 2008, 23(4): 27-31,36. DOI: 10.19515/j.cnki.1003-1545.2008.04.008
    [9]XIE Qing-feng, LI Hao, GAO Yan. Influence of Heat Treatment on Phase Transformation of NiTi Shape Memory Alloys[J]. Development and Application of Materials, 2007, 22(2): 5-7. DOI: 10.19515/j.cnki.1003-1545.2007.02.002
    [10]FU Hao, GU Shu-yan, YAN Guo-qiang. Study on the Welding Procedure of Butt Joint of 10CrNi3MoV/BFe30-1-1 Clad Plate Elbow[J]. Development and Application of Materials, 2004, 19(5): 33-36. DOI: 10.19515/j.cnki.1003-1545.2004.05.009

Catalog

    Article Metrics

    Article views (97) PDF downloads (21) Cited by()
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return