目的 针对长径比大于10、长度超3 m的D406A超高强度钢细长薄壁壳体整体旋压成形难度大、旋压后产品内部残余应力难以有效去除的问题,对旋压工艺和去应力方法进行研究。方法 首先,根据产品特点制定旋压成形工艺方案,为确定合理的旋压工艺参数,设计不同道次减薄率、进给比、旋压道次的旋压实验,并对每组实验的结果进行分析;其次,根据旋压实验的分析结果,对旋压工艺参数与工装进行优化,并进行了实际生产;最后,为有效去除产品内部残余应力,采取去应力退火方法,分组进行低温退火(300~350 ℃)和高温退火(600~650 ℃)实验,并对退火后的应力与金相组织进行检测。结果 实际生产加工结果满足产品的加工质量与精度要求,同时经高温退火后,产品残余应力消除比较完全,且金相组织无变化,为细小球状珠光体。结论 本文的旋压工艺方法切实可行,所选取的道次减薄率、进给比等旋压参数合理,可为大长径比薄壁壳体旋压成形提供借鉴,且高温退火是消除D406A超高强度钢旋压后产品内部残余应力的有效且合理的方法。
Abstract
To solve the difficulty in the whole spinning forming of D406A with the aspect ratio greater than 10 and the length exceeding 3 m and the removal of the residual stress inside the product after spinning, the work aims to study the spinning process and stress removal method. Firstly, according to the characteristics of the product, the spinning forming process plan was established. In order to determine the reasonable spinning process parameters, the spinning experiments with different thinning rates, feed ratios and spinning passes were designed, and the results of each group of experiments were analyzed. Secondly, according to the analysis results of spinning experiments, the spinning process parameters and tooling were optimized, and the actual production was carried out. Finally, in order to effectively remove the residual stress inside the product, the stress relief annealing method was adopted, and the experiments of low temperature annealing (300-350 ℃) and high temperature annealing (600-650 ℃) were carried out in groups, and the stress and metallographic structure after annealing were measured. The actual production and processing results met the processing quality and precision requirements of the product. At the same time, the residual stress of the product was completely eliminated after high temperature annealing, and the metallographic structure did not change, which was a small spherical pearlite. The spinning process method proposed in this work is feasible, and the selected spinning parameters such as pass thinning rate and feed ratio are reasonable, which can provide reference for the spinning forming of thin-walled shells with large aspect ratio. Moreover, high temperature annealing is an effective and reasonable method to eliminate the internal residual stress of D406A ultra-high strength steel after spinning.
关键词
细长薄壁壳体 /
旋压成形 /
工艺参数 /
去应力 /
高温退火
Key words
slender thin-walled shell /
spinning forming /
process parameter /
stress relieving /
high temperature annealing
{{custom_sec.title}}
{{custom_sec.title}}
{{custom_sec.content}}
参考文献
[1] 王北平, 韩冬, 王兆楠, 等. 细长薄壁发动机金属壳体精密制造技术[J]. 锻压技术, 2022, 47(12): 200-205.
WANG B P, HAN D, WANG Z N, et al.Precision Manufacturing Technology on Slender Thin-Walled Engine Metal Shells[J]. Forging & Stamping Technology, 2022, 47(12): 200-205.
[2] 宿纯文, 王安国, 冯航旗, 等. 基于航空金属部件成型工艺的发展现状[J]. 宇航材料工艺, 2022, 52(5): 21-34.
SU C W, WANG A G, FENG H Q, et al.Development Status of Forming Process Based on Aviation Metal Parts[J]. Aerospace Materials & Technology, 2022, 52(5): 21-34.
[3] 廉国安, 程茜茜, 范国军, 等. 消除某发动机壳体旋压裂纹的工艺改进[J]. 锻压技术, 2022, 47(1): 115-118.
LIAN G A, CHENG X X, FAN G J, et al.Process Improvement on Eliminating Spinning Cracks for a Certain Engine Housing[J]. Forging & Stamping Technology, 2022, 47(1): 115-118.
[4] 刘发美, 金俊松, 李斌, 等. 盘形件两工步对称增厚旋压工艺[J]. 锻压技术, 2023, 48(3): 43-53.
LIU F M, JIN J S, LI B, et al.A Two-Step Symmetrical Thickening Spinning Process for Disk-Shaped Part[J]. Forging & Stamping Technology, 2023, 48(3): 43-53.
[5] 黄艺帆, 董芃欣, 吴泽霖, 等. 高应变速率下TA1纯钛薄板的J-C本构及失效模型研究[J]. 锻压技术, 2023, 48(3): 236-243.
HUANG Y F, DONG P X, WU Z L, et al.Research on J-C Constitutive and Failure Models for TA1 Pure Titanium Sheet under High Strain Rate[J]. Forging & Stamping Technology, 2023, 48(3): 236-243.
[6] WANG S B, XU W C, SHAO B, et al.Process Design and Microstructure-Property Evolution during Shear Spinning of Ti2AlNb-Based Alloy[J]. Journal of Materials Science & Technology, 2022, 101: 1-17.
[7] 李帆, 朱成成, 申宇星, 等. 大型筒体对轮强力施压成形特征与规律研究[J]. 精密成形工程, 2022, 14(7): 11-18.
LI F, ZHU C C, SHEN Y X, et al.Characteristics and Rules of Counter-Roller Flow-Forming of Large Tube[J]. Journal of Netshape Forming Engineering, 2022, 14(7): 11-18.
[8] XUE K M, ZHOU J L, YAN S L, et al.Flow Diversion Mechanisms and Control Methodology in Asymmetric Spinning of Special-Shaped Multi-Wedge Belt Pulley[J]. The International Journal of Advanced Manufacturing Technology, 2022, 119(7): 5289-5302.
[9] 雷煜东, 詹梅, 樊晓光, 等. 带筋薄壁构件成形制造技术的发展与展望[J]. 西北工业大学学报, 2022, 40(1): 1-17.
LEI Y D, ZHAN M, FAN X G, et al.A Review on Manufacturing Technologies of Thin-Walled Components with Ribs[J]. Journal of Northwestern Polytechnical University, 2022, 40(1): 1-17.
[10] YANG Z Z, XU W C, WU H, et al.Enhancing Hoop Strength of Titanium Alloy Tube by Cross Spinning[J]. International Journal of Machine Tools and Manufacture, 2020, 152: 103530.
[11] 周宇, 赵勇, 于忠奇, 等. 交叉内筋薄壁筒体错距旋压成形数值仿真[J]. 上海交通大学学报, 2022, 56(1): 62-69.
ZHOU Y, ZHAO Y, YU Z Q, et al.Numerical Simulation of Stagger Spinning of Cylindrical Part with Cross Inner Ribs[J]. Journal of Shanghai Jiao Tong University, 2022, 56(1): 62-69.
[12] 邵玉林, 刘博, 潘贵平, 等. TA1钛合金药型罩剪切旋压成形塑性变形规律的数值模拟研究[J]. 精密成形工程, 2024, 16(8): 1-10.
SHAO Y L, LIU B, PAN G P, et al.Numerical Simulation of the Plastic Deformation of Conical Shaped Charges with TA1 Titanium Alloy Liner in Shear Spinning Forming[J]. Journal of Netshape Forming Engineering, 2024, 16(8): 1-10.
[13] ZHANG D W, YANG G C, ZHAO S D.Frictional Behavior during Cold Ring Compression Process of Aluminum Alloy 5052[J]. Chinese Journal of Aeronautics, 2021, 34(5): 47-64.
[14] ZHU C C, ZHAO S D, LI S P, et al.Comparison of Mandrel and Counter-Roller Spinning Methods for Manufacturing Large Sheaves[J]. The International Journal of Advanced Manufacturing Technology, 2019, 100(1): 409-419.
[15] ABD-ELTWAB A A, EL-ABDEN S Z, AHMED K I E, et al. An Investigation into Forming Internally-Spline Sleeves by Ball Spinning[J]. International Journal of Mechanical Sciences, 2017, 134: 399-410.
[16] 国家国防科技工业局. 固体火箭发动机用超高强度钢壳体强力旋压工艺通用要求: QJ 20263—2012[S]. 北京: 中国航天标准化研究所, 2013: 1-5.
State Administration of Science, Technology and Industry for National Defence.PRC. General Requirements for Process of Flow-Forming Steel Shell with Superhigh-Strength of Solid Fuel Thruster in Rocket Manufacturing: QJ 20263—2012[S]. Beijing: China Aerospace Standardization Institute, 2023: 1-5.
[17] ZHANG H R, ZHAN M, GUO J, et al.Forming the Transverse Inner Rib of a Curved Generatrix Part through Power Spinning[J]. Advances in Manufacturing, 2019, 7(1): 105-115.
[18] LI F, ZHAO S D, ZHU C C, et al.Influence of Process Parameters on the Forming Results of Large-Sized Cylindrical Parts during Counter-Roller Spinning[J]. Journal of Advanced Mechanical Design, Systems, and Manufacturing, 2022, 16(1): 1-14.
[19] LUO W, CHEN F, XU B B, et al.Study on Compound Spinning Technology of Large Thin-Walled Parts with Ring Inner Ribs and Curvilinear Generatrix[J]. The International Journal of Advanced Manufacturing Technology, 2018, 98(5): 1199-1216.
[20] CUI J H, ZHAO Y X, LI X K, et al.Research on the Influence of Ultrasonic on the Inner Rib’s Surface Morphology of Ribbed Cylindrical Parts in Flow Spinning Process[J]. Journal of Manufacturing Processes, 2021, 67: 376-387.
[21] GUO Y M, LI M Z, WANG D L, et al.Research on the Power Spinning Method of Large High-Strength Cylindrical Parts[J]. The International Journal of Advanced Manufacturing Technology, 2019, 104(1): 1005-1016.
[22] 周大地, 曾卫东, 刘江林, 等. 去应力退火对薄壁钛管表面残余应力的影响[J]. 中国有色金属学报, 2019, 29(7): 1384-1390.
ZHOU D D, ZENG W D, LIU J L, et al.Effect of Stress Relieving Annealing on Surface Residual Stress of Thin-Walled Ti Pipe[J]. The Chinese Journal of Nonferrous Metals, 2019, 29(7): 1384-1390.
[23] 李忻婷, 王猛, 吴军, 等. 超高强度钢35CrMnSiA形变热处理工艺研究[J]. 航天制造技术, 2023(2): 16-20.
LI X T, WANG M, WU J, et al.Study on Thermomechanical Treatment Process of 35CrMnSiA Ultra-High Strength Steel[J]. Aerospace Manufacturing Technology, 2023(2): 16-20.
[24] WU J X, DJAVANROODI F, GODE C, et al.Microstructure Evolution, Texture Development, and Mechanical Properties of Hot-Rolled 5052 Aluminum Alloy Followed by Annealing[J]. Materials Research Express, 2022, 9(5): 056516.
[25] DJEMAOUNE Y, KRSTIC B, RASIC S, et al.Numerical Investigation into In-Plane Crushing of Tube-Reinforced Damaged 5052 Aerospace Grade Aluminum Alloy Honeycomb Panels[J]. Materials, 2021, 14(17): 4992.
[26] 国家质量监督检验检疫总局, 中国国家标准化管理委员会. 无损检测 X射线应力测定方法: GB/T 7704— 2017[S]. 北京: 中国标准出版社, 2017: 1-2.
General Administration of Quality Supervision, Inspection and Quarantine of the People’s Republic of China, Standardization Administration of the People’s Republic of China. Non-Destructive Testing—Practice for Residual Stress Measurement by X-Ray: GB/T 7704— 2017[S]. Beijing: Standards Press of China, 2017: 1-2.