Home
Editorial Committee
Brief Instruction
Back Issues
Instruction to Authors
Submission on line
Contact Us
Chinese

  The journal resolutely  resists all academic misconduct, once found, the paper will be withdrawn immediately.

Title:Parameter optimization on aero-engine blade rolling process based on finite element simulation
Authors: Wang Guodong1  Wang Hongyu1  Jiang Lei1 Teng Fei1  Sun Juncai1  Kong Xiangwei2 
Unit: 1. School of Transportation Engineering  Dalian Maritime University 2.School of Mechanical Engineering Automation  Northeastern University 
KeyWords: precision rolling  blade  rolling reduction amount  friction factor rolling force 
ClassificationCode:
year,vol(issue):pagenumber:2022,47(3):109-115
Abstract:

 Precision rolling is an important processing method for aero-engine blades, and it is difficult to determine its process parameters, resulting in controlling the blade forming effect difficultly. Therefore, it was proposed to use finite element simulation software ABAQUS to simulate the rolling process, and by changing rolling reduction amount and friction factor, the coupling influence of the rolling reduction amount and the friction factor on the forming result for blade was studied. Furthermore, the process parameters were optimized, and the optimal parameter settings were obtained. The research results show that with the increasing of the friction factor, the overall blade width of the rolling model increases, and the rolling force is linear positive correlation with the friction factor. With the increasing of the reduction amount in port, the rolling force on the blade and the blade width increase, but when the reduction amount exceeds 0.06 mm, the rolling force and the blade width increase suddenly, and the blade deformation is concentrated in the local area of edge, which is not conducive to the precise control of the forming result.

Funds:
国家自然科学基金资助项目(51905068);辽宁省博士启动基金资助项目(20180540098);辽宁省自然科学基金资助项目(2020-HYLH-24);东北大学重点实验室开放课题基金资助项目(2020RALKFKT012)
AuthorIntro:
王国栋(1995-),男,硕士研究生 E-mail:1026112215@qq.com 通信作者:王鸿雨(1989-),男,博士,副教授 E-mail:wanghongyu@dlmu.edu.cn
Reference:

 [1]刘维伟, 张定华,史耀耀,.航空发动机薄壁叶片精密数控加工技术研究[J].机械科学与技术, 2004, 23(3):329-331.


 


Liu W W, Zhang D H, Shi Y Y, et al. Research on precision cnc machining technology of thin-walled aeroengine blades [J]. Mechanical Science and Technology for Aerospace Engineering, 2004 23 (3): 329-331.


 


[2]李深亮, 乔思佳, 姜绍西 .航空发动机叶段类静子辊轧叶片加工工艺[J].航空制造技术, 2018, 61(15):40-47.


 


Li S L, Qiao S J, Jiang S X. Processing technology of stator rolling blade for aeroengine blade segment [J]. Aeronautical Manufacturing Technology, 2018, 61 (15): 40-47.


 


[3]毛君, 孟辉,陈洪月,.航空发动机叶片热轧与冷轧过程对比分析与研究[J].热加工工艺,2013,42(13):84-86,91.


 


Mao J, Meng H, Chen H Y, et al. Comparative analysis and research on hot rolling and cold rolling process of aeroengine blade [J]. Hot Working Technology, 2013,42 (13): 84-86, 91.


 


[4]邰清安, 李治华, 孙立群, .航空发动机塑性成形技术的应用与展望[J].航空制造技术, 2014, 451(7):34-39.


 


Tai Q A, Li Z H, Sun L Q, et al. Application and prospect of aeroengine plastic forming technology [J]. Aeronautical Manufacturing Technology, 2014, 451 (7): 34-39.


 


[5]霍晓佩. 高温合金叶片辊轧成形数值模拟及边部损伤研究[D].沈阳:东北大学, 2015.


 


Huo X P. Numerical Simulation and Edge Damage Research of Superalloy Blade Roll Forming [D]. Shenyang: Northeast University, 2015.


 


[6]于建民, 张治民, 李国俊.叶片辊轧工艺数值模拟研究[J].弹箭与制导学报, 2006, 26(1):833-835.


 


Yu J M, Zhang Z M, Li G J. Numerical simulation of blade rolling process[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2006, 26 (1): 833-835.


 


[7]毛君, 曹治, 董晓彤.叶片辊轧过程中变形的影响因素[J].科技导报, 2014, 32(7):56-61.


 


Mao J, Cao Z, Dong X T. Influencing factors of blade deformation during rolling [J]. Science & Technology Review, 2014, 32 (7): 56-61.


 


[8]靳淇超, 汪文虎,蒋睿嵩,.压气机叶片辊轧模具型腔回弹补偿方法研究[J].机械工程学报,2017,53(16):148-155.


 


 Jin Q C, Wang W H, Jiang R S, et al. Research on springback compensation method of compressor blade rolling die cavity[J]. Journal of Mechanical Engineering, 2017,53 (16): 148-155.


 


[9]靳淇超, 汪文虎,蒋睿嵩,.一种改进的压气机叶片辊轧成型前滑计算模型[J].航空学报,2016,37(10):3178-3185.


 


 Jin Q C, Wang W H, Jiang R S, et al. An improved forward slip calculation model for compressor blade roll forming[J]. Acta Aeronautica et Astronautica Sinica, 2016,37 (10): 3178-3185.


 


[10]王渊彬, 汪文虎,张艳,.压气机叶片辊轧模具型腔快速建模技术[J].航空学报,2014,35(11):3190-3198.


 


Wang Y B, Wang W H, Zhang Y, et al. Rapid modeling technology of compressor blade rolling die cavity [J]. Acta Aeronautica et Astronautica Sinica, 2014,35 (11): 3190-3198.


 


[11]王玮, 耿文冉, 孔祥伟.航空发动机叶片冷辊轧过程本构模型[J].机械设计与制造, 2018, 328(6):5-8.


 


Wang W, Geng W R, Kong X W. Constitutive model of aeroengine blade cold rolling process [J]. Machinery Design & Manufacture, 2018, 328 (6): 5-8.


 


[12]金加奇, 周道.GH4169叶片冷辊轧成形过程数值模拟分析[J].机械设计与制造, 2019, 338(4):204-206.


 


Jin J Q, Zhou D. Numerical simulation analysis of GH4169 blade cold roll forming process [J]. Machinery Design & Manufacture, 2019, 338 (4): 204-206.


 


[13]Kong X W, Li J, Li B. Finite element analysis of rolling process for variable cross-section blade[J].Journal of Central South University, 2013, 20(12):3431-3436.


 


[14]Jiang Z Y, Du X Z, Du Y B, et al. Strip shape analysis of asymmetrical cold rolling of thin strip[J].Advanced Materials Research, 2010, 97-101:81-84.


 


[15]Ye N Y, Cheng M, Zhang S H. Effect of cold rolling parameters on the longitudinal residual stress distribution of GH4169 alloy sheet[J]. Acta Metallurgica Sinica: English Letters, 2015, 28(12):1510-1517.


 


[16]Kong X W, Wang H Y, Jiang L, et al. Research on rolling force and stress during rolling process of blade with complex surface based on multi-plane slab method[J].Journal of the Brazilian Society of Mechanical Sciences and Engineering, 2020, 42(8):1-12.


 

Service:
This site has not yet opened Download Service】【Add Favorite
Copyright Forging & Stamping Technology.All rights reserved
 Sponsored by: Beijing Research Institute of Mechanical and Electrical Technology; Society for Technology of Plasticity, CMES
Tel: +86-010-62920652 +86-010-82415085     Fax:+86-010-62920652
Address: No.18 Xueqing Road, Beijing 100083, P. R. China
 E-mail: fst@263.net    dyjsgg@163.com