[1]崔静. 钣金零件的坯料展开与回弹算法研究[D].南京:南京航空航天大学,2016.
Cui J. Research on the Algorithms of Blank Unfolding and Spring-back Simulation for Sheet Metal Parts[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2016.
[2]胡丹. 飞机钛合金钣金件橡皮囊精确成形技术研究[D]. 南京:南京航空航天大学,2014.
Hu D. Precision Forming Technology Research on Rubber Bladder Forming of Aircraft Titanium Alloy Sheet Metal[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2014.
[3]李文平. 弯曲回弹变分原理及其数值模拟研究[D].河北:燕山大学,2006.
Li W P. Study on Variational Principles of Springback for Bending and Its Numerical Simulation[D]. Hebei: Yanshan University, 2006.
[4]杨忆湄, 王俊彪,刘闯,等.框肋零件弯边回弹补偿系统的开发与应用[J].锻压装备与制造技术,2013,48(5):68-71.
Yang Y M, Wang J B, Liu C, et al.Development and application of flange springback compensation system for frame and rib parts[J].China Metal Forming Equipment & Manufacturing Technology,2013,48(5):68-71.
[5]陈磊, 邱晞,李善良,等.橡皮液压成形直弯边回弹试验与分析研究[J].塑性工程学报,2008,15(3):47-50,60.
[5]Chen L, Qiu X, Li S L,et al. Analysis and experiment study on springback of straight flanging in rubber fluid forming [J]. Journal of Plastic Engineering,2008,15 (3):47-50,60.
[6]聂昕. 汽车板件回弹相关问题的研究[D].长沙:湖南大学,2008.
Nie X. Key Teehniques Study of Automobile Pane′s Springback. [D].Changsha: Hunan University, 2008.
[7]张建明. 翼肋零件橡皮囊液压成形模具型面设计系统的研究[D].南京:南京航空航天大学,2011.
Zhang J M. Research on Die-face Design System for Rubber Bladder Hydroforming of the Rib[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2011.
[8]付云方. 橡皮囊成形弯曲回弹的研究[D].南京:南京航空航天大学,2009.
Fu Y F. A Research on the Springback of Bending on Rubber Bladder Foring[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009.
[9]Subhrangshu D. The Effect of Forming Pressure on Springback in 2024 Aluminum Alloys[R]. Reno,Nevada:World Aviation Congress, 2004.
[10]张凌云, 周帅,陈瑶,等.基于补偿因子的直弯边下陷零件回弹补偿研究[J].材料科学与工艺,2018,26(4):28-33.
Zhang L Y,Zhou S,Chen Y,et al. Research on springback compensation for straight flanging jogged partbased on compensation factors[J].Materials Science and Technology,2018,26(4):28-33.
[11]HB 6470—90,飞机钣金件尺寸公差及技术条件[S].
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