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阶梯钻钻削CFRP锥形沉头孔实验研究 被引量:1

Experimental Study on Stepped Drilling Tapered Countersunk Hole Of CFRP
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摘要 碳纤维增强复合材料(CFRP)被广泛应用于航空航天、轨道交通等领域。CFRP零件经常通过螺栓与其它零件联接,但是由于CFRP层间强度低,在钻孔过程中容易产生分层、纤维拉出、基体损伤等缺陷。对于锥形沉头孔来说,其锥面加工质量更难保证。文章建立了锥形沉头孔的加工数学模型,研究了沉头锥面缺陷的形成机理;通过实验研究了CFRP锥形沉头孔的加工质量,分析了加工过程中的轴向力、温度的变化规律;采用扫描电镜分析了锥形沉头的孔壁表面特征。结果表明,在沉头锥面上CFRP在层间发生了严重的分层现象,在层内发生了明显的块状断裂,在孔壁锥面和直面过渡区发生了纤维撕裂。通过研究发现,通过改变主轴转速可以提高锥面和过渡区的加工质量。 CFRP is widely used in aerospace,rail transportation and other fields.CFRP parts are often connected to other parts by bolts,but due to the low interlayer strength of CFRP,defects such as delamination,fiber pullout,and matrix damage are prone to occur during the drilling process.For tapered countersunk holes,the machining quality of the tapered surface is more difficult to guarantee.In this paper,a mathematical model for machining the countersink hole is established,and the formation mechanism of the countersunk cone defect is studied.The machining quality of the tapered countersink hole of CFRP was studied experimentally,and the changes of the axial force and temperature during processing were analyzed.The surface characteristics of the hole wall of the tapered countersink were analyzed by sem.The results showed that the CFRP had severe delamination between the layers on the countersunk cone surface,obvious block fractures occurred in the layer,and fiber tearing occurred in the transition zone between the cone wall and the straight surface of the hole wall.It is found through research that the machining quality of the taper surface and the transition zone can be improved by changing the spindle speed.
作者 刘坤祥 高延峰 LIU Kun-xiang;GAO Yan-feng(School of Aeronautic Manufacturing Engineering,Nanchang Hangkong University,Nanchang 330063,China)
出处 《组合机床与自动化加工技术》 北大核心 2020年第11期166-170,174,共6页 Modular Machine Tool & Automatic Manufacturing Technique
基金 航空科学基金项目(2018ZE56013) 江西省自然科学基金项目(20171BAB206033) 江西省重点研发计划项目(20171BBE50011)。
关键词 数学模型 CFRP 沉头孔 加工质量 mathematical model CFRP countersunk hole machining quality
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  • 1张厚江,陈五一,陈鼎昌.碳纤维复合材料(CFRP)钻孔出口缺陷的研究[J].机械工程学报,2004,40(7):150-155. 被引量:83
  • 2姜云鹏,张庆茂,王毅,岳珠峰.复合材料层合板开口翻边补强试验和数值研究[J].复合材料学报,2005,22(5):190-196. 被引量:15
  • 3邹方,薛汉杰,周万勇,许国康.飞机数字化柔性装配关键技术及其发展[J].航空制造技术,2006,49(9):30-35. 被引量:60
  • 4ZOU Z, REID S R, LI S, et al. Application of a delamination model to laminated composite structures[J]. Composite Structures, 2002, 56(4): 375-389.
  • 5TSAO C C, CHENG H H. The effect of chisel length and associated pilot hole on delamination when drilling composite materials[J]. International Journal of Machine Tools & Manufacture, 2003, 43(11): 1087-1092.
  • 6LASRI L, NOUARI M, MANSORI M E. Modelling of chip separation in machining unidirectional FRP composites by stiffness degradation concept[J]. Composites Science and Technology, 2009, 69(5). 684-692.
  • 7DAVIM J P, REIS P. Study of delamination in drilling carbon fiber reinforced plastics (CFRP) using design experiments[J]. Composite Structures, 2003, 59(4): 481-487.
  • 8CANTWELL W J, MORTON J. The significance of damage and defects and their detection in composite materials: A review[J]. Journal of Strain Analysis, 1992, 27(1): 29-42.
  • 9KESSLER M R, SOTTOS N R, WHITE S R. Self-healing structural composite materials[J]. Composites: Part A, 2003, 34(8): 743-753.
  • 10PERSSON E, ERIKSSON I, ZACKRISSON L. Effects of hole machining defects on strength and fatigue life of composite laminates[J]. Composites: PartA, 1997, 28(2): 141-151.

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