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商用飞机复合材料双面加筋壁板制造技术研究 被引量:3

Study on Manufacturing Technology of Double-sided Stiffened Panel of Commercial Aircraft
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摘要 本文以层间增韧环氧树脂碳纤维单向带及织物预浸料为原料,采用手工铺叠的方式制造双面加筋壁板,首先利用热压罐共固化蒙皮及单面长桁,然后采用胶接共固化的方式制造双面加筋壁板,通过利用成型模工装上的凹槽限制筋条轴线位置,解决了壁板轴线偏移问题,将轴线精度由以往的±2mm提升至±0.3mm;通过采用金属工装及筒状真空袋的组合成型方式,解决了传统金属工装传压不均的问题,有效提升了零件的固化质量;通过开发一种特殊形状的特氟龙斜块解决了该类形式工装的零件脱模难题。最终制造出相关性能指标优于现行技术要求的合格零件,该零件的制造过程及检测指标符合设计的意图,零件的外形尺寸及轴线精度能够满足装配的需求。 The paper uses interlaminar toughened epoxy preimpregnated carbon fiber tapes and fabrics as raw material. The double-sided stiffened panel is manufactured by manual lay-up. Firstly, autoclave is used to co-cure skin and one side stringers. Then co-bonding the part with another side stringers to form a final double-sided stiffened panel. By limiting the position of the stringers with molding tool, the problem of the axis deviation of the panel is solved. Axis accuracy has been improved from ±2 mm to ±0.3 mm;By adopting the combination of metal tooling and cylinder vacuum bag, the problem of uneven transfer pressure of metal tooling is solved, and the curing quality of parts is effectively improved;By developing a special shaped Teflon inclined block, the demoulding problem of this kind of tooling and parts is solved. Finally, the relevant performance indicators are better than the current technical requirements of qualified part. The manufacturing process and testing index of part is in line with the design intention, and the dimensions and axis precision of the part can meet the requirements of the assembly.
作者 叶真铭 王韬 马刚 李景钰 YE Zhenming;WANG Tao;MA Gang;LI Jingyu(AVIC Shenyang Aircraft Industry(Group)Co.,Ltd.,Shenyang 110850)
出处 《纤维复合材料》 CAS 2021年第3期18-22,27,共6页 Fiber Composites
关键词 复合材料 加筋壁板 共固化 胶接共固化 composite stiffened panel co-curing co-bonding
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  • 1谢灿军,童明波,刘富,岳广全,刘艳.GLARE平板抗鸟撞数值模拟[J].复合材料学报,2013,30(S1):212-218. 被引量:3
  • 2杜善义.先进复合材料与航空航天[J].复合材料学报,2007,24(1):1-12. 被引量:1022
  • 3刘代军 陈亚莉.先进树脂基复合材料在航空工业中的应用.材料工程,2008,:195-195.
  • 4张纪奎,郦正能,程小全,王军.复合材料整体结构在大型民机上的应用[J].航空制造技术,2007,0(9):38-38. 被引量:22
  • 5Wilkinsin S P. Reactive blends of anaorphous functionalized engineering thermoplastics and bismaleimide/diallyl bisphenol A resins for high performance composite matrices[C]//lnternational SAMPE Symposium. ,:an Diego: SAMPE, 1991, 36: 482-495.
  • 6Steiner P A, Browne J M. Development of failure resistant bismaleimide/carbon composite [J]. SAMPE J, 1987 (3/4) : 8- 14.
  • 7Cheng Qunfeng, Fang Zhengping, Yi Xiaosu. Ex-situ concept for toughening the RTMable BMI matrix composite. Part I.Improving the interlaminar fracture toughenss[J]. Joural of Applied Polymer Science, 2008, 109; 1625-1634,.
  • 8Cheng Qunfeng, Fang Zhengping, Yi Xiaosu, Ex-situ concept for toughening the RTMable BMI matrix composite, lI, Improving the compression after impact [J]. Journal of Applied Polymer Science, 2008, 108: 2211-2217.
  • 9邢丽英,李斌太.一种树脂基复合材料层间增韧方法:中国,200810075870.X[P].2008-06-27.
  • 10Ruud N. Rapid tooling for Resin Transfer Moulding, RTM [C]//Proceedings of the Sixth International Conference on Rapid Prototyping. Dayton, OH: Rapid Prototyping Journal, 1995: 205-215.

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