大尺寸复合材料翼梁数字化设计/制造技术
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摘要
翼梁尺寸大、受力复杂,是飞机的主承力结构。采用复合材料制造翼梁可达到减重、提高起重载荷并延长使用寿命的目的。为了有效承载、传载及工艺装配的需求,要求复合材料翼梁结构铺层位置、铺贴角度精准,外形公差控制严格。大尺寸的复合材料翼梁铺层复杂、截面变化多,传统的手工方法制造大尺寸复合材料零件经常会出现零件内部质量问题及质量稳定性差等状况,这就需要更高的制造工艺水平来满足工程需要。从设计到制造应用数字化技术,材料自动铺贴、裁剪、成型,可以高质量地成型复合材料翼梁,满足设计各项指标要求。
Wing spar is the major load-carrying structure with large dimension and complex stress. Composite wing spar features weight reduction, load-carrying increase and long service life. To achieve the effective load carrying and transfer, and satisfy process coordination, composite wing spars are required to have accurate lay-up position and angle, and strictly controlled profile tolerance. However, due to complex lay-up and various sections of large composite wing spar, the traditional manual process of large composite components frequently brings about quality issues in the internal and unstable quality, which requires higher level of manufacturing process so as to satisfy engineering requirements. The digital technology adopted from design to manufacturing, and the automatic lay-up, cutting and forming of materials will contribute to the high quality forming of composite wing spar so as to satisfy all engineering requirements.
Wing spar is the major load-carrying structure with large dimension and complex stress. Composite wing spar features weight reduction, load-carrying increase and long service life. To achieve the effective load carrying and transfer, and satisfy process coordination, composite wing spars are required to have accurate lay-up position and angle, and strictly controlled profile tolerance. However, due to complex lay-up and various sections of large composite wing spar, the traditional manual process of large composite components frequently brings about quality issues in the internal and unstable quality, which requires higher level of manufacturing process so as to satisfy engineering requirements. The digital technology adopted from design to manufacturing, and the automatic lay-up, cutting and forming of materials will contribute to the high quality forming of composite wing spar so as to satisfy all engineering requirements.
引文
[1]燕瑛,王正龙,刘秀芝.复合材料结构数字化设计与工艺制造一体化技术研究及应用[J].航空制造技术,2007,50(8):46-48.YAN Ying,WANG Zhenglong,LIUXiuzhi.Research and application of design for manufacturing for composite structure[J].Aeronautical Manufacturing Technology,2007,50(8):46-48.
[2]王咏梅.浅谈国内复合材料设计制造一体化技术[J].航空制造技术,2012,55(18):49-52.WANG Yongmei.Integration technology of domestic composites design and manufacturing[J].Aeronautical Manufacturing Technology,2012,55(18):49-52.
[3]冯雁,郑锡涛,吴淑一,等.轻型复合材料机翼铺层优化设计与分析[J].航空学报,2015,36(6):1858-1866.FENG Yan,ZHENG Xitao,WU Shuyi,et al.Layup optimization design and analysis of super lightweight composite wing[J].Acta Aeronautica et Astronautica Sinica,2015,36(6):1858-1866.
[4]方宜武,王显峰,孙成,等.复合材料机翼翼梁的制造及应用概况[J].玻璃钢/复合材料,2014(2):16-22.FANG Yiwu,WANG Xianfeng,SUNCheng,et al.The manufacture and application of composite wing spars[J].Fiber Reinforced Plastics/Composites,2014(2):16-22.
[5]陈际伟,赵艳文,翟全胜.复合材料壁板的数字化成型研究[J].高科技纤维与应用,2015,40(6):56-58.CHEN Jiwei,ZHAO Yanwen,ZHAIQuansheng.Study on digital molding method of composite panels[J].Hi-Tech Fiber&Application,2015,40(6):56-58.
[6]徐福泉,高大伟,杨楠楠.复合材料自动铺带技术应用及方案示例[J].航空制造技术,2009,52(22):51-54.XU Fuquan,GAO Dawei,YANGNannan.Application and proposal sample of composite automatic tape-laying technology[J].Aeronautical Manufacturing Technology,2009,52(22):51-54.
[7]王天玉,梁宪珠,杨进军.飞机复合材料构件自动铺带/丝束铺放典型设备[J].航空制造技术,2008,51(4):40-44.WANG Tianyu,LIANG Xianzhu,YANGJinjun.ATL/AFP typical equipments of aircraft composite parts[J].Aeronautical Manufacturing Technology,2008,51(4):40-44.
[8]王菲,杨博,陈永清,等.大尺寸复合材料翼梁的研制[J].航空制造技术,2015,58(S1):55-57.WANG Fei,YANG Bo,CHEN Yongqing,et al.Manufacturing of large scale composites spar[J].Aeronautical Manufacturing Technology,2015,58(S1):55-57.
[9]唐珊珊.复合材料数字化制造技术在壁板上的应用[J].金属加工,2010(S):112-113.TANG Shanahan.Application of digital manufacturing technology of the composite panels[J].Metal Working,2010(S):112-113.
[10]梁禄忠,李延征.大型复合材料壁板成型技术[J].航空制造技术,2012,55(23/24):62-66.LIANG Luzhong,LI Yanzheng.Molding technology of large scale composites panle[J].Aeronautical Manufacturing Technology,2012,55(23/24):62-66.
[11]郝建伟,陈亚莉.先进复合材料主要制造工艺和专用设备[J].航空制造技术,2008,51(10):42-44.HAO Jianwei,CHEN Yali.Manufacturing technology and special equipment for advanced composites[J].Aeronautical Manufacturing Technology,2008,51(10):42-44.
[12]黄莹.复合材料热隔膜预成型工艺分析[J].机械设计与制造工程,2015,44:20-22.HUANG Ying.The analysis on the hot diaphragm preforming process for composite material[J].Machine Design and Manufacturing Engineering,2015,44:20-22.
[13]蒲永伟,刘沛禹,刘智.大尺寸工字型复合材料长桁整体成型工艺研究[C]//第17届全国复合材料学术会议.北京,2012.PU Yongwei,LIU Peiyu,LIU Zhi.Study of integral manufacture technology for large composite stringers[C]//Proceedings of the Seventeenth National Conference on Composite Materials.Beijing,2012.
[2]王咏梅.浅谈国内复合材料设计制造一体化技术[J].航空制造技术,2012,55(18):49-52.WANG Yongmei.Integration technology of domestic composites design and manufacturing[J].Aeronautical Manufacturing Technology,2012,55(18):49-52.
[3]冯雁,郑锡涛,吴淑一,等.轻型复合材料机翼铺层优化设计与分析[J].航空学报,2015,36(6):1858-1866.FENG Yan,ZHENG Xitao,WU Shuyi,et al.Layup optimization design and analysis of super lightweight composite wing[J].Acta Aeronautica et Astronautica Sinica,2015,36(6):1858-1866.
[4]方宜武,王显峰,孙成,等.复合材料机翼翼梁的制造及应用概况[J].玻璃钢/复合材料,2014(2):16-22.FANG Yiwu,WANG Xianfeng,SUNCheng,et al.The manufacture and application of composite wing spars[J].Fiber Reinforced Plastics/Composites,2014(2):16-22.
[5]陈际伟,赵艳文,翟全胜.复合材料壁板的数字化成型研究[J].高科技纤维与应用,2015,40(6):56-58.CHEN Jiwei,ZHAO Yanwen,ZHAIQuansheng.Study on digital molding method of composite panels[J].Hi-Tech Fiber&Application,2015,40(6):56-58.
[6]徐福泉,高大伟,杨楠楠.复合材料自动铺带技术应用及方案示例[J].航空制造技术,2009,52(22):51-54.XU Fuquan,GAO Dawei,YANGNannan.Application and proposal sample of composite automatic tape-laying technology[J].Aeronautical Manufacturing Technology,2009,52(22):51-54.
[7]王天玉,梁宪珠,杨进军.飞机复合材料构件自动铺带/丝束铺放典型设备[J].航空制造技术,2008,51(4):40-44.WANG Tianyu,LIANG Xianzhu,YANGJinjun.ATL/AFP typical equipments of aircraft composite parts[J].Aeronautical Manufacturing Technology,2008,51(4):40-44.
[8]王菲,杨博,陈永清,等.大尺寸复合材料翼梁的研制[J].航空制造技术,2015,58(S1):55-57.WANG Fei,YANG Bo,CHEN Yongqing,et al.Manufacturing of large scale composites spar[J].Aeronautical Manufacturing Technology,2015,58(S1):55-57.
[9]唐珊珊.复合材料数字化制造技术在壁板上的应用[J].金属加工,2010(S):112-113.TANG Shanahan.Application of digital manufacturing technology of the composite panels[J].Metal Working,2010(S):112-113.
[10]梁禄忠,李延征.大型复合材料壁板成型技术[J].航空制造技术,2012,55(23/24):62-66.LIANG Luzhong,LI Yanzheng.Molding technology of large scale composites panle[J].Aeronautical Manufacturing Technology,2012,55(23/24):62-66.
[11]郝建伟,陈亚莉.先进复合材料主要制造工艺和专用设备[J].航空制造技术,2008,51(10):42-44.HAO Jianwei,CHEN Yali.Manufacturing technology and special equipment for advanced composites[J].Aeronautical Manufacturing Technology,2008,51(10):42-44.
[12]黄莹.复合材料热隔膜预成型工艺分析[J].机械设计与制造工程,2015,44:20-22.HUANG Ying.The analysis on the hot diaphragm preforming process for composite material[J].Machine Design and Manufacturing Engineering,2015,44:20-22.
[13]蒲永伟,刘沛禹,刘智.大尺寸工字型复合材料长桁整体成型工艺研究[C]//第17届全国复合材料学术会议.北京,2012.PU Yongwei,LIU Peiyu,LIU Zhi.Study of integral manufacture technology for large composite stringers[C]//Proceedings of the Seventeenth National Conference on Composite Materials.Beijing,2012.