Composites Moulding Method and System for Windstick

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Composites Moulding Method and System for Windstick
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Key words:叶梁%热压成型%复合材料%预浸料

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[2]Yang Tao,Gao Dianbin,Li Kaiyue.Constant Tension Winding Method of Composites and Its Application for Windstick[J].Aerospace Materials & Technology,2008,38(1):28-30.

[3]ZHAO Qing-lan,LV Yi.Design and Development of a Database System for Aeronautical Advanced Composites[J].Aircraft Design,2008,28(6).

[4]刘菲菲,刘松平,李乐刚,史俊伟,白金鹏.High-Resolution RF Ultrasonic Testing Method for Composites[J].Aeronautical Manufacturing Technology,2009(Z1).

[5]邓良才,吴建军,张深,陈中革.Optimization Layout Method for Composites Automatic Feeding[J].Aeronautical Manufacturing Technology,2013(15).

[6]HU Dian-yin,ZHANG Ze-bang,ZHANG Long,MEI Wen-bin,WANG Rong-qiao.Fatigue Life Prediction Method for Ceramic Matrix Composites[J].Aeroengine,2017,43(4):17-22.

[7]Sui Lijiang,Hu Xiaocai.Decision Support System for Composites Structure Design[J].Aeronautical Manufacturing Technology,2010(24).

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[9]陈光明,李五洲,王涛,邱求元.Design and Realization of Detection and Repair System for Helicopter Composites Components[J].Aviation Maintenance & Engineering,2013(5):65-67.

[10]ZHU He-guo,YUAN Yun-zhan,CHEN Shi,WU Xu,YU Hai-yan.Mechanical Properties of the Composites Fabricated by In Situ Method in Al-TiO2 -C System[J].Journal of Aeronautical Materials,2007,27(4):54-59.

[11]MEI Hui,ZHANG Ding,XIA Junchao,YIN Liangxuan,YU Changkui,CHENG Laifei.Brief Introduction on the Method and Progress of Nondestructive Testing for Ceramic Matrix Composites[J].Aeronautical Manufacturing Technology,2017(5).

[12]秦瑞祥,田军良.Analyzing the Inner Lacuna in ACFRRMP Skin Moulding by Using AHP Method[J].Aeronautical Manufacturing Technology,2004(5):87-89.

[13]Dong Jiwei,Feng Miaolin.Damage Simulation for 3D Braided Composites by Homogenization Method[J].Chinese Journal of Aeronautics,2010,23(6):677-685.

[14]张博明,王洋,叶金蕊.Assessment Method for Suitability of Composites Prepreg for Automated Tape Laying[J].Aeronautical Manufacturing Technology,2012(11):78-81.

[15]Liu Fenglei,Liu Dan.Joining Technologic of Interference Blind Fastener System for Composites Structure[J].Aeronautical Manufacturing Technology,2010(23).

[16]梁岱春,向颖.Research on Automated Tape-Laying NC Programming System for Composites Component[J].Aeronautical Manufacturing Technology,2013(15).

[17]白金鹏,刘松平,刘菲菲,李乐刚.Automated Ultrasonic Inspection System for Composites by Using Pulse-Echo Method[J].Aeronautical Manufacturing Technology,2009(Z1).

[18]SHAO Chuan-jin,ZUO Hong-fu,LU Xiao-hua,XU Yu-tong,LI Xin.Probabilistic Analysis Method for Typical Structural Inspection Interval of Civil Aircraft Composites[J].Aeronautical Computer Technique,2017,47(4).

[19]李薇,张永岩,张超.Research on Machining Datum Setting Method of NC Tooling for Composites Structure[J].Aeronautical Manufacturing Technology,2012(4):85-87,94.

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Cited by

[1]LI Xueqin,CHEN Ke,GUO Shuangxi.Solid Finite Elements Modeling of Composite Propeller Blade Based on Draping Simulation[J].Aerospace Materials & Technology,2020,50(1):30-36.

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