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《Acta Aeronautica Et Astronautica Sinica》 2009-03
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New Development of Extra Large Composite Aircraft Components Application Technology—Advance of Aircraft Manufacture Technology

Fan Yuqing,Zhang Lihua(School of Mechanical Engineering and Automation,Beijing University of Aeronautics and Astronautics,Beijing 100191,China)  
Starting from the evolution of the application of composites to military and civil aircraft,this article provided a survey of the application of composites in aircraft structures,especially in the main structure of Boeing 787.The specific issues in applying composites to fuselage components and the dispute between Boeing and Airbus were presented.The competition between Boeing and Airbus in applying composites was analyzed and their respective strategy was discussed using Boeing 787 and A380 as an example,which dealt with the manufacture technology of monolithic fuselage composite components and the technology of using large-scale composite panels to assemble a fuselage.The new measures of Airbus in coping with the pressure of competition were presented,which was using composite paneled fuselage skins and increasing the amount of composites on A350-XWB to 52%.Finally,the uniqueness and complexity of composite component design and manufacture were summarized,which could shed light on China's development of large-scale aircraft.
【CateGory Index】: V262
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【Citations】
Chinese Journal Full-text Database 1 Hits
1 ;A New Era of Aero-Composite[J];International Aviation;2007-03
【Co-citations】
Chinese Journal Full-text Database 10 Hits
1 Li Wenxiao,Wu Wenping(School of Aerospace Engineering and Applied Mechanics,Tongji University,Shanghai 200092,China);BENDNG PROPERTY OF PM FOAM CORE FLLED GFRP HAT-STFFENED BEAM[J];Engineering Plastics Application;2009-01
2 WANG Ling~(1,2),JIA Pu-rong~1,WANG Wen-gui~3,DAI Di~3,JIAO Guiqiong~1(1.Department of Engineering Mechanics,Northwestern Polytechnical University,Xi'an 710072,China;2.Department of Mechanics,Xi'an University of Engineering Science & Technology,Xi'an 710048,China;3.Beijing Aeronautical Manufacturing Technology Research Institute,Beijing 100024,China);Tension Strength of the Laminate with Ply Splice[J];Journal of Materials Science and Engineering;2009-01
3 YOU Wen,JIA Pu-rong,JIAO Gui-qiong,WANG Wen-gui1,DAI Di1(Department of Engineering Mechanics,Northwestern Polytechnical University,Xi'an 710072,P.R.China;Aeronautical Manufacturing Technology Research Institute1,Beijing 100024,P.R.China);Study of the Stress Concentration on the Ply Splice Region of Composites[J];Science Technology and Engineering;2008-10
4 WANG Qiang,JIA Pu-rong,WANG Wen-gui1,DAI Di1,JIAO Gui-qiong(Nothwestern Polytechnical University,Xi’an 710072 ,P.R.China; Beijing Aeronautical Manufacturing Technology Research Institute1,Beijing 100024,P.R.China);Study of Tension Strength for the Laminate with Ply Splice[J];Science Technology and Engineering;2008-11
5 YU Shouwen~(*,1) WANG Jianxiang~+ * (School of Aerospace,Tsinghua University,Beijing 100084,China) +(College of Engineering,Peking University,Beijing 100871,China);MECHANICS OF COMPOSITE MATERIALS IN THE RESEARCH AND DEVELOPMENT OF LARGE AIRCRAFT[J];Mechanics in Engineering;2007-05
6 ;Mechanical Property of Laminate With Ply Splice[J];Aeronautical Manufacturing Technology;2009-S1
7 LIANG Yong-fang,ZHANG You-qiang(Shandong Non-metallic Materials Institute,Jinan 250031,China);Research Progress and Application of Digital Technology of Composite[J];China Plastics Industry;2009-12
8 Wang Hui-feng,Cao Zeng-qiang(Aircraft Assembly and Join Technology,Northwestern Polytechnical University,Xi'an 710072, CHN);Drilling carbon fiber reinforced plastics experimental and statistical study[J];Modern Manufacturing Engineering;2008-07
9 Zhang Fuguan An Luling Li Rupeng (Nanjing University of Aeronautics and Astronautics,Nanjing 210016);Parameterized Design of Molding Tool for Composite Component[J];Aerospace Materials & Technology;2008-06
10 XU Yong-chao,DONG En-sheng(Department of Aviation Control and Engineering,Aviation University of Air Force,Changchun 130022,China);The detection technology for damages of composite components on military aircraft[J];Journal of China University of Metrology;2009-01
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