NBR Toughened PF Resin Matrix Gradient Density Ablative and Thermal-Protective Composites

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NBR Toughened PF Resin Matrix Gradient Density Ablative and Thermal-Protective Composites
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Key words:变密度%烧蚀材料%酚醛树脂

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[1]Wang Chunming,Ling Ying,Li Ruijie.NBR Toughened PF Resin Matrix Gradient Density Ablative and Thermal-Protective Composites[J].Aerospace Materials & Technology,2006,36(2):41-44.

[2]Zhang Zongqiang,Kuang Songlian,Miao Changli,Shang Long.Distortion of Resin Matrix of Thermal Protection Composites After Long Time Ablation[J].Aerospace Materials & Technology,2012,42(2):54-57.

[3]Hua Xiaoling,Miao Changli,Li Xiang,Pan Xiaoxing,Chen Haikun.Low Density Bi-Matrix Ablative Composites[J].Aerospace Materials & Technology,2013,43(2).

[4]LI Ting,ZHAO Wenbin,YANG Xuejun and TIAN Moufeng.Ablative Resin for RTM and Its Composites[J].Aerospace Materials & Technology,2019,49(3):41-44.

[5]XIAO Juan,YANG Xiaojun,HU Xin,CAI Yige and MA Wei.Near-Net Shape Forming of Thin Walled Profiled Resin Matrix Composites[J].Aerospace Materials & Technology,2018,48(5):88-90.

[6]Tao Zhiqiang,Chen Weiming,Wang Junfeng,Xiong Yanli,Yang Shiyong.Novel Strengthened and Toughened Epoxy Matrix Resins[J].Aerospace Materials & Technology,2007,37(6):25-28.

[7]LI Shujian,ZHAN Lihu,ZHOU Yuanqi and PU Yongwei.Evolution of Paving Defects During Curing Process of Advanced Resin Matrix Composites[J].Aerospace Materials & Technology,2018,48(2):20-24.

[8]Cheng Gong,Xiao Jun,Li Jianjun.Application of Resin Matrix Composites on Airborne Missile[J].Aeronautical Manufacturing Technology,2010(17).

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[10]贾丽杰.Advance in Curing Deformation of Resin Matrix Composites Structure[J].Aeronautical Manufacturing Technology,2011(15).

[11]CHEN Xin-wen,WANG Hai-peng,DENG Li-wei,WANG Xiang,JIANG Shi-cai.Compression Behavior for Aramid Fiber Reinforced Resin Matrix Composites[J].Journal of Aeronautical Materials,2011,31(Z1).

[12]刘强,王晓亮,蒋蔚,周洪飞.Application Progress of BMP Thermosetting Polyimide Resin Matrix Composites[J].Aeronautical Manufacturing Technology,2009(Z1).

[13]BAO Jian-wen,CHEN Xiang-bao.Advance in High Temperature Polyimide Resin Matrix Composites for Aeroengine[J].Journal of Aeronautical Materials,2012,32(6).

[14]ZHOU Hongfei,LIANG Hengliang,ZHANG Guoqing,LIU Yu.Application of New Type Key-Locking Insert in the Resin Matrix Composites[J].Aeronautical Manufacturing Technology,2017(6).

[15]WANG Hai-peng,CHEN Xin-wen,JIANG Shi-cai,DENG Li-wei,WANG Xiang.Comparison of In-plane Shear Test Method of Resin Matrix Composites Materials[J].Journal of Aeronautical Materials,2011,31(Z1).

[16]孙占红,阳晓辉,李小兵,刘天舒.New Approach to Toughening Resin Matrix Composites——Phase Migration Toughening[J].Aeronautical Manufacturing Technology,2012(11):96-97.

[17]ZHENG Tian-liang,ZOU Jing-cheng,YU Bo,WANG Yue-hong,ZHANG Hua.Study on Low Density and Heat-resistant Ablative Coating[J].Chinese Journal of Aeronautics,2005,18(4):372-377.

[18]高禹,李洋洋,王柏臣,于祺,王绍权,董尚利,包建文.Application of Advanced Resin Matrix Composites in Aeroengine and Its Research Progress[J].Aeronautical Manufacturing Technology,2016(21):16-21.

[19]李斌太,邢丽英,包建文,安学锋,张洋,石峰晖,李雪芹,焦健,陈祥宝.Research and Development Progress of National Key Laboratory of Advanced Composites on Advanced Aeronautical Resin Matrix Composites[J].Journal of Aeronautical Materials,2016(3):92-100.

[20]张博明,叶金蕊,周正干,刘卫平,张冬梅,刘奎,于光,周晖.Nondestructive Testing Technology for Toughened Carbon Fiber Reinforced Resin Composites[J].Aeronautical Manufacturing Technology,2010(17).

Cited by

[1]Guo Meimei,Kuang Songlian,Hua Xiaoling,Zhang Zongqiang.Heat-Resistant Effect of Pyrolysis of Resin Composites[J].Aerospace Materials & Technology,2012,42(2):58-60.

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