[1] 金成柱. NOMEX蜂窝材料高速加工工艺及固持可靠性研究[D]. 杭州:浙江大学, 2006. JIN Chengzhu. Study on high speed machining process and reliability of fixture method for Nomex honeycomb[D]. Hangzhou:Zhejiang University,2006. [2] KE Yinglin,JIN Chengzhu,LIU Gang|, et al. Optimization of high-speed milling prosess for Nomex honeycomb[J]. China Mechanical Engineering,2006,17(12):1299-1302. [3] FOO C C,CHAI G B,SEAH L K. Mechanical properties of Nomex material and Nomex honeycomb structure[J]. Composite Structures,2007,80(4):588-594. [4] 张胜文. 纸蜂窝件数控加工方法[J].金属加工,2009(16):25-28 ZHANG Shengwen. Paper honeycomb CNC machining mechod[J]. Machinist Metal Forming,2009(16):25-28. [5] 张超海, 龚清洪. Nomex蜂窝芯结构零件超声切割与传统数控加工的对比研究[C]//全国复合材料学术会议, 2012. ZHANG Chaohai, GONG Qinghong. Contrast research of ultrasonic cutting technology and traditional high-speed machining method for processing honeycomb sandwich structure[C]//National Conference on Composite Materials,2012. [6] KIM D S,LEE J R. Compressive mechanical properties of the Nomex/thermoset honeycomb cores[J]. Polymers for Advanced Technologies,1997,8(1):1-7. [7] GORNET L. Modeling of Nomex honeycomb cores,linear and nonlinear behaviours[J]. Mechanics of Advanced Materials & Structures,2007,14(8):589-601. [8] REDDY J N. Mechanics of advanced materials and structures[J]. London:Taylor and Francis Ltd,2006. [9] 盛磊. 蜂窝夹层结构芯子塌垮的工艺分析[J]. 航天制造技术,1994(6):27-30. SHENG Lei. Processing analysis of honeycomb sandwich structure core collapse[J]. Aerospace Manufacturing Technology,1994(6):27-30. [10] AKTAY L,JOHNSON A F,HOLZAPFEL M. Prediction of impact damage on sandwich composite panels[J]. Computational Materials Science,2005,32(3):252-260. [11] AKTAY L,JOHNSON A F,KRÖPLIN B H. Numerical modelling of honeycomb core crush behaviour[J]. Engineering Fracture Mechanics,2008,75(9):2616-2630. [12] AMINANDA Y,CASTANIE B,BARRAU J J. Behavior of indented sandwiches structure with Nomex honeycomb core and metallic skins subjected to compressive loading (CAI)[J]. Key Engineering Materials,2007,345-346:729-732. [13] HERUP E J,PALAZOTTO A N. Low-velocity impact damage initiation in graphite/epoxy/Nomex honeycomb-sandwich plates[J]. Composites Science & Technology,2013,57(12):1581-1598. [14] YAO Wuwen,FENG Chunxiao,LU Yang. Bonding and repairing technique for airplane honeycomb components[J/OL]. Adhesion in China,2003:1. http://en.cnki.com.cn/Article_en/CJFDTOTAL-NIAN200301022.htm. [15] 中华人民共和国国家军用标准. GJB 1874-94飞机结构用芳纶纸基蜂窝芯材规范[S]. 北京:国防科学技术工业委员会,1994. People's Republic of China National Military Standard. GJB 1874-94 Specification of paper honeycomb material for aircraft[S]. Beijing:National Defense Science and Technology Industry Committee,1994. [16] ROY R,PARK S J,KWEON J H,et al. Characterization of Nomex honeycomb core constituent material mechanical properties[J]. Composite Structures,2014,117(1):255-266. [17] 许潮华,张小珍,宋桂枝. 新型Nomex蜂窝芯材及其制造[J]. 材料工程,1984(5):23-24. XU Chaohua,ZHANG Xiaozhen,SONG Guizhi,New type of Nomex honeycomb material and manufacturing[J]. Materials Engineering,1984(5):23-24. [18] 黄秀秀,胡小平,于保华. 蜂窝复合材料超声切割力建模及工艺参数选择研究[J]. 机电工程,2015,32(1):32-36. HUANG Xiuxiu,HU Xiaoping,YU Baohua. Ultrasonic cutting force model of honeycomb composites and selection of processing parameters[J]. Journal of Mechanical & Electrical Engineering,2015,32(1):32-36. |