[1] 纪双英, 王晋, 邢军, 等. 国外航空发动机风扇包容机匣研究进展[J]. 航空制造技术, 2010(14):44-46, 48. JI S Y, WANG J, XING J,et al. Research development of containment casing of aeroengine fan abroad[J]. Aeronautical Manufacturing Technology, 2010(14):44-46, 48(in Chinese). [2] 中国民用航空总局. 航空发动机适航规定:CCAR33-R1[S]. 北京:中国民用航空总局, 2005:105. Civil Aviation Administration of China. Aero engine airworthiness regulations of china civil aviation regulations:CCAR33-R1[S]. Beijing:Civil Aviation Administration of China, 2005:105. [3] 何庆, 宣海军, 刘璐璐. 某型发动机一级风扇机匣包容性数值仿真[J]. 航空动力学报, 2012, 27(2):295-300. HE Q, XUAN H J, LIU L L. Numericalanalysis of real aero-engine first-stage fan blade containment[J]. Journal of Aerospace Power, 2012, 27(2):295-300(in Chinese). [4] ROBERTS G D, REVILOCK D M, BINIENDA W K, et al. Impact testing and analysis of composites for aircraft engine fan cases[J]. Journal of Aerospace Engineering, 2002, 15(3):104-110. [5] SHARDA J, DEENADAYALU C, MOBASHER B, et al. Modeling of multilayer composite fabrics for gas turbine engine containment systems[J]. Journal of Aerospace Engineering, 2006, 19(1):38-45. [6] STAHLECKER Z, MOBASHER B. Development of reliable modeling methodologies for engine fan blade out containment analysis. Part II:Finite element analysis[J]. International Journal of Impact Engineering, 2009, 36(3):447-459. [7] NAIK D, SANKARAN S, MOBASHER B, et al. Development of reliable modeling methodologies for fan blade out containment analysis. Part I:Experimental studies[J]. International Journal of Impact Engineering, 2009, 36(1):1-11. [8] BINIENDA W, SANCAKTAR E, ROBERTS G D. Design, progressive modeling, manufacture, and testing of composite shield for turbine engine blade containment:NASA 20020036226[R]. Washington, D.C.:NASA, 2002. [9] GOLDBERG R K, BLINZLER B J, BINIENDA W K. Modification of a macromechanical finite element-based model for impact analysis of triaxially braided composites[J]. Journal of Aerospace Engineering, 2010, 25(3):383-394. [10] SUN X C, HALLETT S R. Failure mechanisms and damage evolution of laminated composites under compression after impact (CAI):Experimental and numerical study[J]. Composites Part A:Applied Science and Manufacturing, 2018, 104:41-59. [11] TIRILLÒ J, FERRANTE L, SARASINI F, et al. High velocity impact behaviour of hybrid basalt-carbon/epoxy composites[J]. Composite Structures, 2017, 168:305-312. [12] 陈战辉, 万小朋, 黄文博, 等. 混杂与非混杂层合板弹丸冲击试验研究[J]. 机械科学与技术, 2019, 38(5):803-808. CHEN Z H, WAN X P, HUANG W B, et al. Experimental investigation of bullet impact damage of hybridand non-hybrid laminates[J]. Mechanical Science and Technology for Aerospace Engineering, 2019, 38(5):803-808(in Chinese). [13] AHMED S, ZHENG X T, YAN L L, et al. Influence of asymmetric hybridization on impact response of 3D orthogonal woven composites[J]. Composites Science and Technology, 2020, 199:108326. [14] WAGNER T, HEIMBS S, FRANKE F, et al. Experimental and numerical assessment of aerospace grade composites based on high-velocity impact experiments[J]. Composite Structures, 2018, 204:142-152. [15] 胡年明, 陈长海, 侯海量, 等. 高速弹丸冲击下复合材料层合板损伤特性仿真研究[J]. 兵器材料科学与工程, 2017, 40(3):66-70. HU N M, CHEN C H, HOU H L, et al. Simulationon damage characteristic of composite laminates under high-velocity projectile impact[J]. Ordnance Material Science and Engineering, 2017, 40(3):66-70(in Chinese). [16] 王绪财, 彭刚, 冯家臣, 等. 弹道冲击条件下芳纶织物增强复合材料靶板破坏模式及吸能研究[J]. 防护工程, 2015(3):21-25. WANG X C, PENG G, FENG J C,et al. Experimental research on the fracture pattern and energy absorbing of Kevlar fabric reinforced composite under ballistic impact[J]. Protective Engineering, 2015(3):21-25(in Chinese). [17] 邓君. 纤维增强复合材料层合板抗冲击性试验及数值分析[D]. 南京:南京航空航天大学, 2010. DENG J. Test and numerical simulation of impact resistance of fiber reinforced[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2010(in Chinese). [18] 陆晓. 碳纤维增强复合材料机匣包容性的数值仿真研究[D]. 杭州:浙江大学, 2011. LU X. Numerical simulation of carbon fiber reinforced composite aeroengine case containment[D]. Hangzhou:Zhejiang University, 2011(in Chinese). [19] 何泽侃, 宣海军, 胡燕琪, 等. Kevlar缠绕增强机匣包容过程研究[J]. 工程力学, 2017, 34(增刊1):308-313. HE Z K, XUAN H J, HU Y Q, et al. Investigation on containment process of case wrapped with Kevlar fabric[J]. Engineering Mechanics, 2017, 34(Sup. 1):308-313(in Chinese). [20] 刘璐璐, 宣海军, 张娜. 航空发动机复合材料机匣叶片包容性研究[J]. 工程力学, 2013, 30(增刊1):314-319. LIU L L, XUAN H J, ZHANG N. Investigation on blade containment of aero-engine composite case[J]. Engineering Mechanics, 2013, 30(Sup. 1):314-319(in Chinese). [21] XUAN H J, LIU L L, CHEN G T, et al. Impact response and damage evolution of triaxial braided carbon/epoxy composites. Part I:Ballistic impact testing[J]. Textile Research Journal, 2013, 83(16):1703-1716. [22] LIU L L, XUAN H J, ZHANG N, et al. Impact response and damage evolution of triaxial braided carbon/epoxy composites. Part II:Finite element analysis[J]. Textile Research Journal, 2013, 83(17):1821-1835. [23] 李明. 2.5D机织复合材料冲击后剩余强度研究[D]. 南京:南京航空航天大学, 2010. LI M. Analyses of residual strength of 2.5D woven composites after impact[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2010(in Chinese). [24] REN C L, LIU T, SIDDIQUE A, et al. High-speed visualizing and mesoscale modeling for deformation and damage of 3D angle-interlock woven composites subjected to transverse impacts[J]. International Journal of Mechanical Sciences, 2018, 140:119-132. [25] 宋曼丽. 三维编织/机织复合材料机匣包容性研究[D]. 杭州:浙江大学, 2020. SONG M L. Research on the containment of 3D braided/woven composite casing[D]. Hangzhou:Zhejiang University, 2020(in Chinese). |