Citation: | ZHENG Jingbo, ZHANG Ying, JIANG Wenlong, WEI Lin, CHI Xue, YI Wenzhao, LIU Lulu, CHEN Wei. Tests and Numerical Analyses of the Composite Casing Containment Under Hydrothermal Environment[J]. Applied Mathematics and Mechanics, 2025, 46(5): 661-675. doi: 10.21656/1000-0887.450289 |
陈光. 航空发动机结构设计分析[M]. 北京: 北京航空航天大学出版社, 2006: 548-551.(CHEN Guang.Analysis of Aeroengine Structure Design[M]. Beijing: Beihang University Press, 2006: 548
-551. (in Chinese))
|
[2]United States Air Force. Engine structural integrity program: MIL2STD21783B[S]. USA: Department of Defense, 2002.
|
[3]中国民用航空局. 航空发动机适航规定: CCAR—33R2[S]. 北京: 中国民用航空局, 2016.(Civil Aviation Administration of China. Aviation engine air-worthiness regulations: CCAR—33R2[S]. Beijing: Civil Aviation Administration of China, 2016. (in Chinese))
|
[4]HOLMES M. Carbon fibre reinforced plastics market continues growth path[J].Reinforced Plastics,2013,57(6): 24-29.
|
[5]MARSH G. Aero engines lose weight thanks to composites[J].Reinforced Plastics,2012,56(6): 32-35.
|
[6]MAZUMDAR S.Composites Manufacturing: Materials, Product, and Process Engineering[M]. Boca Raton: CRC Press, 2001.
|
[7]沈尔明, 王志宏, 赵凤飞, 等. 风扇机匣材料应用现状与发展[J]. 航空制造技术, 2013,56(13): 92-95.(SHEN Erming, WANG Zhihong, ZHAO Fengfei, et al. Application and development of material for aeroengine fan case[J].Aeronautical Manufacturing Technology,2013,56(13): 92-95. (in Chinese))
|
[8]李佳楠, 姜亚明, 项赫, 等. 高性能纤维增强树脂基复合材料湿热老化研究进展[J]. 化工新型材料, 2024,52(1): 1-7.(LI Jianan, JIANG Yaming, XIANG He, et al. Research progress on the hygrothermal aging of high-performance fiber reinforced resin matrix composites[J].New Chemical Materials,2024,52(1): 1-7. (in Chinese))
|
[9]DEWHURST T B. The impact load on containment rings during a multiple blade shed in aircraft gas turbine engines[C]//Proceedings of the ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition. Orlando, FL, USA: ASME, 1991.
|
[10]RICHARDSON I J, HYDE T M, BECKER A A, et al. A three-dimensional finite element investigation of the bolt stresses in an aero-engine Curvic coupling under a blade release condition[J].Proceedings of the Institution of Mechanical Engineers,Part G:Journal of Aerospace Engineering,2000,214(4): 231-245.
|
[11]张伯熹, 宣海军, 吴荣仁. 航空发动机涡轮叶片包容模拟试验研究[J]. 机械工程师, 2006(10): 114-116.(ZHANG Boxi, XUAN Haijun, WU Rongren. Research on aero-engine turbine blade containment experiment[J].Mechanical Engineer,2006(10): 114-116. (in Chinese))
|
[12]古兴瑾. 复合材料层板高速冲击损伤研究[D]. 南京: 南京航空航天大学, 2011.(GU Xingjin. Research on high velocity impact damage of composite laminates[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2011. (in Chinese))
|
[13]蔡雄峰. 复合材料层合板高速冲击损伤研究[D]. 天津: 中国民航大学, 2020.(CAI Xiongfeng. Research on high-speed impact damage of composite laminates[D]. Tianjin: Civil Aviation University of China, 2020. (in Chinese))
|
[14]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 Qing, XUAN Haijun, LIU Lulu. Numerical analysis of real aero-engine first-stage fan blade containment[J].Journal of Aerospace Power,2012,27(2): 295-300. (in Chinese))
|
[15]杜长美. 三维四向编织复合材料湿热老化后低速冲击及其剩余压缩性能研究[D]. 哈尔滨: 哈尔滨理工大学, 2023.(DU Changmei. Study on low-velocity impact and residual compression properties of three-dimensional four-directions braided composites after damp-heat aging[D]. Harbin: Harbin University of Science and Technology, 2023. (in Chinese))
|
[16]MOKHTAR H, SICOT O, ROUSSEAU J, et al. The influence of ageing on the impact damage of carbon epoxy composites[J].Procedia Engineering,2011,10: 2615-2620.
|
[17]HOSUR M V, JAIN K, CHOWDHURY F, et al. Low-velocity impact response of carbon/epoxy laminates subjected to cold-dry and cold-moist conditioning[J].Composite Structures,2007,79(2): 300-311.
|
[18]ZHANG C, BINIENDA W K, MORSCHER G N, et al. Experimental and FEM study of thermal cycling induced microcracking in carbon/epoxy triaxial braided composites[J].Composites (Part A):Applied Science and Manufacturing,2013,46: 34-44.
|
[19]ATAS C, DOGAN A. An experimental investigation on the repeated impact response of glass/epoxy composites subjected to thermal ageing[J].Composites Part B:Engineering,2015,75: 127-134.
|
[20]徐凯龙. 循环湿热作用下三维编织复合材料力学性能与抗冲击性能研究[D]. 南京: 南京航空航天大学, 2018.(XU Kailong. Effect of cyclic hygrothermal aging on mechanical properties and impact resistance of three dimensional braided composites[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2018. (in Chinese))
|
[21]LIU L, ZHAO Z, CHEN W, et al. An experimental investigation on high velocity impact behavior of hygrothermal aged CFRP composites[J].Composite Structures,2018,204: 645-657.
|
[22]惠旭龙, 牟让科, 白春玉, 等. TC4钛合金动态力学性能及本构模型研究[J]. 振动与冲击, 2016,35(22): 161-168.(HUI Xulong, MU Rangke, BAI Chunyu, et al. Dynamic mechanical property and constitutive model for TC4 titanium alloy[J].Journal of Vibration and Shock,2016,35(22): 161-168. (in Chinese))
|