Volume 46 Issue 5
May  2025
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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
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

Tests and Numerical Analyses of the Composite Casing Containment Under Hydrothermal Environment

doi: 10.21656/1000-0887.450289
Funds:

The National Science Foundation of China(52375150)

  • Received Date: 2024-10-28
  • Rev Recd Date: 2024-11-23
  • Available Online: 2025-05-30
  • To obtain the inclusion characteristics of carbon fiber resin matrix composite casing in service environment, 2 high-speed impact ballistic tests were conducted before and after hygrothermal treatment, and the corresponding simulation model for the casing hygroscopicity partition hygrothermal test simulation model along with the finite element high-speed impact numerical simulation-analysis model, was established. The results show that, the hygrothermal treatment has significant effects on the impact resistance and energy absorption capacity of the carbon fiber resin matrix composite casing. Under the high-speed impact, the impact resistance and energy absorption capacity of the casing without hygrothermal treatment are better than those of the casing with hygrothermal treatment. The damage form of the casing under high-speed impact is dominated by the tensile failure of fiber and matrix, accompanied by a certain amount of fiber crush and in-plane shear failure, with little or no compression failure observed. The damage occurs in the vicinity of the impact area, and extends along the axial and circumferential direction of the casing. In addition, the tensile failure area of the matrix of the hygrothermally treated layer is significantly larger than that of the matrix of the untreated layer, which verifies the degradation of the mechanical properties of the matrix after hygrothermal treatment.
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  • 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))
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