Study on the effect of geometric errors of CFRP connection holes on the tensile strength of bolted structures
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摘要: 针对CFRP沉头螺栓连接孔制孔几何误差对连接结构拉伸强度的影响规律开展了相关研究。为了更为准确预测连接结构的应力变化情况,首先基于准静态试验建立了TC4ELI钛合金的本构模型,并基于Hashin失效准则以及界面的双线性本构建立了复合材料模型,在此基础上形成了复合材料沉头螺栓连接结构的有限元模型,并针对3个主要的制孔误差对连接结构力学性能的影响进行了数值模拟以及实验验证。研究结果表明所建立的有限元模型能够较为准确地预测连接结构失效形式以及拉伸强度。其次,相较于沉头角度以及倒角半径误差,沉头深度几何误差对最终连接结构最大应力值的影响最为显著,同时锪窝孔尺寸上下偏差对连接结构拉伸性能的影响具有较为明显的差异性。Abstract: In this study, the effects of geometrical errors of CFRP countersunk bolt connection holes on the tensile strength of the connection structure are investigated. In order to obtain the stress distribution of the joint structure, the constitutive model of TC4ELI titanium alloy was developed by quasi-static experiments, and the material model of CFRP was established by combining the Hashin failure criterion and the bilinear constitution for the material interface. On this basis, a finite element model of the composite countersunk bolt joint structure was developed, and numerical simulations and experiments were conducted to verify the effects of three major hole-making errors on the mechanical properties of the bolted joint. The results showed that the proposed finite element model can accurately predict the failure pattern and tensile strength of the bolted joint. Secondly, the geometric error of countersink depth has the most significant impact on the final maximum stress value of the jointed structure compared to the error of countersink angle and fillet radius. Meanwhile, the influence of the upper and lower deviation of the countersink hole size on the tensile properties of the bolted joints has an obvious diversity.
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Key words:
- constitutive model /
- hole-making error /
- FEM /
- bolted joint
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表 1 复合材料力学性能参数[15]
参数名 选取值 参数名 选取值 $ {E_{{\text{11}}}}{\text{/GPa}} $ 133 ${G_{23} }/{\rm{GP}}{\text{a} }$ 3.99 ${E}_{22}、{E}_{33}/{\rm{GP} }{{\rm{a}}}$ 8 $ {\nu _{12}} $、$ {\nu _{13}} $ 0.25 ${G_{12} }/{\rm{GP} }{\rm{a}}$ 5.32 $ {\nu _{23}} $ 0.34 ${G_{13} }/{\rm{GP}}{\text{a} }$ 5.32 ${S}_{12}、{S}_{13}、{S}_{23}/{\rm{MPa}}$ 81 ${X_T}/{\rm{MPa}}$ 1 300 ${K}_{n}、{K}_{s}、{K}_{t}/({\rm{N} }\cdot {\rm{m} }{{\rm{m}}}^{-3})$ 106 ${X_C}/{\rm{MPa}}$ 1 900 ${G_n}/({\rm{N}} \cdot {\rm{m}}{{\rm{m}}^{ - 1} })$ 0.33 ${Y_T}/{\rm{MPa}}$ 41 ${G_s} = {G_t}/({\rm{N}} \cdot {\rm{m}}{{\rm{m}}^{ - 1} })$ 1.209 ${Y_C}/{\rm{MPa}}$ 170 $t_n^0/{\rm{MPa}}$ 60 $t_s^0 = t_t^0/{\rm{MPa}}$ 110 表 2 制孔误差正交试验方案和实验结果
组号 沉头深度
/mm沉头角度
/(°)倒角半径
/mm应力最大值
/MPa1 1.1 99 0.6 1 055 2 1.1 100 0.75 1 011 3 1.1 101 0.9 1 109 4 1.0 99 0.75 1 219 5 1.0 100 0.9 1 204 6 1.0 101 0.6 1 169 7 0.9 99 0.9 1 086 8 0.9 100 0.6 1 077 9 0.9 101 0.75 1 111 表 3 制孔误差正交试验极差分析
水平 沉头深度/mm 沉头角度/(°) 倒角半径/mm 1 1 086 1 109 1 169 2 1 069 1 011 1 219 3 1 104 1 055 1 230 极差 139 32 33 F值 0.099 0.678 0.683 -
[1] Coleman R M. The effects of design, manufacturing processes and operations management on the assembly of aircraft composite structure[J]. Massachusetts Institute of Technology, 1991(3): 120-135. [2] 姜立业, 李娜, 陈鹏. 碳纤维复合材料在轻量化的应用和前景[J]. 塑料工业, 2022, 50(1): 14-19. doi: 10.3969/j.issn.1005-5770.2022.01.004 [3] 包建文, 蒋诗才, 张代军. 航空碳纤维树脂基复合材料的发展现状和趋势[J]. 科技导报, 2018, 36(19): 52-63. [4] 罗云烽, 姚佳楠. 高性能热塑性复合材料在民用航空领域中的应用[J]. 航空制造技术, 2021, 64(16): 93-102. doi: 10.16080/j.issn1671-833x.2021.16.093 [5] 周松. 复合材料螺栓连接渐进损伤的实验及数值分析[D]. 哈尔滨: 哈尔滨工程大学, 2013. [6] 陈群志, 关志东, 王进, 等. 分层缺陷对复合材料结构疲劳寿命影响研究[J]. 机械强度, 2004, 26(z1): 121-123. doi: 10.3321/j.issn:1001-9669.2004.z1.036 [7] König W, Graß P. Quality definition and assessment in drilling of fibre reinforced thermosets[J]. CIRP Annals - Manufacturing Technology, 1989, 38(1): 119-124. doi: 10.1016/S0007-8506(07)62665-1 [8] Andrews S D, Ochoa O O, Owens S D. The effects of fastener hole defects[J]. Journal of Composite Materials, 1993, 27(1): 2-20. doi: 10.1177/002199839302700101 [9] 张勋. CFRP承载结构制孔过程有限元分析及验证[D]. 南京: 南京航空航天大学, 2020. [10] 李万平. CFRP/铝合金叠层构件制孔工艺与连接性能研究[D]. 大连: 大连理工大学, 2020. [11] 谢奇, 吕运冰. Ramberg—Osgood形幂硬化材料的硬化系数及硬化指数的确定[J]. 武汉交通科技大学学报, 1996, 20(3): 319-322. [12] Hashin Z. Fatigue failure criteria for unidirectional fiber composites[J]. Journal of Applied Mechanics, 1981, 48(4): 846-852. doi: 10.1115/1.3157744 [13] Hashin Z, Rotem A. A fatigue failure criterion for fiber reinforced materials[J]. Journal of Composite Materials, 1973, 7(4): 448-464. doi: 10.1177/002199837300700404 [14] Benzeggagh M L, Kenane M. Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus[J]. Composites Science and Technology, 1996, 56(4): 439-449. doi: 10.1016/0266-3538(96)00005-X [15] 秦旭达, 唐心凯, 葛恩德, 等. CFRP三维铣削仿真模型的建立及层间损伤分析[J]. 宇航材料工艺, 2020, 50(1): 22-29. doi: 10.12044/j.issn.1007-2330.2020.01.003