Effect of thermo-oxidative aging on the mechanical properties of multi-layered biaxial weft knitted fabric reinforced composites
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摘要: 通过改变预制体结构衬纱取向的方法制备了几种含不同剪切角的纬编双轴向多层衬纱(Multilayered biaxial weft knitted,MBWK)织物增强复合材料。基于Arrhenius模型和Ozawa法设计了热氧老化试验,采用力学性能测试、DSC、FTIR和DMA测试对老化前后的试样热-物理性能进行了表征。实验结果表明:预制体的纱线剪切角不同,其复合材料受热氧老化后力学性能的保留率也显著不同,由于乙烯基酯树脂在热氧老化环境中会发生后固化现象,因此复合材料的弯曲模量在老化过程中呈现先增加后下降的趋势,而拉伸性能则受到增强体结构的影响,纤维/基体界面的结合力退化使拉伸模量在老化过程中持续下降;随着老化时间的延长,树脂的固化度逐渐增加,玻璃化转变温度Tg逐渐升高,储能模量峰值在老化初期由于分子链交联上升,老化后期分子链断裂占据主导作用致使峰值逐渐下降。
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关键词:
- 纬编双轴向多层衬纱织物增强复合材料 /
- 芳纶纤维 /
- 热氧老化 /
- 力学性能 /
- 剪切角
Abstract: Several multilayered biaxial weft knitted (MBWK) fabric reinforced composites with different shear angles were prepared by changing the orientation of preform inserting yarns. The thermo-oxidative aging test was designed based on Arrhenius model and Ozawa method. The thermal and physical properties of the samples before and after aging were characterized by mechanical properties, DSC, FTIR and DMA tests. The experimental results show that: With the change of yarns’ shearing angle, the composite mechanical properties retention rate after thermo-oxidative aging is also significantly different, because the post curing will occur for the vinyl ester resin in the thermo-oxidative aging environment. Therefore, the bending modulus of the composite materials in the aging process presents downward trend after increased first, and the tensile properties are affected by the reinforcement structure. The degradation of adhesion strength at fiber/matrix interface makes the tensile modulus decrease continuously during the aging process. With the aging time prolongation, the curing degree of resin increases gradually, and the glass transition temperature Tg increases gradually. The peak value of energy storage modulus increases at the initial stage of aging due to molecular chain crosslinking, while decreasing of the peak value is caused by molecular chain fracture at the later stage of aging. -
图 4 不同剪切角的MBWK复合材料试样
Figure 4. MBWK composite samples with different shear angles
Z-0°, Z-10°, Z-20°, Z-30°, Z-40°—Specimens with shear angles of 0°, 10°, 20°, 30°, 40° liner warp orientation in the same direction as the length of specimen; N-0°, N-10°, N-20°, N-30°, N-40°—Sample with shear angles of 0°, 10°, 20°, 30°, 40° liner warp orientation perpendicular to the sample length direction
表 1 MBWK织物参数
Table 1. MBWK fabric parameters
Type Parameter Weft inserting yarns Kevlar-49 (474 g·km−1 (158×3)) Warp inserting yarns Kevlar-49 (948 g·km−1 (158×6)) Stitching yarns Polyester (16.7 g·km−1 (8.33×2)) Layer structure 90°/0°/90° Warp density/(tows·cm−1) 30 Weft density(tows·cm−1) 30 Thickness/mm 1.5 表 2 RIPOXY R-806 乙烯基酯树脂(VER)成品性能指标
Table 2. RIPOXY R-806 vinyl ester resin (VER) finished product performance indicators
Parameter Value Tensile strength/MPa 69-89 Tensile modulus/GPa 2.9-3.3 Tensile elongation at break/% 3.2-4.0 Flexural strength/MPa 120-150 Flexural modulus/GPa 2.9-3.3 Distortion temperature/℃ 108-118 Barcol hardness 40 Volume shrinkage/% 7.5-8.5 表 3 VER浇铸体活化能计算数据
Table 3. Calculation data of activation energy of the VER casting body
Mass loss ratio Slope Activation energy/eV Average value/eV Deviation/% 0.90 −4315.24 0.8315 0.8029 3.56 0.85 −4238.74 0.7941 0.80 0.80 −4227.99 0.7832 1.97 表 4 MBWK复合材料和VER浇铸体的热氧老化实验时间与自然老化时间对应关系
Table 4. Relationship between the thermo-oxidative aging experimental time and the natural aging time of the MBWK composite and VER casting body
Temperature/
℃Thermo-oxidative
aging/hNatural aging
time/Month100 0.5 1 3.5 7 6.5 13 10 20 13.5 27 18 36 表 5 VER液态体系DSC测试结果
Table 5. DSC test results of VER liquid system
Heating rate/(℃·min−1) Initial temperature/℃ Peak temperature/℃ Final temperature/℃ Total enthalpy of reaction/(J·g−1) 2 83.6 88.9 93.0 266.1 5 89.3 98.6 113.6 235.1 10 125.1 138.4 155.5 279.5 12 149.9 164.1 173.9 249.9 15 155.5 172.8 185.3 256.6 表 6 VER浇铸体热氧老化后DSC测试结果
Table 6. DSC test results of the VER casting body after thermo-oxidative aging
Aging time/h Heating rate/
(℃·min−1)Initial
temperature/℃Peak
temperature/℃Final
temperature/℃Heat enthalpy/
(J·g−1)Degree of
cure/%0 5 61.4 80.5 132.6 73.270 71.54 0.5 5 76.5 93.9 131.3 37.770 85.33 3.5 5 128.9 135.3 148.7 11.460 95.55 6.5 5 129.7 137.1 150.8 11.400 95.57 10 5 111.4 120.3 134.9 11.310 95.60 13.5 5 119.4 137.6 146.4 4.078 98.42 18 5 123.1 136.1 150.3 3.635 98.60 -
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