制备工艺对亚麻增强热塑性复合材料拉伸力学性能的影响

将增强体亚麻纱线和基体丙纶复丝制成pp/亚麻包覆纱后,进行织造,织物用层合热压法制成复合材料.制备工艺中,包覆纱法对复合材料的拉伸强度最好;麻含量50%的复合材料的拉伸强度达到最佳;当纬纱密度相同时,随着经纱密度的增大经向的拉伸强力和拉伸弹性模量也随之增大,而纬向的却随之减小,当经纱密度相同时,随着纬纱密度的增大,经向的拉伸强力和拉伸弹性模量随之减小,纬向的随之增大.     

亚麻/PP复合材料的制备及其弯曲性能研究

将亚麻纤维作为增强体,与聚丙烯(PP)纤维进行混合,同时与PP长丝形成PP包覆亚麻的纱线结构,利用机织工艺织造成机织布作为复合板材的预制件,采用层合热压方法制备亚麻/PP复合材料。通过对板材弯曲性能进行测试,研究了制备工艺、纱线结构以及亚麻纤维含量(质量分数)等因素对复合材料弯曲性能的影响。研究结果表明,"三明治"铺层方法制备的板材较"混纤法"制备的板材体现出更优异的弯曲性能;与加捻纱相比,包覆纱结构板材表现出更优良的弯曲性能;以亚麻/PP包覆纱为增强体的复合材料,当亚麻纤维质量分数为46%时,其弯曲性能最优良。     

汽车内饰用2.5维机织复合材料的制备及拉伸性能

本文以丙纶(PP)长丝、亚麻为原料,通过包缠方式将PP长丝包覆在亚麻表面以形成PP/亚麻包缠纱;分别以PP/亚麻包缠纱为经纬纱,在全自动剑杆织样机上制织三种典型的2.5维(浅交弯联、浅交直联、深角联)机织物,并将该机织物通过热压的方式制成汽车内饰用2.5维机织复合材料,研究不同组织结构对复合材料拉伸性能的影响。结果表明,2.5维机织物的经向拉伸性能表现为深角联>浅交直联>浅交弯联,纬向拉伸性能相差不大;2.5维机织复合材料的拉伸性能表现为浅交直联>浅交弯联>深角联,纬向拉伸性能相差不大。     

亚麻增强热塑性树脂复合材料板材的研究与应用

以亚麻纤维为增强体,与聚丙烯(PP)纤维按一定比例进行混合,然后制备加捻纱及PP长丝包覆的包覆纱,并利用机织工艺织成二维机织布作为复合材料的预制铺层.采用层合热压方法制备PP/亚麻纤维复合材料板材.通过对板材弯曲性能的测试及分析,研究了制备工艺、纱线结构及亚麻纤维含量等因素对复合材料弯曲性能的影响.     

聚丙烯/亚麻复合材料的制备及其冲击性能的研究

以亚麻纱线作为增强体与聚丙烯(PP)纤维按不同质量比进行混合,制备出PP长丝包覆的包覆纱,利用机织工艺织成二维机织布作为复合材料的预制铺层,采用热压法进行层合热压,制备出亚麻增强PP复合材料板材。通过对板材冲击性能的测试及分析,研究了制备工艺、纱线结构及纤维含量等因素对复合材料冲击性能的影响。结果表明,当亚麻纱线质量分数为68%时板材的冲击性能最好;"三明治"(纯亚麻织物与聚丙烯纤维毡交替铺层)法制备的板材表现出较好的冲击性能;0°/0°板材在受到冲击时比0°/90°板材吸收的冲击能更多,表现出较好的耐冲击性。     

PP/甘蔗皮纤维复合材料的拉伸性能

采用热压工艺制造聚丙烯(PP)/甘蔗皮纤维复合材料,并研究其拉伸性能。研究热压温度为175℃、压力为2 MPa、时间15 min工艺条件下纤维粒径大小和质量分数对复合材料拉伸强度和拉伸弹性模量的影响。结果表明:在甘蔗皮纤维质量分数为40%条件下,复合材料拉伸性能随着粒径减小呈现先增加后减少的趋势,当纤维粒径为40~60目(0.45~0.3 mm)时材料拉伸强度最大,为8.58 MPa,此时弹性模量为2.44 GPa;在相同纤维粒径40~60目条件下,纤维质量分数为40%时PP复合材料拉伸强度最大,纤维质量分数为50%时PP复合材料拉伸弹性模量最大,达到2.65 GPa。根据实验结果,甘蔗皮纤维增强PP复合材料在纤维粒径为40~60目、质量分数在40%时综合拉伸性能最佳。     

亚麻/聚丙烯机织复合材料薄板的制备与研究

本文以聚丙烯长丝作为基体,亚麻纱线为增强体,二者按一定体积含量进行捻合,形成合股纱,采用机织的方法织造亚麻/聚丙烯共织平纹布.选取五层平纹布进行层合热压,制备出亚麻增强聚丙烯(PP)热塑性复合材料薄板.对其拉伸性能进行测试,并分析破坏机理.     

双罗纹衬纬纬编针织物增强复合材料的拉伸性能

在电脑横机上使用玻璃纤维编织了三种双罗纹衬纬纬编针织物,以玻璃纤维针织物作为增强体,采用手糊工艺与环氧树脂复合制备了复合材料板材,在万能强力机上测试了复合材料试样的拉伸性能。结果表明,双罗纹衬纬纬编针织物增强复合材料在横向拉伸时的应力应变曲线呈现近似线性,纵向拉伸具有明显的屈服现象,横向拉伸断裂强度和模量最高,斜向次之,纵向最低;拉伸应变沿横列方向最小,拉伸性能各向异性明显;复合材料拉伸性能与增强织物结构、密度和纤维体积分数有关。     

亚麻针织物增强聚丙烯基热塑性复合材料的制备

本文以天然亚麻纤维为增强纤维,聚丙烯为基体,编织形成不同纤维体积比、不同结构的亚麻/聚丙烯针织物预制件,并经过热压复合制备形成一定的亚麻/聚丙烯针织物增强热塑性绿色环保的民用纺织复合材料。通过对增强纤维及基体材料性能的分析,以及对预制件和复合材料板材结构参数和制备工艺的设计和分析,得到较优的产品结构和制备工艺,认为亚麻/聚丙烯针织结构预制件的编织工序简单且效率高,并可直接热压复合,降低了复合材料的制备成本。4层、6层预制件热压过程中施加的最大压力为10MPa时最优,8层预制件热压过程中施加的最大压力为15MPa时最优。     

前处理对亚麻增强热塑性复合材料力学性能的影响

将增强体亚麻纱线进行碱处理和偶联剂处理，再制成pp／亚麻包覆纱后进行平纹布织造，用层合热压法制成复合材料。处理后的亚麻纱线性能发生了变化；对最终复合材料进行了拉伸性能和声发射的测试，结果表明前处理后的复合材料界面粘结性提高，拉伸强度提高，弹性模量减小，其中碱处理的作用更大。     

纤维束丝数对平纹编织C/SiC复合材料力学性能的影响

通过对2种丝束平纹编织碳纤维布增强SiC（C/SiC）复合材料的力学性能实验,研究了纤维束丝数（1 k和3 k）对复合材料性能的影响.实验结果表明：1 k C/SiC复合材料的拉伸模量、拉伸强度、压缩模量、压缩强度、面内剪切强度和弯曲强度分别为90.8 GPa,281.8 MPa,135.8 GPa,452.2 MPa,464.3 MPa和126.8 MPa,分别比3 k C/SiC高39%,15.8%,25%,132%,29.3%和30.2%.纤维束粗细不同是导致纤维束弯曲度和复合材料孔隙率差异的主要原因,对压缩强度的影响最大,对拉伸强度的影响最小.     

Fabrication and mechanical response of commingled GF/PET composites

The mechanical properties and the response to mechanical load of continuous glass fiber reinforced polyethylene terephthalate (GF/PET) laminates have been characterized. The laminates were manufactured by compression molding stacks of novel woven and warp knitted fabrics produced from commingled yarns. The laminate quality was examined by means of optical and scanning electron microscopy. Few voids were found and the laminate quality was good. Resin pockets occurred in the woven laminates, originating from the architecture of the woven fabric. The strength of the fiber/matrix interface was poor. Some problems were encountered while manufacturing the laminates. These led to fiber misalignment and consequently resulted in tensile mechanical properties that were slightly lower than expected. Flexural failures all initiated as a result of compression, and it is possible that the compression strength of the matrix material, rather than its tensile strength, might limit the ultimate mechanical performance of the composites. Flexural failures for both materials were very gradual. The warp knitted laminates were stronger and stiffer than the woven laminates. The impact behavior was also investigated; the woven laminates exhibited superior damage tolerance compared with the warp knitted laminates.     

热塑性复合材料板材拉伸强度近似计算

针对热塑性复合材料拉伸强度,以亚麻增强聚丙烯机织层合复合材料板材为例,结合理论分析,首先对其进行理想条件下的强度计算,通过推导得到理想状况下的强度理论计算公式,进而结合具体试验条件,在此理论计算公式基础上引进板材经、纬向纤维伸直系数aj、aw作为修正系数进行修正。利用多项式拟合,最终得出符合试验条件下的强度近似计算公式及拟合曲线。     

Open hole flexural and izod impact strength of unidirectional flax yarn reinforced polypropylene composites as a function of laminate lay‐up

An open hole flexural strength and impact energy of flax yarn‐reinforced polypropylene (PP) composites were studied in this work. Highest flexural strength and strength retention were observed for axial (0₆) and cross‐ply (0/90/0)_s laminates, respectively, while also examining the influence of laminate lay‐up and open hole size on flexural strength. It was found that maleic anhydride‐grafted polypropylene (MAPP)‐treated composite laminates achieved marginal improvement on flexural strength for all kinds of laminate lay‐up. Off‐axial laminates (±45₆) showed a good strength retention for open hole laminates after MAPP treatment. The fractography study confirmed microbuckling and matrix crack propagation over the compressive and tensile side of the laminate, respectively. Furthermore, severe surface damage was detected over the tensile side of 8‐mm hole size laminates. Impact test of the flax/PP laminates showed slight improvement by MAPP treatment. High‐ and low‐impact energy was experienced for axial and off‐axial laminates. The damaged impact sample shows evidence of fiber pull‐out for untreated flax yarn reinforced laminates. POLYM. COMPOS., 34:1912–1920, 2013. © 2013 Society of Plastics Engineers     

An acoustic emission study on the fracture behavior of continuous glass fiber/polypropylene composites based on commingled yarn

The fracture behavior of continuous glass fiber reinforced polypropylene composites made of commingled yarn in the form of biaxial (±±45°) noncrimp warp‐knitted fabric, twill woven fabric, and swirl mat, respectively, was investigated by virtue of single edge notched tensile (SEN‐T) specimens. These composite laminates were manufactured by compression molding and cooled at two different rates (1°C/min and 10°C/min) during the last processing phase of the laminates. The failure mechanisms were studied by acoustic emission (AE) analysis. AE amplitude ranges corresponding to the individual failure modes have been identified. For biaxial noncrimp fabric reinforced materials, the failure mechanisms involved in the fracture procedure are governed by the interface related failure events. Higher cooling rate, which is accompanied by better fiber/matrix adhesion, results in not only the increase in the relative proportion of high‐amplitude failure events, but also the occurrence of a large quantity of fiber fracture events. For woven fabric and mat reinforced composites, fiber‐dominated failure mechanisms result in the higher fracture toughness when compared with biaxial noncrimp fabric composites. Under this circumstance, the change in cooling rate only results in the difference in the relative frequency of the individual failure modes. In addition, it is found out that the initiation fracture toughness of SEN‐T specimens can be easily assessed by marking the load value which corresponds to the first point of AE signals emitted stably in AE events‐displacement curves. POLYM. COMPOS., 2008. © 2008 Society of Plastics Engineers     

加工条件对PP/芳纶复合材料横向拉伸性能的影响

对单向聚丙烯／芳纶纤维复合材料的横向拉伸性能进行了研究，讨论了压制时间、成型温度、成型压力，以及芳纶纤维的体积含量等对复合材料体系横向拉伸强度的影响。结果发现，随着压制时间、成型温度的增加，复合材料体系的横向拉伸强度提高；随成型压力的提高，复合材料的横向拉伸强度先升后降。此外，复合材料的横向拉伸强度随着芳烃纤维体积含量的增加而大幅度降低。