首页> 外文会议>SEM Annual Conference and Exposition on Experimental and Applied Mechanics >Design of a Low-Cost Aircraft Structural Material Based on Epoxy: Recycled Rubber Composites Modified with Multifunctional Nano Particles
【24h】

Design of a Low-Cost Aircraft Structural Material Based on Epoxy: Recycled Rubber Composites Modified with Multifunctional Nano Particles

机译:基于环氧树脂的低成本飞机结构材料设计:用多功能纳米颗粒改性再生橡胶复合材料

获取原文

摘要

Recycling is an intensely studied subject in terms of sustainable development and it offers clean and cost-efficient solutions in many industries. For this reason, manufacturers tend to find clean and cost-efficient solutions by utilizing recycled materials to produce new components. In this regard, rubbers have a very wide usage area in aeronautic and automotive industries including structural and interior body components. Rubbers are also used to modify brittle polymer components in the existence of hard, resistant fillers. In this study, fresh scrap EPDM (ethylene propylene diene monomer) rubbers are used to manufacture novel composites by modifying epoxy resin with the inclusion of alumina (Al_2O_3) fibers (AFs). In case of a homogeneous distribution, addition of AFs ensures desired mechanical properties due to its favorable structural characteristics such as interlocking effects of fibers. These novel composites can be used in the manufacture of various solid structural parts of the fuselage and suspension pads in aerospace industry. This paper primarily explains the manufacturing of these composites and after the mechanical characterization, numerical approaches are implemented to test the durability of the structures. The mechanical and physical properties of these composite systems are studied in the present work. Dynamic Mechanical Analysis (DMA) analyses are carried out to determine thermal-mechanical properties. Three-point bending and compression tests are performed to see the mechanical behavior of the composites. In the end, manufactured compositions are tested numerically in terms of the structural reliability of a body component in a commercial aircraft.
机译:在可持续发展方面,回收是一项强烈研究的主题,它在许多行业提供干净且经济高效的解决方案。因此,制造商通过利用再循环材料生产新组件,制造商倾向于找到清洁和成本效益的解决方案。在这方面,橡胶在航空和汽车工业中具有非常广泛的使用区域,包括结构和内部主体部件。橡胶还用于改变脆性聚合物组分,存在硬质耐填料。在本研究中,新鲜废料EPDM(乙烯丙烯二烯单体)橡胶用于通过包含氧化铝(AL_2O_3)纤维(AFS)来改变环氧树脂制造新型复合材料。在均匀分布的情况下,由于其良好的结构特征,例如纤维的互锁效应,因此由于其良好的结构特征而确保了AFS确保所需的机械性能。这些新型复合材料可用于制造机身和悬架垫的各种固体结构部件,在航空航天工业中。本文主要解释了这些复合材料的制造和在机械表征之后,实现了数值方法以测试结构的耐用性。在本作工作中研究了这些复合系统的机械和物理性质。进行动态力学分析(DMA)分析以确定热机械性能。进行三点弯曲和压缩测试以看出复合材料的机械行为。最终,在商用飞机中的主体部件的结构可靠性方面进行了数量地测试制造的组合物。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号