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high strength nanomaterials fiber for lightweight composite missile cases

机译:用于轻型复合导弹外壳的高强度纳米材料纤维

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Solid rocket motor cases for advanced tactical missile systems use lightweight, high strength carbon fiber reinforced composite materials to achieve high propellant mass fractions and increase overall propulsion system efficiency. In order to meet the challenging performance goals for next-generation missile systems, significant improvements in the performance of the motor case materials are desired. Recent advances in the development of carbon nanotube (CNT) reinforced composite materials provide an opportunity for achieving improved composite strength and multifunctional performance capability for advanced lightweight composite missile cases. While processes for producing relatively short lengths of CNT reinforced carbon fibers have been previously demonstrated on a laboratory scale, further research and development is needed to scale-up such processes to achieve production of significant lengths of CNT reinforced fibers that are suitable for incorporation into continuous fiber reinforced composite structures such as filament wound composite motor cases.Under a U.S. Army Small Business Innovation Research (SBIR) program, Materials Sciences Corporation (MSC) and Drexel University Fibrous Materials Research Laboratory (DU/FMRL) are collaborating on the development and characterization of CNT reinforced fibers produced via a modified electrospinning process. The ultimate goal of this research is to develop and demonstrate a robust, scaleable process for continuous production of CNT reinforced carbon fibers having significantly greater strength than commercially available carbon fibers (e.g., IM7, T1000) currently used in high performance filament wound composite structures. An integrated manufacturing, analysis and experimentation approach is being carried out to evaluate the influence of different CNT concentrations and process conditions on delivered fiber strength.As part of the Phase I research, single wall nanotube (SWNT) and multiwall nanotube (MWNT) reinforced PAN fibers were synthesized via a drum electrospinning process and tensile testing was performed to compare the mechanical properties and processing characteristics for electrospun yarns having different concentrations of SWNT and MWNT reinforcement. Characterization via Raman spectroscopy, Scanning Electron Microscopy (SEM) and High Resolution Transmission Electron Microscopy (HRTEM) was performed to assess SWNT and MWNT alignment and dispersion. A simplified analytical model based on proven micromechanics was also developed as part of this research for predicting the elastic properties of CNT reinforced fibers with different SWNT and MWNT concentrations. This model is intended to serve as a first level approximation tool for supporting the design and evaluation of CNT reinforced carbon fibers with different types and concentrations of CNT loading.
机译:用于高级战术导弹系统的固体火箭发动机壳体使用轻质,高强度碳纤维增强复合材料来获得较高的推进剂质量分数并提高总体推进系统效率。为了满足下一代导弹系统具有挑战性的性能目标,需要对机壳材料的性能进行重大改进。碳纳米管(CNT)增强复合材料开发的最新进展为提高轻型复合导弹壳体的复合强度和多功能性能提供了机会。虽然先前已经在实验室规模上证明了生产相对较短长度的CNT增强碳纤维的方法,但仍需要进一步的研究和开发以扩大此类方法的规模,以实现大量长度的CNT增强碳纤维的生产,这些纤维适合掺入连续生产中纤维增强复合材料结构,例如缠绕纤维的复合电机外壳。 根据美国陆军小型企业创新研究(SBIR)计划,材料科学公司(MSC)和德雷塞尔大学纤维材料研究实验室(DU / FMRL)正在合作开发和改性通过改性电纺丝工艺生产的CNT增强纤维。这项研究的最终目标是开发并证明一种稳健的,可缩放的方法,用于连续生产CNT增强碳纤维,其强度明显高于目前在高性能长丝缠绕复合结构中使用的市售碳纤维(例如IM7,T1000)。正在进行集成的制造,分析和实验方法,以评估不同的CNT浓度和工艺条件对输送的纤维强度的影响。 作为第一阶段研究的一部分,通过鼓式电纺丝工艺合成了单壁纳米管(SWNT)和多壁纳米管(MWNT)增强PAN纤维,并进行了拉伸测试以比较不同浓度的电纺纱的机械性能和加工特性。 SWNT和MWNT加固。通过拉曼光谱,扫描电子显微镜(SEM)和高分辨率透射电子显微镜(HRTEM)进行表征,以评估SWNT和MWNT的排列和分散。作为该研究的一部分,还开发了基于可靠的微力学的简化分析模型,用于预测不同SWNT和MWNT浓度的CNT增强纤维的弹性。该模型旨在用作一级近似工具,以支持不同类型和浓度的CNT负载的CNT增强碳纤维的设计和评估。

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