4.7 Article

High-Volume-Fraction Textured Carbon Nanotube-Bis(maleimide) and -Epoxy Matrix Polymer Nanocomposites: Implications for High-Performance Structural Composites

期刊

ACS APPLIED NANO MATERIALS
卷 5, 期 7, 页码 9008-9023

出版社

AMER CHEMICAL SOC
DOI: 10.1021/acsanm.2c01212

关键词

carbon nanotubes; high-performance structural composites; thermoset resin; infusion model; nanoscale confinement

资金

  1. Airbus
  2. ANSYS
  3. Boeing
  4. Embraer
  5. Lockheed Martin
  6. Saab AB
  7. Saertex
  8. Teijin Carbon America through MIT's Nano-Engineered Composite aerospace STructures (NECST) Consortium
  9. National Aeronautics and Space Administration (NASA) Space Technology Research Institute (STRI [NNX17AJ32G]
  10. U.S. Army Research Laboratory
  11. U.S. Army Research Office through the Institute for Soldier Nanotechnologies (ISN) [W911NF-13-D-0001, W911NF-18-2-0048]
  12. U.S. Army Research Office [W911NF-07-D-0004]
  13. Office of Naval Research (ONR) [ONR. N000141712068]
  14. Department of Defense (DoD) through the National Defense Science and Engineering Graduate Fellowship (NDSEG) Program
  15. National Science Foundation [DMR-0819762]
  16. U.S. Department of Defense (DOD) [N000141712068] Funding Source: U.S. Department of Defense (DOD)

向作者/读者索取更多资源

This study reports the fabrication of high-volume fraction CNT nanocomposites and investigates their process-structure-property relationships. The research found that a diluted resin is required to achieve complete infusion into high-volume fraction A-CNT arrays. The addition of A-CNTs enhances the anisotropic mechanical properties.
Polymer matrix nanocomposites (PNCs) incorpo-rating high volume fractions (V-f in excess of 10 vol %) of aligned carbon nanotubes (A-CNTs) are promising for high-performance structural composite applications leveraging texture for multi -functionality and performance-to-weight ratios. However, to enable the manufacturing of scalable structures using A-CNT PNCs, nanoscale confinement and interfacial effects due to high A-CNT content in aerospace-grade polymer matrices need to be better understood. Here, we report the model-informed fabrication of high-V-f CNT PNCs to develop process-structure-property relationships, including a scaled film and laminate technique for A-CNT polymer laminates and the fabrication of microvoid-free and fully infused bis(maleimide) (BMI) and epoxy PNCs with high packing densities (or V-f) of biaxially mechanically densified millimeter-tall A-CNT array reinforcement (1-30 vol % corresponding to the average inter-CNT spacings of similar to 70 to 6 nm). A polymer infusion model developed from Darcy ' s law accurately predicts the time for resin to infuse into CNT arrays during capillary-assisted PNC processing, corroborated by experimental observations via X-ray microcomputed tomography and scanning electron microscopy showing that a diluted resin with similar to 10X lower viscosity than a neat resin is required to obtain complete infusion into high-V-f A-CNT arrays (10-30 vol %). For each tested A-CNT volume percent, the cured PNCs maintain vertical CNT alignment and glass transition temperature, and the decomposition onset temperature remains constant for epoxy PNCs but increases by similar to 8 degrees C for 30 vol % A-CNT-BMI PNCs compared to the neat resin. For both polymer matrix systems, a similar to 2X increase in the axial indentation modulus for 30 vol % A-CNT PNCs compared to that of a neat resin is measured, and no significant change in the transverse A-CNT modulus is shown experimentally and via modeling, indicating that reinforcement with A-CNTs at higher V-f values leads to enhanced anisotropic mechanical properties. Through the process-structure-property scaling relationships established here, this work supports the development of next-generation structures comprised of nanomaterials with enhanced performance and manufacturability.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.7
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据