Interface engineering of carbon fiber composites using CNT: A review

被引:22
作者
Sahu, Renuka [1 ]
Ponnusami, Sathiskumar A. [2 ]
Weimer, Christian [3 ]
Harursampath, Dineshkumar [1 ]
机构
[1] Indian Inst Sci, Dept Aerosp Engn, Bangalore 560012, India
[2] Univ London, Dept Mech Engn & Aeronaut, London, England
[3] Airbus Def & Space Gmbh, Cent Res & Technol CRT, Taufkirchen, Germany
关键词
carbon fiber; CNT; effective properties; electrical and thermal properties; fuzzy fiber; interface; NANOTUBE-REINFORCED POLYMER; PREDICTING MECHANICAL-PROPERTIES; INTERLAMINAR FRACTURE-TOUGHNESS; PULSED-LASER DEPOSITION; THERMAL-PROPERTIES; FIBER/EPOXY COMPOSITES; HIERARCHICAL COMPOSITES; TENSILE-STRENGTH; EPOXY COMPOSITES; ELECTROPHORETIC DEPOSITION;
D O I
10.1002/pc.27772
中图分类号
TB33 [复合材料];
学科分类号
摘要
This paper aims to explore the potential of carbon nanotubes (CNTs) in enhancing the structural capability and multifunctionality of carbon fiber composites in aerospace applications, primarily by focusing on interfacial applications. The conventional method of dispersing CNTs in a matrix is not fully efficient in exploiting the mechanical and multifunctional performance of CNTs. Hence, the use of CNTs at the interface or as a coating on the surface of carbon fibers has been suggested as a means of achieving multifunctionality, in addition to enhanced mechanical performance. The paper presents an overview of the various processes for growing CNTs on carbon fiber surfaces and examines the effects of CNT geometry and growth parameters on the properties of grafted fibers and their composites. Furthermore, it discusses the potential improvements in thermal and electrical conductivity achievable by incorporating CNTs at the interface, as well as the benefits of using CNTs as a sizing layer for carbon fibers, including enhanced fracture toughness and resistance to delamination.
引用
收藏
页码:9 / 42
页数:34
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