2021
DOI: 10.1016/j.compositesb.2021.108737
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Experimental study on CF/PEEK thermoplastic fastener: Effects of fastener matrix crystallinity and fibre content on the strength of single-lap joint

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Cited by 31 publications
(12 citation statements)
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“…%—CF, 60 vol. %—PEEK–binder) was identified through the literature analysis and the results of the previous studies by the authors [ 45 , 46 , 47 ].…”
Section: Methodsmentioning
confidence: 99%
“…%—CF, 60 vol. %—PEEK–binder) was identified through the literature analysis and the results of the previous studies by the authors [ 45 , 46 , 47 ].…”
Section: Methodsmentioning
confidence: 99%
“…Owing to their superior features, such as high specific strength and stiffness, high specific moduli, damage tolerance, and environmental resilience, carbon-fiber-reinforced thermoplastic (CFRTP) composites have been widely used in the aerospace industry [ 1 , 2 , 3 , 4 , 5 ]. Composite components are divided into numerous parts as per the requirements of structural design, manufacture, and maintenance of composites, as well as the limitations of the integrity molding technology.…”
Section: Introductionmentioning
confidence: 99%
“…The use of metallic fasteners undermine the potential of such assemblies to take advantage of the beneficial specific weight of composite materials. CFRP fasteners have shown great potential for replacing the conventional metallic fasteners in the hybrid bonded/fastened joints configurations [3]- [7]. They can provide with a weight benefit against using metallic fasteners, they are not susceptible to galvanic corrosion and, depending on the fastener design, they can exhibit higher specific strength compared to their metallic counterparts.…”
Section: Introductionmentioning
confidence: 99%
“…Similarly, Fortier et al manufactured and reshaped thermoplastic composite rivets from pultruded rods [6]. Yao et al [7] extend the research to study the effect of matrix crystallinity and fibre content on fastener strength. The thermoplastic composite fasteners in the studies above have demonstrated their potential for applications in the aerospace industry, with the drawback of requiring complicated moulds and a time-consuming process for their application, which raises the production costs.…”
Section: Introductionmentioning
confidence: 99%