Quasi-static and fatigue bending behavior of a continuous fiber-reinforced thermoplastic/metal laminate

Zopp, Camilo; Dittes, Axel; Nestler, Daisy; Scharf, Ingolf; Kroll, Lothar; Lampke, Thomas

doi:10.1016/j.compositesb.2019.107043

Cited by 28 publications

(16 citation statements)

References 28 publications

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“…Selecting a matrix material with excellent property, safety, and environmental protection is more conducive to achieving energy conservation and environmental protection. ermoplastic FMLs have higher toughness and good impact resistance and are recyclable [23,24,137]. From the current research, there are few studies on the tensile property and fatigue property of the surface-treated thermoplastic FMLs.…”

Section: Development Trend Of Fmlsmentioning

confidence: 98%

Research Progress on Interlaminar Failure Behavior of Fiber Metal Laminates

Chen

Wang

2020

Advances in Polymer Technology

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Fiber metal laminate (FML) is a kind of lightweight material with excellent mechanical properties combining advantages of metal laminates and fiber reinforced composites. It has been widely used in the aerospace and transportation fields and is especially used as structural material such as aircraft skins, wings, and tails. However, under complex service conditions, interlaminar failure in FMLs greatly reduced mechanical properties of the material, even leading to serious economic and safety disasters. The failure and destruction of important structural parts of aircraft and other manned transportation vehicles are extremely unsafe for people. Therefore, it is of great significance to summarize the interlaminar failure behavior of FMLs and find ways to avoid these defects. This review paper is a collection of various researches done by many groups, which systematically discuss the interlaminar failure behaviors and their control methods of FMLs. The application status of several common FMLs in aircraft structures was given. The common interlaminar failure modes of FMLs and the testing and evaluation methods of interlaminar properties were stated. The failure mechanisms and the corresponding control methods were analyzed. Finally, the future developments of FMLs were also discussed by the authors. Through this review article, readers can obtain new research progress about the control method, the mechanism and future development on the failure behavior of FMLs in a more efficient way.

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Section: Development Trend Of Fmlsmentioning

confidence: 98%

Research Progress on Interlaminar Failure Behavior of Fiber Metal Laminates

Chen

Wang

2020

Advances in Polymer Technology

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“…[ 8 ] The thermoplastic matrix are typically made up of polyaminde (PA), polypropylene (PP), thermoplastic polyurethanes (TPU), and polyetheretherketone (PEEK), and so forth. [ 9 ] Among these materials, PP is one of the most popular resin in vehicle industry, possesses the advantage of low price, rapid processing, recyclability, and so forth. [ 10 ] Continuous glass fiber reinforced PP (PP/GF) has been used as automobile structural parts.…”

Section: Introductionmentioning

confidence: 99%

Mechanical performance of a novel glass fiber reinforced maleic anhydride grafted polypropylene composite and its thermoplastic‐based fiber metal laminates

et al. 2022

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In this article, continuous glass fiber reinforced thermoplastic prepreg is proposed using maleic anhydride grafted polypropylene (MAPP) as the matrix resin. The compression molding parameters and plying sequences are optimized. Under the process parameters of 155 C and 15 MPa, both the tensile and flexural properties achieve the maximum values, and the plying sequence of (0 /90 ) possess a balanced mechanical performance. Then, MAPP/GF/Al fiber-metal laminates are further fabricated in two stacking configurations of 2/1 and 3/2. The mechanical results showed that the tensile and bending strength were basically maintained, while the modulus are significantly enhanced by 114.9% and 135.4% in 2/1 and 3/2 fiber metal laminates (FMLs) in contrast with MAPP/GF controls. In addition, the large deflection behavior in bending test for FMLs suggest that MAPP/GF and aluminum alloy show a synergy deformation due to the good bonding between metal layer and thermoplastic resin. The optical microstructure also revealed that the interlaminar adhesion are well joined between FML constituents. The findings in this study are important from a design viewpoint of FMLs because of the lower material cost, less processing time, and good lightweight effect, which potentially be tailored to use as structural parts in automobile applications.

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“…Jaroslaw et al 32 stated that the size of the affected area depends on the size of the colliding member and larger collisions cause thematic deformations without creating critical cracks and delamination in these plates. Zop et al 33 pondered the quasi-static and the bending behavior of FMLs. The several layers studied in their study were made of carbon fiber-reinforced polyamide plates, aluminum plates, and glass fiber-reinforced polyamide plates.…”

Section: Introductionmentioning

confidence: 99%

Experimental investigation on mechanical behavior of fiber–metal laminates reinforced by hybrid carbon nanotubes and nanosilica under quasi-static pressure load

Saleh

Tooski

Khorshidvand

et al. 2022

Proceedings of the Institution of Mechanical Engineers, Part C:

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In this study, the effect of carbon nanotubes (CNT) and silica nanoparticles on quasi-static behavior of fiber–metal laminates (FML) has been experimentally scrutinized. FML consists of two layers of aluminum alloy plates and four composite layers including CNT/nanosilica-reinforced epoxy resin and glass fibers. The effect of weight percentage of carbon nanotube and nanosilica incorporated and their weight ratio in resin epoxy on the performance of FMLs against quasi-static compressive load has been considered. Furthermore, the design of experiments method and response surface methodology have been put into practice to develop an accurate mathematical relationship between the input parameters and the response variable. After designing and performing the experiments based on analysis of variance, a mathematical model corresponding to the real process is obtained. Moreover, the presented model has been validated by statistical methods. The results of this study indicate that the energy absorption capacity of these materials significantly increase through adding CNT to the FML, the highest failure force of 11.64 kN was obtained for FLMs comprising 0.6 wt.% of CNT and 3 wt.% of SiO2. An improvement of 27.88% and 45.86% in the absorbed energy and failure force was achieved, respectively, by adding 3 wt.% of SiO2 and 0.6 wt.% of CNT to FLM compared to pristine FLM.

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Quasi-static and fatigue bending behavior of a continuous fiber-reinforced thermoplastic/metal laminate

Cited by 28 publications

References 28 publications

Research Progress on Interlaminar Failure Behavior of Fiber Metal Laminates

Research Progress on Interlaminar Failure Behavior of Fiber Metal Laminates

Mechanical performance of a novel glass fiber reinforced maleic anhydride grafted polypropylene composite and its thermoplastic‐based fiber metal laminates

Experimental investigation on mechanical behavior of fiber–metal laminates reinforced by hybrid carbon nanotubes and nanosilica under quasi-static pressure load

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