Damage to inverse hybrid laminate structures: an analysis of shear strength test

• Autorzy: Frankiewicz Mariusz , Ziółkowski Grzegorz , Dziedzic Robert , Osiecki Tomasz , Scholz Peter

Identyfikatory

DOI

10.2478/msp-2022-0016

• Języki publikacji: EN

Abstrakty

EN

Hybrid laminates with continuous fiber reinforcement, such as glass reinforced aluminium laminate (GLARE), aramid reinforced aluminum laminate (ARALL), or carbon reinforced aluminum laminate (CARALL), have been developed to increase the lightweight potential and fatigue resistance applied for aircraft structures. However, the use of thermosetting matrices imposes material limitations regarding recycling, malleability, and manufacturing-cycle times. The inverse hybrid laminate approach is based on a continuous fiber-reinforced thermoplastic matrix, in which a metal insert is integrated. For efficient manufacturing of the novel composites in high-volume production processes, conventional sheet metal–forming methods have been applied. It helped to reduce the cycle times and the costs of the forming equipment compared to currently used hybrid laminate-processing technologies. The present study analyzes the damage to the inverse hybrid laminate structures resulting from the interlaminar shear strength test. The tests were performed for eight laminate material configurations, which differed by the type and directions of the reinforced glass and carbon fibers in the polyamide matrix and the number of the fiber-reinforced polymer (FRP) layers in the laminates. Industrial computed tomography and scanning electron microscopy were used for analysis. Observed damages, including fiber–matrix debonding, fiber breakages, matrix fractures, interfacial debonding, and delamination in selected areas of the material, are strictly dependent on the laminate configurations. FRP layers reinforced by fibers perpendicular to the bending axis presented better resistance against fractures of the matrix, but their adhesion to the aluminum inserts was lower than in layers reinforced by fibers parallel to the bending axis.

Słowa kluczowe

EN

interlaminar strength; fibre metal laminate; composite material; hybrid laminate

• Wydawca: De Gruyter
• Czasopismo: Materials Science Poland
• Rocznik: 2022
• Tom: Vol. 40, No. 1
• Strony: 130--144
• Opis fizyczny: Bibliogr. 29 poz., rys., tab.

Twórcy

autor

Frankiewicz Mariusz

• Centre for Advanced Manufacturing Technologies – Fraunhofer Project Center, Department of Laser Technologies, Automation and Production Management, Faculty of Mechanical Engineering, Wroclaw University of Science and Technology, Lukasiewicza 5, 50-371 Wroclaw, Poland

autor

Ziółkowski Grzegorz

• Centre for Advanced Manufacturing Technologies – Fraunhofer Project Center, Department of Laser Technologies, Automation and Production Management, Faculty of Mechanical Engineering, Wroclaw University of Science and Technology, Lukasiewicza 5, 50-371 Wroclaw, Poland

autor

Dziedzic Robert

• Centre for Advanced Manufacturing Technologies – Fraunhofer Project Center, Department of Laser Technologies, Automation and Production Management, Faculty of Mechanical Engineering, Wroclaw University of Science and Technology, Lukasiewicza 5, 50-371 Wroclaw, Poland

autor

Osiecki Tomasz

• Institute of Lightweight Structures and Polymer Technology, Technische Universität Chemnitz, Reichenhainer Str. 31-33, 09126 Chemnitz, Germany

autor

Scholz Peter

• Fraunhofer Institute for Machine Tools and Forming Technology IWU, Reichenhainer Str. 88, 09126 Chemnitz, Germany

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