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Preparation and properties of Fibre–Metal Laminates based on carbon fibre reinforced PMR polyimide
Affiliation:1. Sapienza Università di Roma, Dipartimento di Ingegneria Meccanica e Aerospaziale, Via Eudossiana, 18, 00184 Roma, Italy;2. Università degli Studi Roma Tre, Dipartimento di Ingegneria, Via V. Volterra 62, 00146 Roma, Italy;1. Faculty of Mechanical Engineering, Universiti Teknologi Malaysia (UTM), Skudai, Johor 81310, Malaysia;2. Department of Physics Energy Engineering, Surya University, Jl. Boulevard Gading Serpong Blok O/1, Summarecon Serpong Tangerang 15810 Indonesia;3. Department of Aerospace Engineering, Khalifa University of Science, Technology and Research (KUSTAR), PO Box 127788, Abu Dhabi, United Arab Emirates;4. Department of Engineering, University of Liverpool, Liverpool L69 3BX, United Kingdom
Abstract:A novel Fibre–Metal Laminates (FMLs) based on carbon fibre reinforced PMR polyimide were prepared using a hot press process in this paper. Pre-treatment on the titanium surface were conducted prior to laminating. Scanning Electron Microscope (SEM) were used to observe the morphologies of the titanium and the cross-sections of the FMLs. SEM results showed that micro-roughness structures were formed on the titanium surface after anodization. This structure enhanced the interlaminar bond strength between titanium and polyimide. Flexural and Interlaminar shear (ILSS) tests showed that the FMLs possess excellent flexural and interlaminar properties at both room temperature and elevated temperature. Thermostability tests proved that the FMLs based on carbon fibre reinforced PMR polyimide offered excellent thermal properties. It is shown that no delamination appears between titanium layer and the fibre-reinforced polyimide layer after 1000 times thermal shock.
Keywords:A  Hybrid  A  Laminates  B  Thermal properties  E  Surface treatments
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