The effect of an elastomer interlayer thickness variation on the mechanical properties of Fiber-Metal-Laminates
Source abstract
Abstract
Abstract Fiber-Metal-Laminates with elastomer interlayers (FMEL) consisting of CFRP and Al 2024-T3 were manufactured with standard and thin elastomer interlayers to evaluate the mechanical properties of the FMELs. The elastomer layer thickness reduction was necessary to increase lightweight potential of the laminate. The layer thickness was reduced using a new process step. The thin elastomer layers were obtained using a solvent and deposited on the aluminum core layer before manufacturing the laminate. The effects of the additional manufacturing step and the thickness variation on the mechanical properties of the laminate were examined focusing on interfacial and flexural behavior . The FMEL were compared to FML to determine the impact of the elastomer interlayer. The FMEL with thin elastomer interlayers exhibited a higher flexural stiffness but lower strain to failure than the FMEL accounting for the lower deformation in the thinner elastomer layer. The interfacial properties showed a satisfactory quality after the solution step, which was presented by identical interfacial shear strength compared to the FMEL. The FMEL with thin elastomer interlayers could be manufactured through a solution step and the mechanical properties led to the desired results.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Mechanical Behavior of Composites · Fiber-reinforced polymer composites · Additive Manufacturing and 3D Printing Technologies
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (17)
Show source-provided references
1. Development of fiber metal laminates for advanced aerospace structures10.1016/S0924-0136(00)00411-8 ↗
2. Vlot · 2001
3. Wang W-X, Takao Y, Matsubara T. Galvanic corrosion-resistant carbon fiber metal laminates. In 16th International Conference on Composite Materials Japan.
4. Thermal residual strains in carbon fibre-reinforced aluminium laminates10.1016/0010-4361(94)90223-2 ↗
5. Adhesion properties of novel corrosion resistant hybrid structures10.1016/j.ijadhadh.2013.12.009 ↗
6. Ageing of corrosion resistant steel/rubber/composite hybrid structures10.1016/j.ijadhadh.2013.12.008 ↗
7. Optimization of corrosive properties of carbon fiber reinforced aluminum laminates due to integration of an elastomer interlayer10.4028/www.scientific.net/KEM.742.287 ↗
8. The impact of environmental stress on the mechanical behavior of fiber-metal-laminates with elastomer interlayers (fmel)
9. Liebig WV, Sessner V, Weidenmann KA, Kärger L. Numerical and experimental investigations of the damping behaviour of hybrid CFRP-elastomer-metal laminates. Compos Struct.
10. Luukkonen A, Sarlin E, Villman V, Hoikkanen M, Vippola M, Kallio M, et al. Heat generation in dynamic loading of hybrid rubber-steel composite structure.
11. Impact properties of novel corrosion resistant hybrid structures10.1016/j.compstruct.2013.10.023 ↗
12. High-resolution photoelectron spectroscopy study of degradation of rubber-to-brass adhesion by thermal aging10.1016/j.apsusc.2012.12.025 ↗
13. Stoll M, Weidenmann K. Materials selection for a fiber-metal-laminate with elastomer interlayers. In Proceedings of 21st ICCM.
14. characterization of interface properties of fiber-metal-laminates (fml) with optimized surfaces
15. The edge shear test – an alternative testing method for the determination of the interlaminar shear strength in composite materials
16. Manufacturing of glare parts and structures10.1023/A:1025589230710 ↗
17. Din en iso 14125: 2011. Faserverstärkte Kunststoffe Bestimmung der Biegeeigenschaften (ISO 14125: 1998+ Cor. 1: 2001+ Amd. 1: 2011).