Influence of the Selected Physical Modifier on the Dynamical Behavior of the Polymer Composites Used in the Aviation Industry |
| |
| Authors: | Ewelina Kosicka Marek Borowiec Marcin Kowalczuk Aneta Krzyzak Robert Szczepaniak |
| |
| Institution: | 1.Department of Production Engineering, Lublin University of Technology, 20-618 Lublin, Poland;2.Department of Applied Mechanics, Lublin University of Technology, 20-618 Lublin, Poland; (M.B.); (M.K.);3.Department of Airframe and Engine, Military University of Aviation, 80-521 Dęblin, Poland; (A.K.); (R.S.) |
| |
| Abstract: | In this research, an analysis of polymer composite with the matrix of L285-cured hardener H286 and six reinforcement layers of carbon fabric GG 280 T was provided. It involved a comparison of the dynamical behavior responses for three cases of composite structures in the context of the presence of the mass share modifier. The samples with the addition of a physical modifier with varying mass percentages were investigated by being subjected to dynamic tests with specific parameters, i.e., constant excitation amplitude and vibration frequency in the vicinity of the base resonance zone. The analysis allowed for indicating the relationship between the composition of the prepared composites and their dynamic response via stiffness characteristics. In addition, the investigation resulted in determining the range of harmful dynamical operating conditions, which may contribute to damage to the composite structures. |
| |
| Keywords: | composite material vibrations resonance zone |
|
|
