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Next, optimization calculations were performed for a composite panel with a core madę of two-phase composite, in which the average value of the thermal energy was minimized. Likewise, in this case the obtained results were compared with laminates in the form of three panels with the same boundary conditions. The results of the average value of the thermal energy were the lowest in the composite piąte [Nie2014a]. When the minimization of the average thermal energy and strain energy was performed simultaneously, with equal scales for both energies, the distribution of the control variable was similar to the distribution of the control variable in the case when only the average thermal energy was minimized. This leads to a conclusion that thermal energy dominates in this calculation case. The reverse is true in a situation when results of the minimization of the average thermal energy and strain energy are analysed simultaneously with different scales.
The last stage of the research was to carry out the analysis of dynamie parameters of the thermally optimal composite panel. The eigenfreąuency, the freąuency response and the modę shapes for the particular eigenvalue were determined. The analysis of dynamie properties was carried out also for three types of laminate panels. For most of the subseąuent eigenvalues of the thermally optimal composite, the values of those eigenvalues were higher than the eigenvalues for the laminate panels [Nie2014b].
The proposed methods and composite structures with thermal boundary conditions or thermo-mechanical boundary conditions can be applied in design and construction of: a) optimal cooling devices (radiators); b) electronic devices; c) building elements (e.g. bricks with inereased insulation, along with simultaneous inerease in strength); d) battery electrodes for energy recovery in the case of smali temperaturę differences using the gaWanic effect.
The results obtained during the numerical research and their analysis lead to a conclusion that the thesis and the aims of the dissertation have been confirmed. Conclusions from the performed numerical research show that the use of computational methods such as the optimization of topology structure of two-phase materials allow to achieve composite materials with better thermal properties than thermal properties in classic layer composites (laminates). The achieved materials and composite structures can vent the heat generated by the device better and thus cool it. In the optimized structures, the distribution of the temperaturę and thermal energy was minimized, which allowed to achieve morę optimal structures, different from those commonly known. Literaturę studies show that similar structures are analysed in some automotive concerns. Further research will enable their use in other areas related to thermal issues.
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