In the aerospace field, transportation electrification is considered as one of the main solutions that allow the reduction of greenhouse gas levels in the air and slow down the climate change. One of the ways that can allow to reach this goal for electrified systems is the voltage increase and reduce the volume of system onboard. This approach induces consequently induce very high electrical constraints on the insulation materials used in the power conversion systems. These local high electric fields can cause premature failure, by partial discharge activity and insulation breakdown. In order to efficiently reduce the electrical stresses, the design of new system of stress-control encapsulation seem be promising it does not impact the volume of the power module and has a negligible impact on the overall mass.
An approach based on the use of low filler ratio composites and the monitoring of the particles (SrTiO3, BaTiO) density by the electric potential to tailor around critical areas where the electric field is high has been validated on simple configuration between two adjacent electrodesErreur ! Source du renvoi introuvable.Erreur ! Source du renvoi introuvable.. In addition, this approach has been used successfully to apply the FGM on various substrate electrodes of a power module by using a removable electrode in front of the substrate Erreur ! Source du renvoi introuvable.. In this paper, the impact of the applied electric potential and its duration will be presented in order to evaluate and optimize the process to allow apply an electrodeposition with a homogenous thinness of stress-control layer.