Baseline limits for conducted and radiated EMI are specified for voltage ratings lower than what is required for the propulsive power electrical system. Therefore, it is a project objective to identify which should be the new baseline, validate the approach with the airframers and interact with regulatory and standardisation agencies to promote its adoption.
- Expected results: Propulsion electric suction of the aircraft power system could possibly adopt different values in terms of EMI limits when compared to the rest of the aircraft power system, especially in terms of differential mode noise.
- Success evaluation: In this objective, it is fundamental to reach a consensus with the entities mentioned in the objective description such that the solutions are safe in terms of equipment operation and human health.
