Fig. 16
Diagram of the flow of currents in a node \(\:\text{k}\) of the power supply system of an electrified aircraft, where: \(\:{\text{U}}_{\text{k}\text{f}}\)- node voltage \(\:\text{k}\); \(\:{\text{U}}_{\text{l}\text{f}}\)- voltage in node l; \(\:{\text{J}}_{\text{k}\text{l}}\)- current flowing between nodes \(\:\text{k}\) and \(\:\text{l}\); \(\:{\text{J}}_{\text{k}}\)- receiving current in node \(\:\text{k}\); \(\:{\text{J}}_{\text{k}\text{g}}\)- generator current in node \(\:\text{k}\); \(\:{\text{Z}}_{\text{k}\text{l}}\), \(\:{\text{Y}}_{\text{k}\text{l}}\)- impedance and admittance of the element connecting nodes \(\:\text{k}\) and \(\:\text{l}\); \(\:{\text{U}}_{\text{k}\text{o}}\), \(\:{\text{U}}_{\text{l}\text{o}}\)- admittance of transverse branches in nodes \(\:\text{k}\) and \(\:\text{l}\); \(\:{\text{Y}}_{\text{k}}\)- reception replacement admittance at the node \(\:\text{l}\).
