The invention relates to a power communication architecture (100) for an aircraft comprising: a power electronics module management unit (103) that is capable of receiving input signals (104) and of delivering a current setpoint (106); at least one power electronics module (107) that is capable of receiving said current setpoint (106); at least one load (105) that is controlled by the at least one power electronics module (107); the power electronics module management unit (103) storing control laws (108) for controlling the one or more loads (105) allowing a current setpoint (106) to be transmitted according to the input signals (104) and said control laws (108). The invention also relates to an electrical distribution device for an aircraft comprising at least one such architecture.