Power sharing in an aircraft using centralized control

An installation for exchanging power in an aircraft, comprising:

• a voltage bus designed to present a bus voltage;
• a low-pressure electromechanical converter designed to exchange power between the voltage bus and a low-pressure body of a turbomachine of the aircraft;
• a high-pressure (HP) electromechanical converter designed to exchange power between the voltage bus and a high-pressure body of the turbomachine of the aircraft;
• and
• for each electromechanical converter:
• a voltage control module designed to receive a voltage setpoint (VDC*), the same for both voltage control modules (130BP, 130HP), and to receive a voltage setpoint, the same for both voltage control modules, and to control the bus voltage by determining an exchange setpoint for the electromechanical converter in question, and
• a control module designed to control the electromechanical converter in question, so that the electromechanical converter in question complies with the exchange setpoint;
• wherein it further comprises a power adjustment module designed, for each of the electromechanical converters, for:
• determining a voltage correction, and
• applying, in the voltage control module associated with the electromechanical converter in question, the voltage correction to the voltage setpoint so that the voltage control module controls the bus voltage to the corrected voltage setpoint.