Power communication architecture for an aircraft
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.
1. A power communication architecture for an aircraft comprising:
a power electronics module management unit (PEMMU) that is capable of receiving input signals and of delivering a current setpoint;
at least one power electronics module (PEM) that is capable of receiving said current setpoint; and
at least one load that is controlled by the at least one power electronics module;
the power electronics module management unit storing control laws for controlling the at least one load allowing a current setpoint to be transmitted according to the input signals and said control laws.
2. The power communication architecture according to claim 1 , further comprising an electrical network management unit (ENMU) that is configured to communicate with the power electronics module management unit and to set up associations between the at least one power electronics module and the at least one load.
3. The power communication architecture according to claim 2 , further comprising a contactor matrix that is configured by the electrical network management unit, said contactor matrix being capable of communicating with each power electronics module and each load.
4. The power communication architecture according to claim 2 , wherein the electrical network management unit is comprised within the power electronics module management unit.
5. The power communication architecture according to claim 1 , wherein the at least one current sensor is incorporated within the power electronics module management unit.
6. The power communication architecture according to claim 1 , wherein the control laws of the power electronics module management unit incorporate the current loops of the power electronics modules.
7. An electrical distribution device for an aircraft comprising at least one power communication architecture according to claim 1 .