ELECTRICAL ARCHITECTURE FOR CONTROLLING CONVERTERS AND AIRCRAFT COMPRISING THE ARCHITECTURE

摘要

The invention relates to an electrical architecture for controlling inverters and an aircraft comprising the architecture. The electrical architecture comprises: several converters that can operate independently of each other, each converter being intended to supply a load, associated with each converter / load pair: a load loop, comprising at least one sensor measuring a characteristic parameter of the operation of the load, an operating servo module, receiving a load operating instruction and information from the operating sensor, the operating servo module controlling a current setpoint of the converter in question so that the output information the operating sensor follows the operating instruction. According to the invention, the operating servo module is common to the converters.