A power supply system comprising: a first converter module comprising an AC/DC converter and being arranged to produce an intermediate voltage from an input voltage; a second converter module comprising a DC/DC converter and being controllable to use the intermediate voltage to produce selectively at least two distinct output voltage levels; and a control unit arranged to acquire a flight parameter representative of the flight phase and/or of the altitude, and to control the power supply system in such a manner that the second converter module delivers to each electrical system a power supply voltage that depends on the flight parameter and on said electrical system, and that is equal to one of the output voltage levels.
CONFIGURABLE POWER SUPPLY SYSTEM
13.06.2024
Patent
Elektronische Ressource
Englisch
Configurable device for aviation power supply test and aviation power supply test method
Europäisches Patentamt | 2024