SYSTEM FOR CONTROLLING THE ELECTRICAL POWER SUPPLY OF AN AIRCRAFT

摘要

A system for controlling electrical power supply of an aircraft includes at least two control boards and at least two switching members. Each switching member is connected to each control board. Each control board includes a processor. Each processor is configured to determine a command for switching states of switch contacts of each switching member and to determine information relating to validity of each switching command. Each switching member includes a transmitter to determine a command to be transmitted to a detector to detect parallelization, a power actuator configured to transmit a power signal to the switch contacts depending on the command received from the detector, and switch contacts configured to selectively open or close an electrical power supply line. The command is selected from the switching commands and the information relating to the validity of each switching command.

主权项

1. A system for controlling electrical power supply of an aircraft, the system comprising:
at least two control boards; and at least two switching members, each switching member being connected to each control board, wherein:
each control board comprises a processor, each processor configured to determine a command for switching states of switch contacts of each switching member and to determine information relating to validity of each switching command; andeach switching member comprises a transmitter to determine a command to be transmitted, the command selected from the switching commands and the information relating to the validity of each switching command, to a detector to detect parallelization, a power actuator configured to transmit a power signal to the switch contacts depending on the command received from the detector, and switch contacts configured to selectively open or close an electrical power supply line.