SYSTEM AND METHOD FOR POWER DISTRIBUTION

摘要

A direct current (DC) power distribution system is provided for an aircraft. The system includes a DC system bus configured to carry electrical power from a source of electrical power to a plurality of electrical loads. The electrical loads are onboard the aircraft. The DC system bus includes a load side. The system includes a plurality of power converter modules that are electrically coupled in series to the DC system bus on the load side of the DC system bus. The power converter modules are configured to be electrically attached to corresponding sub-sets of the electrical loads. At least one of the power converter modules is configured to be short circuited in response to a fault such that the at least one power converter module does not supply electrical power to the corresponding subset of the electrical loads.