Systems and method for fault protection
AssigneeGE Aviation Systems LLC
InventorsJames Angelo Elder, Kieran Sandeep Pancholi, Seyed Fazeli
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AssigneeGE Aviation Systems LLC
InventorsJames Angelo Elder, Kieran Sandeep Pancholi, Seyed Fazeli
Estimating the term…
A system and method for fault protection are described herein. An electrical power system architecture for an aircraft includes at least one electrical source, at least one electrical load, and a power distribution system connecting the at least one electrical source to the at least one electrical load. The power distribution system is grounded to an electrical ground of the aircraft through a high impedance grounding circuit and a plurality of protection devices are coupled electrically upstream and downstream of the high impedance grounding circuit. In some approaches, the electrical power system architecture includes a fault detection circuit configured to detect a fault and a controller to selectively open or close the plurality of protection devices based on the detected fault. In some approaches, an electrical wiring interconnection system separates positive power lines and negative power lines of the power distribution system for reducing line-to-line faults.
An electrical power system architecture for an aircraft, the electrical power system architecture, comprising:
A protection system for an electrical power distribution network of an aircraft, the electrical power distribution network including one or more electrical sources connected to one or more electrical loads through a power distribution system, the power distribution system connected to an electrical ground of the aircraft by a high impedance grounding circuit, the protection system comprising:
A method of responding to faults in an electrical power distribution network of an aircraft, the electrical power distribution network including a power distribution system grounded through a high impedance grounding circuit, and a plurality of protection devices, the method comprising:
Dependencies are inferred from the claim text.