Abstract: A system and method for an arc fault detection system for aircraft wiring system is disclosed. Upon detection of arc fault events, the system transmits a signal that may be sent to an existing circuitry of the aircraft electrical system, which disconnects the power to the circuits, thereby extinguishing the arc. The system can be either utilized as a stand-alone system or incorporated into existing products or systems. When an arc event occurs on a power cable, a broadband noise event is similarly induced upon the affected cable. The system first uses a pick-up coil (15) to sense and pick up this broadband signal from the power cable (5) of the wiring system, and then amplifies (17) the signal. The amplified signal is applied to a high-pass filter (20) to only pass frequency components above a predetermined frequency.

Abstract: A system and method for an arc fault detection system for aircraft wiring system is disclosed. Upon detection of arc fault events, the system transmits a signal that may be sent to an existing circuitry of the aircraft electrical system, which disconnects the power to the circuits, thereby extinguishing the arc. The system can be either utilized as a stand-alone system or incorporated into existing products or systems. When an arc event occurs on a power cable, a broadband noise event is similarly induced upon the affected cable. The system first uses a pick-up coil (15) to sense and pick up this broadband signal from the power cable (5) of the wiring system, and then amplifies (17) the signal. The amplified signal is applied to a high-pass filter (20) to only pass frequency components above a predetermined frequency.