초록 ▼

Apparatus and methods for detecting high level arc faults in aircraft power systems are disclosed. One embodiment of the invention with reduced susceptibility to nuisance trips includes three low pass filters each having an output connected to a threshold detector. In addition, a three input compara

Apparatus and methods for detecting high level arc faults in aircraft power systems are disclosed. One embodiment of the invention with reduced susceptibility to nuisance trips includes three low pass filters each having an output connected to a threshold detector. In addition, a three input comparator is connected to an output of each of the threshold detectors and a fault verification circuit is connected to an output of the three input comparator. An embodiment of the method of the invention for detecting arc faults in three phase aircraft power systems involves detecting at least one of the three phases having a current exceeding a predetermined threshold, detecting differences between the three phases and generating a signal indicative of difference being detected between the three phases for a time period exceeding a predetermined duration.

대표청구항 ▼

What is claimed is: 1. An arc fault detector for detecting arc faults in three phase aircraft power systems, comprising: three full wave rectifiers, each of the three full wave rectifiers having an input of a load current in the three phase power system and having an output connected to one of a pl

What is claimed is: 1. An arc fault detector for detecting arc faults in three phase aircraft power systems, comprising: three full wave rectifiers, each of the three full wave rectifiers having an input of a load current in the three phase power system and having an output connected to one of a plurality of threshold detectors; a three input comparator having at least three inputs, each of the least three inputs being connected to an output of one of the plurality of threshold detectors; and a fault verification circuit connected to an output of the three input comparator. 2. The arc fault detector of claim 1, wherein each of the plurality of threshold detectors comprises: a first comparator having: a first input connected to an output of one of the full wave rectifiers; a second input connected to a signal indicative of a predetermined threshold; and an output. 3. The arc fault detector of claim 2, wherein each of the plurality of threshold detectors further comprise an integrator configured to integrate the output of the first comparator. 4. The arc fault detector of claim 1, wherein the three input comparator is configured to generate a signal indicative of the outputs of any two of the threshold detectors differing by more than a predetermined amount. 5. The arc fault detector of claim 1, wherein the fault verification circuit comprises: an integrator connected to the output of the three input comparator; and a comparator connected to the output of the integrator and configured to generate a signal indicative of the detection of a fault, when the output of the integrator exceeds a predetermined threshold. 6. An arc fault detector for detecting arc faults in three phase aircraft power systems; comprising: means for generating three load currents in the three phase system, where each load current in the three phase system is indicative of each of the three phases; means for rectifying the generated load currents; mean for comparing the three rectified load currents; means for generating a signal in response to the three rectified load currents differing for a time period exceeding a predetermined duration; and means for detecting that one of the three rectified currents exceeds a predetermined threshold, wherein the means for generating a signal in response to the three rectified load currents differing for a time period exceeding a predetermined duration generates a signal if at least one of the three filtered load current exceeds the predetermined threshold. 7. A method of detecting arc faults in three phase aircraft power systems, comprising: detecting when at least one of the three load currents in the three phase power system has a current exceeding a predetermined threshold; detecting differences between the three load currents; and generating a signal indicative of differences being detected between the three load currents for a time period exceeding a predetermined duration; wherein the detecting differences comprises generating load currents in the three chase system, each load current indicative of one of the three phases and generating a signal indicative of at least two of the three load currents differing by more than a predetermined amount, and detecting differences further comprises continuously monitoring the load currents indicative of the three phases. 8. The method of claim 7, wherein detecting differences further comprises continuously sampling the load currents indicative of the three phases. 9. The method of claim 7, wherein generating a signal indicative of at least two of the three load currents differing by more than a predetermined amount comprises integrating over at least one cycle each of the load currents indicative of each of the three phases. 10. The method of claim 9, wherein generating a signal indicative of at least two of the three load currents differing by more than a predetermined amount further comprises: comparing the magnitude of each load current to a predetermined threshold; and generating a signal for each load current indicative of the magnitude of the load current relative to the threshold. 11. The method of claim 7, wherein generating a signal indicative of differences being detected between the three load currents for a time period exceeding a predetermined duration comprises: generating a signal indicative of the time period during which at least two of the three load currents differ by more than a predetermined amount; and comparing the generated signal to a signal indicative of the predetermined duration.