Diode fault detection
A power delivery system includes a controller, configured to receive a voltage indication signal indicating a measured voltage of a battery management system and to determine whether first and second diodes of the battery management system are faulty based on the voltage indication signal. The controller is also configured to respectively receive first and second current indication signals from first and second current sensors of the battery management system and to determine whether the first and second diodes of the first battery management system are faulty based on the first and second current indication signals.
1. A power delivery system for an aircraft, the power delivery system comprising:
a first battery management system and a second battery management system, each comprising:
a battery system,
at least one diode configured to conduct current from the battery system to a power supply node along a current path,
a first switch and a second switch, each configured to selectively conduct current from the battery system to the at least one diode;
one or more sensors configured to generate a signal based on at least one of a sensed current and a sensed voltage of the current path; and
a controller configured to:
receive the signal from the first battery management system or the second battery management system, and
determine whether the at least one diode of the first battery management system or the second battery management system is faulty based at least in part on the signal.
2. The power delivery system of claim 1 , wherein the controller is configured to control a conductivity of the first switch of at least one of the first battery management system and the second battery management system.
3. The power delivery system of claim 2 , wherein the controller is configured to control the conductivity of the first switch of at least one of the first battery management system and the second battery management system so as to conditionally test the at least one diode.
4. The power delivery system of claim 1 , wherein the controller of the first battery management system performs operations comprising:
causing at least one of the first switch and the second switch of the first battery management system to be conductive, whereby current from the battery system of the first battery management system is conducted to a power supply conductor.
5. The power delivery system of claim 4 , wherein the controller of the second battery management system performs operations comprising:
causing the first switch and the second switch of the second battery management system to be nonconductive;
determining a voltage of the second battery management system; and
determining whether the at least one diode of the second battery management system has a short based on the determined voltage of the second battery management system.
6. The power delivery system of claim 1 , wherein the controller of the first battery management system performs operations comprising:
causing the first switch of the first battery management system to be conductive, whereby current from a battery of the battery system is conducted to a first power supply node of the first battery management system;
causing the first switch and the second switch of the first battery management system to be nonconductive;
determining a voltage of the first power supply node while the first switch and the second switch of the first battery management system are nonconductive; and
determining whether the diode of the first battery management system has an open based on the determined voltage of the first power supply node.
7. A method of operating a power delivery system for an aircraft, the power delivery system comprising a first battery management system and a second battery management system, each comprising a battery system, at least one diode configured to conduct current from the battery system to a power supply node along a current path, a first switch and a second switch, each configured to selectively conduct current from the battery system to the at least one diode, the method comprising:
receiving a signal from the first battery management system, wherein the signal is generated based on at least one of a sensed current and a sensed voltage of the current path; and
determining whether the at least one diode of the first battery management system is faulty based at least in part on the signal.
8. The method of operating the power delivery system of claim 7 , further comprising:
controlling a conductivity of the first switch of at least one of the first battery management system and the second battery management system.
9. The method of operating the power delivery system of claim 8 , further comprising:
conditionally testing the at least one diode.
10. The method of operating the power delivery system of claim 7 , further comprising:
causing at least one of the first switch and the second switch of the first battery management system to be conductive, whereby current from the battery system of the first battery management system is conducted to a power supply conductor.
11. The method of operating the power delivery system of claim 7 , further comprising:
causing the first switch and the second switch of the second battery management system to be nonconductive;
determining a voltage of the second battery management system; and
determining whether the at least one diode of the second battery management system has a short based on the determined voltage of the second battery management system.
12. The method of operating the power delivery system of claim 7 , further comprising:
causing the first switch of the first battery management system to be conductive, whereby current from a battery of the battery system is conducted to a first power supply node of the first battery management system;
causing the first switch and the second switch of the first battery management system to be nonconductive;
determining a voltage of the first power supply node while the first switch and the second switch of the first battery management system are nonconductive; and
determining whether the diode of the first battery management system has an open based on the determined voltage of the first power supply node.
13. A power system for an aviation system, comprising:
a plurality of battery management systems, each of the plurality of battery management systems including:
one or more batteries,
a first diode configured to conduct a first current from the batteries to a power supply conductor,
a first current monitor configured to sense a first measurement value of the first current,
a second diode configured to conduct a second current from the batteries to the power supply conductor,
a second current monitor configured to sense a second measurement value of the second current, and
a switch configured to conditionally electrically connect the batteries to the first and second diodes to conditionally cause the batteries to provide current to the power supply conductor; and
a controller, where the controller is configured to perform operations comprising:
receiving first current values and second current values from the first current monitor and the second current monitor of a particular battery management system of the plurality of battery management systems, and
controlling a conductivity of the switch of the particular battery management system based at least in part on the first current values and the second current values.
14. The power system of claim 13 , wherein the controller is configured to determine a diode short or a diode open in one or more of the plurality of battery management systems during flight diode testing.
15. The power system of claim 13 , where the controller of a first battery management system of the battery management systems is configured to perform operations comprising:
receiving first current values and second current values from the first current monitor and the second current monitor of the first battery management system, wherein the first current values provide an indication of a first current amount flowing through the first diode of the first battery management system, and where the second current values provide an indication of a second current amount flowing through the second diode of the first battery management system; and
detecting a short in one of the first and second diodes by detecting that one of the first and second current values or a magnitude of one of the first and second current values is greater than a threshold.
16. The power system of claim 13 , where the controller of a first battery management system of the battery management systems is configured to perform operations comprising:
receiving first current values and second current values from the first current monitor and the second current monitor of the first battery management system, wherein the first current values provides an indication of a first current amount flowing through the first diode of the first battery management system, and where the second current value provide an indication of a second current amount flowing through the second diode of the first battery management system; and,
detecting an open in one of the first and second diodes by detecting that one of the first and second current values is less than a threshold.
17. A method of operating a power delivery system for an aircraft, the power delivery system comprising a plurality of battery management systems, each of the plurality of battery management system including: one or more batteries, a first diode configured to conduct a first current from the batteries to a power supply conductor, a first current monitor configured to sense a first measurement value of the first current, a second diode configured to conduct a second current from the batteries to the power supply conductor, a second current monitor configured to sense a second measurement value of the second current, and a switch configured to conditionally electrically connect the batteries to the first and second diodes to conditionally cause the batteries to provide current to the power supply conductor, the method comprising:
receiving first current values and second current values from the first current monitor and the second current monitor of a particular battery management system of the plurality of battery management systems, and
controlling a conductivity of the switch of the particular battery management system based at least in part on the first current values and the second current values.
18. The method of claim 17 , further comprising:
determining a diode short or a diode open in one or more of the plurality of battery management systems during flight diode testing.
19. The method of claim 17 , further comprising:
receiving first current values and second current values from the first current monitor and the second current monitor of a first battery management system of the plurality of battery management systems, wherein the first current values provides an indication of a first current amount flowing through the first diode of the first battery management system, and wherein the second current values provide an indication of a second current amount flowing through the second diode of the first battery management system; and
detecting a short in one of the first and second diodes by detecting that one of the first current values and the second current values or a magnitude of one of the first current values and the second current values is greater than a threshold.
20. The method of claim 17 , further comprising:
receiving first current values and second current values from the first current monitor and the second current monitor of a first battery management system of the plurality of battery management systems, wherein the first current values provides an indication of a first current amount flowing through the first diode of the first battery management system, and where the second current values provide an indication of a second current amount flowing through the second diode of the first battery management system; and
detecting an open in one of the first diode and the second diode by detecting that one of the first current values and the second current values is less than a threshold.