Power distribution health management and monitoring
A switch arrangement includes a switch with a source lead and a load lead, a sensor coupled to the switch, and a switch monitor. The switch monitor is in communication with the sensor and is responsive to instructions recorded on a memory to receive a measurement of a switch parameter from the sensor, compare the measurement to a baseline associated with the switch, and determine switch margin using the comparison of the measurement with the baseline associated with the switch. Aircraft electrical systems and methods of monitoring electrical systems are also disclosed.
1. A switch arrangement, comprising:
a switch with a source lead and a load lead;
a sensor coupled to the switch;
a switch monitor in communication with the sensor and responsive to instructions recorded on a memory to:
receive a measurement of a switch parameter from the sensor;
compare the measurement to a baseline associated with the switch; and
determine switch margin using the comparison of the measurement with the baseline associated with the switch.
2. The switch arrangement as recited in claim 1 , wherein the switch includes an electromechanical switching device.
3. The switch arrangement as recited in claim 1 , wherein the switch includes a contactor switching device or a relay switching device.
4. The switch arrangement as recited in claim 1 , wherein the switch parameter is open/close cycles, wherein the instructions further cause the switch monitor to increment a cycle count associated with the switch when the sensor indicates that the switch has opened or closed.
5. The switch arrangement as recited in claim 1 , wherein the switch margin is cycles remaining until a predicted end-of-life of the switch.
6. The switch arrangement as recited in claim 1 , wherein the predicted end-of-life of the switch is calculated using at least one of (a) service data of switches in similar applications, (b) a profile of aircraft operation; and (c) test of a similar switch under similar load conditions.
7. The switch arrangement as recited in claim 1 , wherein the switch includes a solid-state switching device.
8. The switch arrangement as recited in claim 1 , wherein the switch includes an IGBT switching device or a MOSFET switching device.
9. The switch arrangement as recited in claim 1 , wherein the switch parameter is duration of loading above a predetermined value and below a trip value of the switch, wherein the instructions cause the switch monitor:
trigger monitoring when loading exceeds the predetermined value; and
record at least one of duration and peak loading until the loading drops below the predetermined value.
10. The switch arrangement as recited in claim 9 , wherein the loading is current loading or voltage loading.
11. The switch arrangement as recited in claim 9 , wherein the predetermined value is about 80% of the switch trip value.
12. The switch arrangement as recited in claim 1 , wherein the switch margin is a differential between the peak loading and trip value.
13. An electrical system, comprising:
a plurality of switch arrangements as recited in claim 1 ; and
a switch monitor disposed in communication with the plurality of switch monitors and responsive to instructions recorded on a memory to determine electrical system margin using the switch margin determined for the switches,
wherein a first switch arrangement of the plurality of switch arrangements includes an electromechanical switching device,
wherein the switch parameter for the first switch arrangement is open/close cycles, wherein the instructions further cause the switch monitor of the first switch arrangement to increment a cycle count associated with the switch of the first switch arrangement when the sensor of the first switch arrangement indicates that the switch of the first switch arrangement has opened or closed, and
wherein a second switch arrangement of the plurality of switch arrangements includes a solid-state switching device, wherein the switch parameter for the second switch arrangement is duration of loading above a first predetermined value and below a trip value of the switch of the second switch arrangement,
wherein the instructions cause the switch monitor of the second switch arrangement to trigger monitoring when loading exceeds a second predetermined value and record at least one of duration and peak loading until the loading drops below the second predetermined value.
14. The electrical system as recited in claim 13 , wherein the electrical system is an aircraft electrical system.
15. An electrical system health management and monitoring method performed by a switch monitor, the method comprising:
receiving a measurement of a switch parameter of a switch from a sensor coupled to the switch;
comparing -the measurement to a baseline associated with the switch; and
determining switch margin using the comparison of the measurement with the baseline associated with the switch.
16. The method as recited in claim 15 , wherein the switch parameter is open/close cycles, the method further comprises incrementing a cycle count associated with the switch when the sensor indicates that the switch has opened or closed.
17. The method as recited in claim 15 , wherein the switch margin is cycles remaining until a predicted end-of-life of the switch, the method further comprising calculating the predicted end-of-life using at least one of (a) service data of switches in similar applications, (b) a profile of aircraft operation; and (c) test of a similar switch under similar load conditions.
18. The method as recited in claim 15 , wherein switch parameter is duration of loading above a predetermined value and below a trip value of the switch, the method further comprising:
triggering monitoring when loading exceeds the predetermined value; and
recording at least one of duration and peak loading until the loading drops below the predetermined value.
19. The method as recited in claim 15 , further comprising determining electrical system margin using the determined switch margin.
20. A switch arrangement of an electrical system of an aircraft, comprising:
a switch with a source lead and a load lead;
a sensor coupled to the switch;
a switch monitor in communication with the sensor and responsive to execution of instructions recorded on a memory, which when executed by the switch monitor cause the switch monitor to:
receive a measurement of a switch parameter from the sensor;
compare the measurement to a baseline associated with the switch; and
determine switch margin associated with a predicted end of life using the comparison of the measurement with the baseline associated with the switch, wherein the predicted end of life is calculated using a profile of aircraft operation.