Self-learning monitoring systems for electrical devices

Patent metadata

Field	Value
Publication number	US-9488533-B2
Application number	US-201414251102-A
Country	US
Kind code	B2
Filing date	Apr 11, 2014
Priority date	Apr 11, 2014
Publication date	Nov 8, 2016
Grant date	Nov 8, 2016

Abstract

A method of monitoring an electrical device includes receiving an operational condition of an electrical device, receiving a measurement indicative of a thermal parameter of the electrical device corresponding to the operational condition, and storing the measurement in memory in association with the operational condition. A system for monitoring electrical devices includes a processor communicative with a memory and the memory has instructions recorded thereon that, when read by the processor, cause the processor to execute the method.

First claim

What is claimed is:

1. A method of monitoring an electrical device, comprising:
receiving a first operational condition of an electrical device, wherein the first operational condition corresponds to an aircraft operating regime;
receiving a first measurement indicative of a thermal parameter of the electrical device while in the first operational condition;
determining a first limit using the first measurement;
storing the first limit in association with the first operational condition in memory;
receiving a second operational condition of the electrical device, wherein the second operational condition is different than the first operational condition;
receiving a second measurement indicative of the thermal parameter while of the electrical device while in the second operational condition;
determining a second limit using the second measurement; and
storing the second limit in association with the second operational condition in memory,
wherein the first measurement and the second measurement are acquired by scanning an interior surface the electrical device using an infrared or ultraviolet charged coupled device.

2. A method as recited in claim 1 , wherein the aircraft operating regime comprises an aircraft operating regime selected from a group comprising taxiing, takeoff, cruise, and landing.

3. A method as recited in claim 1 , wherein the aircraft operating regime corresponds to at least one of an aircraft altitude, external air temperature or engine power setting, load on the electrical device, or other equipment condition.

4. A method as recited in claim 1 , further comprising:
receiving a second measurement while the electrical device is in the first operational condition;
comparing the second measurement with the first limit; and
providing a response if the measurement is outside the first limit.

5. A method as recited in claim 4 , wherein determining the first includes statistically determining a limit using the first and second measurements.

6. A method as recited in claim 4 , wherein providing a response includes providing an alert.

7. A method as recited in claim 4 , wherein providing a response includes load shedding.

8. A method as recited in claim 1 , wherein the limit is a first limit and the method further comprises:
receiving an operational condition selected from a group including the first and the second operational conditions;
receiving a third measurement in the received operational condition;
selecting one of the first and second limits based on the received operational condition;
comparing the third measurement with the selected limit; and
providing a response if the third measurement is outside the selected limit.

9. A method as recited in claim 1 , wherein receiving a measurement further comprises acquiring an image of the interior surface of the electrical device.

10. A method as recited in claim 1 , wherein receiving a measurement further comprises acquiring a relative intensity map of an interior surface the electrical device using the infrared or ultraviolet charged coupled device.

11. A non-transitory, machine-readable medium with instructions recorded thereon that, when read by a processor causes the processor to:
receive a first operational condition of an electrical device, wherein the first operational condition corresponds to an aircraft operating regime;
receive a first measurement indicative of a thermal parameter of the electrical device while in the first operational condition;
determine a first limit using the first measurement;
store the first limit in association with the first operational condition in memory;
receive a second operational condition of the electrical device, wherein the second operational condition is different than the first operational condition;
receive a second measurement indicative of the thermal parameter while of the electrical device while in the second operational condition;
determine a second limit using the second measurement; and
store the second limit in association with the second operational condition in memory
wherein the first measurement and the second measurement are acquired by scanning an interior surface the electrical device using an infrared or ultraviolet charged coupled device.

12. A medium as recited in claim 11 , wherein the instructions further cause the processor to:
receive an operational condition selected from a group including the first and second operational conditions;
receive a third measurement indicative of the thermal parameter while the electrical device is in the operational condition;
select one of the first and second limits based on the operational condition;
compare the third measurement with the selected limit; and
provide a response if the measurement is outside the selected limit.

Assignees

• Kidde Tech Inc

Inventors

• Schnetker Ted R

Classifications

• G01R31/62

  Testing of transformers · CPC title

• G01R31/64

  Testing of capacitors · CPC title

• G01R31/40

  Testing power supplies (testing photovoltaic devices H02S50/10) · CPC title

• G01K2205/00

  Application of thermometers in motors, e.g. of a vehicle · CPC title

• G01J2005/0077

  Imaging · CPC title