Electrical machine monitor

Patent metadata

Field	Value
Publication number	US-11514732-B2
Application number	US-202016803382-A
Country	US
Kind code	B2
Filing date	Feb 27, 2020
Priority date	Feb 27, 2020
Publication date	Nov 29, 2022
Grant date	Nov 29, 2022

Abstract

An example method includes receiving, by one or more processors and via a sensor, a signal representing operational characteristics of a device included in an aircraft; determining, by the one or more processors and based on the signal, a partial discharge intensity value; receiving, by the one or more processors and via an environmental sensor, at least one environmental measurement of the device; modifying, by the one or more processors and based on the at least one environmental measurement, the partial discharge intensity value to determine a modified partial discharge intensity value; and responsive to determining that the modified partial discharge intensity value satisfies a threshold, outputting an alert signal for the device.

First claim

What is claimed is:

1. A method comprising:
receiving, by one or more processors and via a sensor, a signal representing operational characteristics of a device included in an aircraft;
determining, by the one or more processors and based on the signal, a partial discharge intensity value;
receiving, by the one or more processors and via an environmental sensor, at least one environmental measurement of the device;
modifying, by the one or more processors and based on the at least one environmental measurement, the partial discharge intensity value to determine a modified partial discharge intensity value; and
responsive to determining that the modified partial discharge intensity value satisfies a threshold, outputting an alert signal for the device.

2. The method of claim 1 , wherein modifying the partial discharge intensity value further comprises modifying the partial discharge intensity value based on at least one equipment usage factor.

3. The method of claim 2 , wherein the at least one equipment usage factor includes one or more of a direct current (DC) line voltage, an average conductor coil current, and a winding temperature.

4. The method of claim 1 , wherein the at least one environmental measurement comprises one or more of a relative humidity and an air pressure.

5. The method of claim 3 , wherein the device included in the aircraft includes a conductor driven with a variable frequency current.

6. The method of claim 1 , wherein the sensor comprises one or more of a resistance temperature sensor, a high frequency current transformer, a common mode high frequency current transformer, a voltage derivative sensor, and a Y capacitor.

7. The method of claim 1 , wherein determining the modified partial discharge intensity value comprises determining a plurality of modified partial discharge intensity values that each correspond to a different time during a time period, wherein determining whether the modified partial discharge value satisfies the threshold comprises determining whether the plurality of modified partial discharge intensity values satisfy the threshold.

8. The method of claim 7 , wherein determining whether the plurality of modified partial discharge intensity values satisfy the threshold comprises determining whether a rate of change of the plurality of modified partial discharge intensity values is greater than a threshold rate of change.

9. The method of claim 7 , wherein the plurality of modified partial discharge intensity values comprises a first plurality of modified partial discharge intensity values for a first time period, the method further comprising:
determining, based on a plurality of modified partial discharge intensity values for a second time period that is before the first time period, a baseline modified partial discharge intensity value,
wherein determining whether the plurality of modified partial discharge intensity values satisfy the threshold comprises determining whether an average of the first plurality of modified partial discharge intensity values is greater than a scaled version of the baseline modified partial discharge intensity value.

10. A system comprising:
a device included in an aircraft;
an environmental sensor;
a sensor; and
one or more processors configured to:
receive, via the sensor, a signal representing operational characteristics of a device included in an aircraft;
determine, based on the signal, a partial discharge intensity value;
receive, via the environmental sensor, at least one environmental measurement of the device;
modify, based on the at least one environmental measurement, the partial discharge intensity value to determine a modified partial discharge intensity value; and
responsive to determining that the modified partial discharge intensity value satisfies a threshold, output an alert signal for the device.

11. The system of claim 10 , wherein modifying the partial discharge intensity value further comprises modifying the partial discharge intensity value based on at least one equipment usage factor.

12. The system of claim 11 , wherein the sensor comprises one or more of a resistance temperature sensor, a high frequency current transformer, a common mode high frequency current transformer, a voltage derivative sensor, and a Y capacitor, and
wherein the at least one equipment usage factor includes one or more of a direct current (DC) line voltage, an average conductor coil current, and a winding temperature.

13. The system of claim 10 , wherein the at least one environmental measurement comprises one or more of a relative humidity and an air pressure.

14. The system of claim 10 , wherein determining the modified partial discharge intensity value comprises determining a plurality of modified partial discharge intensity values that each correspond to a different time during a time period, wherein determining whether the modified partial discharge value satisfies the threshold comprises at least one of determining whether the plurality of modified partial discharge intensity values satisfy the threshold and determining whether a rate of change of the plurality of modified partial discharge intensity values is greater than a threshold rate of change.

15. The system of claim 14 , wherein the plurality of modified partial discharge intensity values comprises a first plurality of modified partial discharge intensity values for a first time period, the one or more processors further configured to:
determine, based on a plurality of modified partial discharge intensity values for a second time period that is before the first time period, a baseline modified partial discharge intensity value,
wherein determining whether the plurality of modified partial discharge intensity values satisfy the threshold comprises determining whether an average of the first plurality of modified partial discharge intensity values is greater than a scaled version of the baseline modified partial discharge intensity value.

16. A variable frequency drive system comprising:
an electric machine;
one or more conductor coils;
an environmental sensor;
a sensor; and
at least variable frequency drive configured to provide electrical power to the electric machine, the at least variable frequency drive comprising:
at least one high voltage terminal; and
at least one processor configured to:
receive, via the sensor, a signal representing operational characteristics of the variable frequency drive system;
determine, based on the signal, a partial discharge intensity value;
receive, via the environmental sensor, at least one environmental measurement of the variable frequency drive system;
modify, based on the at least one environmental measurement, the partial discharge intensity value to determine a modified partial discharge intensity value; and
responsive to determining that the modified partial discharge intensity value satisfies a threshold, output an alert signal for the device.

17. The variable frequency drive system of claim 16 , wherein modifying the partial discharge intensity value further comprises modifying the partial discharge intensity value based on at least one equipment usage factor.

18. The variable frequency drive system of claim 17 , wherein the at least one environmental measurement comprises one or more of a relative humidity and an air pressure.

19. The variable frequency drive system of claim 18 , wherein the sensor comprises one or more of a resistance temperature sensor, a high frequency current transformer, a common mode high freq

Assignees

• Rolls Royce Corp

Inventors

• Loder David

Classifications

• B60L2200/10

  Air crafts · CPC title

• B60L3/12

  Recording operating variables {; Monitoring of operating variables} · CPC title

• B60L2240/66

  Ambient conditions · CPC title

• Y02T10/72

  Electric energy management in electromobility · CPC title

• B60L2240/429

  Current · CPC title