Health monitoring for multi-channel pressure transducers

1. A health monitoring method for a multi-channel pressure transducer of a gas turbine engine, the method comprising

monitoring a deviation between a first channel and a second channel of a multi-channel pressure transducer over time;

determining a rate of change of the deviation;

extrapolating a trend over time based on the rate of change of the deviation to predict when the deviation will reach a threshold; and

triggering a maintenance action for the multi-channel pressure transducer based on the trend.

2. The method of claim 1 , wherein the multi-channel pressure transducer comprises at least three channels, and monitoring the deviation comprises doing channel to channel comparisons between channel pairs.

3. The method of claim 2 , wherein determining the rate of change of the deviation comprises determining the rate of change for each of the channel pairs, and wherein extrapolating the trend comprises extrapolating the trend for each of the channel pairs.

4. The method of claim 1 , wherein the first channel drifts over time and the second channel is stable.

5. The method of claim 1 , wherein monitoring the deviation comprises:

measuring and recording pressure readings for the first channel and the second channel at a plurality of instances in time at first pressure and temperature conditions; and

determining a difference between the pressure readings of the first channel and the second channel at the plurality of instances in time, the difference corresponding to the deviation.

6. The method of claim 5 , wherein monitoring the deviation comprises monitoring the deviation for a plurality of pressure and temperature conditions.

7. The method of claim 6 , wherein determining the rate of change of the deviation comprises determining the rate of change of the deviation for the plurality of pressure and temperature conditions.

8. The method of claim 7 , wherein extrapolating the trend over time comprises extrapolating the trend for the plurality of pressure and temperature conditions, and predicting when the deviation will reach the threshold at any one of the pressure and temperature conditions.

9. The method of claim 6 , wherein the plurality of pressure and temperature conditions comprise an engine operating point prior to an engine start, at least one engine operating point after the engine start, and an engine operating point following engine shutdown.

10. A health monitoring system for a multi-channel pressure transducer of a gas turbine engine, the system comprising:

a processing unit; and

a non-transitory computer readable medium having stored thereon program instructions executable by the processing unit for:

monitoring a deviation between a first channel and a second channel of a multi-channel pressure transducer over time;

determining a rate of change of the deviation;

extrapolating a trend over time based on the rate of change of the deviation to predict when the deviation will reach a threshold; and

triggering a maintenance action for the multi-channel pressure transducer based on the trend.

11. The system of claim 10 , wherein the multi-channel pressure transducer comprises at least three channels, and monitoring the deviation comprises doing channel to channel comparisons between channel pairs.

12. The system of claim 11 , wherein determining the rate of change of the deviation comprises determining the rate of change for each of the channel pairs, and wherein extrapolating the trend comprises extrapolating the trend for each of the channel pairs.

13. The system of claim 10 , wherein the first channel drifts over time and the second channel is stable.

14. The system of claim 10 , wherein monitoring the deviation comprises:

measuring and recording pressure readings for the first channel and the second channel at a plurality of instances in time at first pressure and temperature conditions; and

determining a difference between the pressure readings of the first channel and the second channel at the plurality of instances in time, the difference corresponding to the deviation.

15. The system of claim 14 , wherein monitoring the deviation comprises monitoring the deviation for a plurality of pressure and temperature conditions.

16. The system of claim 15 , wherein determining the rate of change of the deviation comprises determining the rate of change of the deviation for the plurality of pressure and temperature conditions.

17. The system of claim 16 , wherein extrapolating the trend over time comprises extrapolating the trend for the plurality of pressure and temperature conditions, and predicting when the deviation will reach the threshold at any one of the pressure and temperature conditions.

18. The system of claim 17 , wherein the plurality of pressure and temperature conditions comprise an engine operating point prior to an engine start, at least one engine operating point after the engine start, and an engine operating point following engine shutdown.

19. A system comprising:

a gas turbine engine;

at least one multi-channel pressure transducer coupled to the gas turbine engine for measuring pressure along a gas path thereof; and

a controller coupled to the at least one multi-channel pressure transducer and configured for:

monitoring a deviation between a first channel and a second channel of the at least one multi-channel pressure transducer over time;

determining a rate of change of the deviation;

extrapolating a trend over time based on the rate of change of the deviation to predict when the deviation will reach a threshold; and

triggering a maintenance action for the at least one multi-channel pressure transducer based on the trend.

20. The system of claim 19 , wherein the first channel drifts over time and the second channel is stable.