Method and system for inlet blockage detection
Herein provided are methods and systems for detecting blockage of an inlet of gas turbine engine. An oil temperature measurement of the engine and an ambient temperature measurement is obtained. The oil temperature measurement is compared to a threshold based on the ambient temperature measurement. Blockage of the inlet of the engine is detected when the oil temperature measurement exceeds the threshold.
1. A computer-implemented method for detecting blockage of an inlet of a gas turbine engine, the method comprising:
obtaining an oil temperature measurement of the engine from at least one first temperature sensor and an ambient temperature measurement from at least one second temperature sensor;
comparing the oil temperature measurement to a threshold based on the ambient temperature measurement;
detecting blockage of the inlet of the engine when the oil temperature measurement exceeds the threshold; and
in response to detecting blockage of the inlet, outputting an alert indicating blockage of the inlet to an aircraft system or shutting down the engine.
2. The method of claim 1 , wherein the threshold varies as a function of ambient temperature ranges.
3. The method of claim 2 , wherein the threshold is constant at a first value for at least a first one of the ambient temperature ranges.
4. The method of claim 3 , wherein the threshold is constant at a second value for at least a second one of the ambient temperature ranges, the first value being different from the second value.
5. The method of claim 1 , wherein comparing the oil temperature measurement to the threshold based on the ambient temperature measurement comprises determining a threshold value corresponding with the ambient temperature measurement and comparing the oil temperature measurement to the threshold value.
6. The method of claim 5 , wherein the threshold comprises a curve defining a relationship between oil temperature and ambient temperature and wherein determining the threshold value comprises locating the threshold value on the curve.
7. The method of claim 1 , wherein the engine is an auxiliary power unit and the inlet provides air to an oil cooler of the auxiliary power unit.
8. The method of claim 1 , wherein the inlet is an auxiliary inlet of the engine and the auxiliary inlet provides air to an oil cooler of the engine.
9. A system for detecting blockage of an inlet of a gas turbine engine, the system comprising:
a processing unit; and
a non-transitory computer-readable memory having stored thereon program instructions executable by the processing unit for:
obtaining an oil temperature measurement of the engine from at least one first temperature sensor and an ambient temperature measurement from at least one second temperature sensor;
comparing the oil temperature measurement to a threshold based on the ambient temperature measurement;
detecting blockage of the inlet of the engine when the oil temperature measurement exceeds the threshold; and
in response to detecting blockage of the inlet, outputting an alert indicating blockage of the inlet to an aircraft system or shutting down the engine.
10. The system of claim 9 , wherein the threshold varies as a function of ambient temperature ranges.
11. The system of claim 10 , wherein the threshold is constant at a first value for at least a first one of the ambient temperature ranges.
12. The system of claim 11 , wherein the threshold is constant at a second value for at least a second one of the ambient temperature ranges, the first value being different from the second value.
13. The system of claim 9 , wherein comparing the oil temperature measurement to the threshold based on the ambient temperature measurement comprises determining a threshold value corresponding with the ambient temperature measurement and comparing the oil temperature measurement to the threshold value.
14. The system of claim 13 , wherein the threshold comprises a curve defining a relationship between oil temperature and ambient temperature and wherein determining the threshold value comprises locating the threshold value on the curve.
15. The system of claim 9 , wherein the engine is an auxiliary power unit and the inlet provides air to an oil cooler of the auxiliary power unit.
16. The system of claim 9 , wherein the inlet is an auxiliary inlet of the engine and the auxiliary inlet provides air to an oil cooler of the engine.
17. A non-transitory computer readable medium having stored thereon program code executable by a processor for detecting blockage of an inlet of a gas turbine engine, the program code comprising instructions for:
obtaining an oil temperature measurement of the engine from at least one first temperature sensor and an ambient temperature measurement from at least one second temperature sensor;
comparing the oil temperature measurement to a threshold based on the ambient temperature measurement;
detecting blockage of the inlet of the engine when the oil temperature measurement exceeds the threshold; and
in response to detecting blockage of the inlet, outputting an alert indicating blockage of the inlet to an aircraft system or shutting down the engine.
18. The non-transitory computer readable medium of claim 17 , wherein comparing the oil temperature measurement to the threshold based on the ambient temperature measurement comprises determining a threshold value corresponding with the ambient temperature measurement and comparing the oil temperature measurement to the threshold value.