Gas turbine engine debris monitoring arrangement
An example method of controlling gas turbine engine debris monitoring sensors includes detecting debris carried by air moving through an engine using at least first and second debris sensors, and processing signals from both the first and second debris sensors using a common signal conditioning unit. Another example method of monitoring gas turbine engine debris includes configuring at least one first debris sensor to detect debris carried by airflow moving through a first portion of an engine and configuring at least one second debris sensor to detect debris carried by airflow moving though a second portion of the engine. The method alternates between using the first debris sensor to detect debris and using the second debris sensor to detect debris.
1. A method of monitoring gas turbine engine debris comprising:
configuring at least one first debris sensor to detect debris carried by airflow moving through a first portion of an engine;
configuring at least one second debris sensor to detect debris carried by airflow moving though a second portion of the engine;
alternating between using the first debris sensor to detect debris, the second debris sensor to detect debris, or both; and
including measuring the speed of debris carried by the airflow by detecting the debris using the at least one first debris sensor and the at least one second debris sensor.
2. The method of claim 1 including alternating between the first debris sensor and the second debris sensor in response to a type of debris.
3. The method of claim 1 wherein the alternating includes alternating between using exclusively the first debris sensor to detect debris and exclusively using the second debris sensor to detect debris.
4. The method of claim 1 , wherein both the first and second debris sensor are located axially forward a fan of the engine.
5. The method of claim 1 wherein a fan section of the engine comprises the first portion, and a bypass flow path of the engine comprises the second portion.
6. The method of claim 5 including subtracting an amount of debris in the bypass flow path from an amount of debris in the fan section to determine an amount of debris entering a core of the engine.
7. A method of controlling gas turbine engine debris monitoring sensors comprising:
detecting debris carried by air moving through an engine using at least first and second debris sensors; and
conditioning signals from both the first and second debris sensors that are at different axial locations within the engine using a common signal conditioning unit, wherein at least one of the plurality of debris sensors has a different electrostatic charge sensitivity than another of the plurality of debris sensors.
8. The method of claim 7 including sequentially processing the signals.
9. The method of claim 7 wherein the processing comprises amplifying features of the signal.
10. The method of claim 7 , wherein both the first and second debris sensor are located in an inlet section of the engine.
11. The method of claim 7 including the first debris sensor in an inlet section of the engine and a second debris sensor in a bypass flow path of the engine.
12. The method of claim 11 including subtracting a measured amount of debris in the bypass flow path from a measured amount of debris in the inlet section to determine an amount of debris entering a core of the engine.
13. A gas turbine engine monitoring arrangement comprising:
at least one first sensor configured to detect debris at a first axial location in an engine;
at least one second sensor configured to detect debris at a second, different axial location in the engine; and
a single signal conditioning unit configured to condition signals from both of the at least one first sensor and the at least one second sensor, wherein both the first and second debris sensor are located within a fan section of the engine.
14. The arrangement of claim 13 wherein the at least one first sensor, the at least one second sensor, or both comprise a ring sensor circumferentially disposed about an axis of the engine.
15. The arrangement of claim 13 wherein the at least one first sensor is positioned within a fan section of the engine and the at least one second sensor is in a bypass flow duct of the engine.
16. The arrangement of claim 13 including a controller configured to selectively initiate debris detection using exclusively the at least one first sensor, exclusively the at least one second sensor, or both.
17. The arrangement of claim 13 wherein the first sensor has an exposed surface area that is different than the second sensor.
18. The arrangement of claim 13 where the single signal conditioning unit conditions signals from the at least one first sensor during a first time period, and from the at least one second sensor during a second time period different than the first time period.