Detecting engine exhaust debris using saturation current
A method is provided for an engine. During this method, a saturation current of a gas flow is measured. The gas flow includes combustion products generated by the engine. The saturation current is monitored to determine presence of debris entrained within the gas flow.
1. A method for a gas turbine engine, the gas turbine engine comprising a combustor section, a turbine section, and an exhaust section, the method comprising:
measuring a saturation current of a gas flow using one or more saturation current probes, the one or more saturation current probes arranged downstream of the combustor section, the gas flow comprising combustion products generated by the engine;
monitoring the saturation current to determine presence of debris entrained within the gas flow; and
providing an indicator when debris is detected within the gas flow.
2. The method of claim 1 , wherein
the combustion products include a plurality of emissions molecules, and a first of the plurality of emissions molecules has an emissions molecule mass;
the debris comprises a plurality of debris particles, and a first of the plurality of debris particles has a debris particle mass and volume; and
the debris particle mass is at least one order of magnitude greater than the emissions molecule mass.
3. The method of claim 1 , wherein
the debris comprises a plurality of debris particles; and
a first of the plurality of debris particles has a size equal to or greater than one nanometer.
4. The method of claim 1 , wherein
the debris comprises a plurality of debris particles; and
a first of the plurality of debris particles has a size equal to or greater than one micron.
5. The method of claim 1 , wherein the debris comprises metal liberated from an internal component of the engine.
6. The method of claim 1 , wherein the debris comprises ceramic or other non-metallic material liberated from an internal component of the engine.
7. The method of claim 1 , further comprising:
ingesting foreign particulate matter into the engine with air for combustion;
wherein the debris comprises the foreign particulate matter.
8. The method of claim 1 , wherein the measuring of the saturation current of the gas flow includes
directing electrical potential across a gap between a plurality of electrodes through the gas flow;
varying a voltage of the electrical potential; and
measuring a current of the electrical potential as the voltage is varied.
9. The method of claim 1 , further comprising determining presence of the debris entrained within the gas flow with the combustion products.
10. The method of claim 1 , wherein the one or more saturation current probes are arranged downstream of the turbine section of the gas turbine engine.
11. The method of claim 1 , further comprising determining a characteristic of the debris entrained within the gas flow based on the saturation current.
12. The method of claim 1 , wherein the combustion products are generated within the engine by combustion of a fuel-air mixture.
13. The method of claim 1 , wherein the one or more saturation current probes are arranged within the exhaust section of the gas turbine engine.
14. A method for a gas turbine engine, comprising:
directing a gas flow through a gap between a plurality of electrodes, the gas flow comprising combustion products generated by combustion of a fuel-air mixture within the gas turbine engine;
directing electrical potential across the gap through the gas flow between the plurality of electrodes;
varying a voltage of the electrical potential directed across the gap;
measuring a saturation current of the electrical potential directed across the gap as the voltage is varied, using one or more saturation current probes;
determining presence of debris particles entrained within the gas flow based on the saturation current; and
providing a notification when debris particles are detected within the gas flow.
15. The method of claim 14 , wherein the debris particles are distinct from emissions molecules within the combustion products.
16. The method of claim 14 , wherein the debris comprises metal liberated from an internal component of the gas turbine engine.
17. The method of claim 14 , wherein the debris comprises ceramic or other non-metallic material liberated from an internal component of the gas turbine engine.
18. The method of claim 14 , further comprising:
ingesting foreign particulate matter into the gas turbine engine with air for combustion;
wherein the debris comprises the foreign particulate matter.