Aircraft and particulate detection method

1. A particulate detection method for an aircraft having a jet engine comprising a core having a compressor and a combustion chamber, the method comprising:

sensing particulates within the core and providing a corresponding particulate value for the sensed particulates;

determining at least one of a geographic position and altitude of the aircraft corresponding to the sensing of the particulates;

selecting a particulate reference value for the determined at least one of the geographic position and altitude;

comparing the particulate value to the particulate reference value; and

providing an indication based on the comparison,

wherein providing an indication based on the comparison further comprises providing the indication to a computer aboard the aircraft, providing an alert on a flight deck of the aircraft and providing an indication to one or more ground systems, and

wherein sensing particulates further comprises sensing particulates during at least one of taxi, takeoff, descent, and landing, but not sensing particulates during cruise.

2. The method of claim 1 wherein the particulate sensing occurs within forward stages of the compressor.

3. The method of claim 2 wherein the particulate sensing comprises sensing using one particulate sensor.

4. The method of claim 1 wherein the particulate sensing is conducted with an electrostatic sensor.

5. The method of claim 1 wherein the determining at least one of the geographic position and the altitude comprises determining at least the geographic position.

6. The method of claim 1 wherein the determining at least one of the geographic position and the altitude comprises determining both the geographic position and the altitude.

7. The method of claim 6 wherein the determining the geographic position comprises determining a GPS coordinate from a GPS device on the aircraft and determining the altitude comprises determining an altitude from an altimeter on the aircraft.

8. The method of claim 1 wherein the selecting the particulate reference value comprises conducting a query of a database of reference values on a computer aboard the aircraft.

9. The method of claim 8 wherein the providing an indication comprises providing an alert on a flight deck of the aircraft.

10. The method of claim 1 wherein the comparing comprises taking a difference between the particulate value and the particulate reference value.

11. The method of claim 10 wherein providing an indication comprises when the comparison indicates a satisfying of a comparison threshold.

12. The method of claim 11 wherein the satisfying the comparison threshold comprises determining the absolute value of the difference being equal to or greater than the comparison threshold.

13. The method of claim 1 wherein the particulate reference value is a running average of a predetermined number of prior particulate values.

14. An aircraft, comprising:

a jet engine assembly, comprising:

a core having a compressor and a combustion chamber downstream of the compressor; and

a single button particulate sensor located within the core and configured to output a signal indicative of sensed particulates in a limited portion of the core; and

a controller having a processor to process the sensor signal indicative of sensed particulates and determine a corresponding particulate value for the sensed particulates and configured to provide an indication regarding the sensed particulates,

wherein the single button particulate sensor senses particulates during at least one of taxi, takeoff, descent, and landing, but not during cruise.

15. The aircraft of claim 14 wherein the controller is further configured to determine at least one of a geographic position and altitude of the aircraft corresponding to the sensing of the particulates, select a particulate reference value for the determined at least one of a geographic position and altitude, compare the particulate value to the particulate reference value, and provide an indication when the comparison indicates the satisfying of a comparison threshold.

16. A particulate detection method for an aircraft having a jet engine, the jet engine comprising a core, the core comprising a compressor and a combustion chamber, the method comprising:

sensing particulates within the core and providing a corresponding particulate value for the sensed particulates;

determining at least one of a geographic position and altitude of the aircraft corresponding to the sensing of the particulates;

selecting a particulate reference value for the determined at least one of the geographic position and altitude;

comparing the particulate value to the particulate reference value; and

alerting a pilot of potentially harmful concentrations of particulate,

wherein sensing particulates further comprises sensing particulates during at least one of taxi, takeoff, descent, and landing, but not sensing particulates during cruise.

17. The method of claim 1 wherein sensing particulates within the core comprises sensing particulates within the core of a jet engine comprising a core having a compressor and a combustion chamber.

18. The method of claim 1 wherein selecting a particulate reference value further comprises accessing a computer-searchable database of information, the computer-searchable database of information including memory and one or more processors.