Heating prognostics system for ice protection system

1. A method of monitoring an ice protection system of a rotorcraft or an aircraft, the method comprising:

applying heat to rotating blades of the rotorcraft or the aircraft according to a heater duty cycle;

determining an anticipated ice shed time for ice to shed from the rotating blades;

sensing a torque of the rotating blades;

determining an actual ice shed time for ice to shed from the rotating blades based on the sensed torque;

determining a status of the ice protection system based on the anticipated ice shed time and the actual ice shed time; and

outputting the status of the ice protection system for consumption by a consuming system.

2. The method of claim 1 , and further comprising:

sensing a liquid water content of air outside of the rotorcraft or the aircraft;

sensing an outside air temperature; and

determining the heater duty cycle based on the liquid water content and the outside air temperature.

3. The method of claim 2 , and further comprising:

sensing at least one of a voltage of the ice protection system, a current of the ice protection system, a power of the ice protection system, or a blade temperature of the rotating blades;

determining an actual power application based on at least one of the sensed voltage, the sensed current, the sensed power, or the sensed blade temperature; and

determining if the ice protection system has failed based on the actual power application and the heater duty cycle.

4. The method of claim 3 , wherein determining if the ice protection system has failed based on the actual power application and the heater duty cycle further comprises:

setting a threshold that that the actual power application, based on at least one of the sensed voltage, the sensed current, or the sensed power, can be within based on power application comments from the heater duty cycle; and

determining whether the actual power application is within the threshold;

wherein if the actual power application is outside of the threshold, the ice protection system can output a signal indicating that the ice protection system has failed.

5. The method of claim 1 , and further comprising:

sensing at least one of a voltage of the ice protection system, an outside air temperature, or an RPM of the rotating blades;

wherein determining the anticipated ice shed time is based on at least one of the sensed voltage, the sensed outside air temperature, or the sensed RPM.

6. The method of claim 1 , and further comprising:

sensing a current of the ice protection system;

wherein determining the actual ice shed time is based on the sensed torque and the sensed current.

7. The method of claim 1 , wherein determining the status of the ice protection system based on the anticipated ice shed time and the actual ice shed time further comprises:

setting a threshold that the actual ice shed time can be from the anticipated ice shed time; and

determining if the actual ice shed time is within the threshold to determine if the ice protection system is in a nondegraded state or a degraded state.

8. The method of claim 1 , wherein outputting the status of the ice protection system for consumption by the consuming system further comprises:

generating an alert that the ice protection system is degrading and a pilot should exit icing conditions; and

sending the alert to an electronic flight instrument system (EFIS) of the rotorcraft or the aircraft.

9. The method of claim 1 , wherein outputting the status of the ice protection system for consumption by the consuming system further comprises:

generating an alert that maintenance of the ice protection system is needed; and

sending the alert to an electronic flight instrument system (EFIS) or maintenance system of the rotorcraft or the aircraft.

10. The method of claim 1 , wherein outputting the status of the ice protection system for consumption by the consuming system further comprises:

sending a control command to a heater controller of the ice protection system; and

automatically adjusting a voltage, a current, or a power being applied to the ice protection system based on the control command.

11. The method of claim 1 , and further comprising:

storing prognostic data for each deicing event in a memory; and

analyzing the prognostic data for multiple deicing events to determine if there is degradation of the ice protection system.

12. A method of monitoring an ice protection system of a rotorcraft or an aircraft, the method comprising:

sensing a liquid water content of air outside of the rotorcraft or the aircraft;

sensing an outside air temperature;

sensing a voltage of the ice protection system;

determining a heater duty cycle based on the sensed liquid water content and the sensed outside air temperature;

applying heat to rotating blades of the rotorcraft or the aircraft according to the heater duty cycle;

determining an anticipated ice shed time for ice to shed from the rotating blades based on the sensed voltage and the sensed outside air temperature;

sensing a torque of the rotating blades;

determining an actual ice shed time for ice to shed from the rotating blades based on the sensed torque;

determining a status of the ice protection system based on the anticipated ice shed time and the actual ice shed time; and

outputting the status of the ice protection system for consumption by a consuming system.

13. The method of claim 12 , and further comprising:

sensing at least one of a current of the ice protection system, a power of the ice protection system, or a blade temperature of the rotating blades;

determining an actual power application based on at least one of the sensed voltage, the sensed current, the sensed power, or the sensed blade temperature; and

determining if the ice protection system has failed based on the actual power application and the heater duty cycle, wherein determining if the ice protection system has failed based on the actual power application and the heater duty cycle further comprises:

setting a threshold that that the actual power application, based on at least one of the sensed voltage, the sensed current, or the sensed power, can be within based on power application comments from the heater duty cycle; and

determining whether the actual power application is within the threshold;

wherein if the actual power application is outside of the threshold, the ice protection system can output a signal indicating that the ice protection system has failed.

14. The method of claim 12 , and further comprising:

sensing an RPM of the rotating blades;

wherein determining the anticipated ice shed time is based on at least one of the sensed voltage, the sensed outside air temperature, or the sensed RPM.

15. The method of claim 14 , and further comprising:

sensing a current of the ice protection system; and/or

sensing a vibration of the rotating blades;

wherein determining the actual ice shed time is also based on at least one of the the sensed current, and the sensed vibration.

16. The method of claim 15 , wherein determining the status of the ice protection system based on the anticipated ice shed time and the actual ice shed time further comprises:

setting a threshold that the actual ice shed time can be from the anticipated ice shed time; and

determining if the actual ice shed time is within the threshold to determine if the ice protection system is in a nondegraded state or a degraded state.

17. The method of claim 12 , wherein outputting the status of the ice protection system for consumption by the consuming system further comprises:

generating an alert that the ice protection system is degrading and a pilot should exit icing conditions; and

sending the alert to an electronic flight instrument system (EFIS) of the rotorcraft or the aircraft.

18. The method of claim 12 , wherein outputting the status of the ice protection system for consumption by the consuming system further comprises:

generating an alert that maintenance of the ice protection system is needed; and

sending the alert to an electronic flight instrument system (EFIS) or maintenance system of the rotorcraft or the aircraft.

19. The method of claim 12 , wherein outputting the status of the ice protection system for consumption by the consuming system further comprises:

sending a control command to a heater controller of the ice protection system; and

automatically adjusting a voltage, a current, or a power being applied to the ice protection system based on the control command.

20. The method of claim 12 , and further comprising:

storing prognostic data for each deicing event in a memory; and

analyzing the prognostic data for multiple deicing events to determine if there is degradation of the ice protection system.