Ice detection and mitigation device
A method for deicing an aerostructure includes driving a sensing current through a heater element coated to an aerostructure, the heater element having a resistance that is temperature dependent. A resistance of the heater element is monitored. It is determined whether there is icing at the heater element using the monitored resistance of the heater element. A melting current is driven through the heater element when it is determined that there is icing at the heater element.
1. A method for deicing an aerostructure, comprising:
driving a sensing current through a heater element coated to an aerostructure, the heater element having a resistance that is temperature dependent;
monitoring a resistance of the heater element;
determining whether there is icing at the heater element using the monitored resistance of the heater element; and
driving a melting current through the heater element when it is determined that there is icing at the heater element,
wherein determining whether there is icing at the heater element comprises determining the resistance of the heater element at a first time based on the monitored resistance of the heater element, determining the resistance of the heater element at one or more second times based on the monitored resistance of the heater element, calculating an instantaneous rate of change of the resistance of the heater element based on the determined resistance at the first time and one or more second times, and determining that there is icing on the heater element when the calculated instantaneous rate of change of the resistance of the heater is within a predetermined threshold.
2. The method of claim 1 , wherein the heater element is organized as arrays of heater elements on the surface of the aerostructure.
3. The method of claim 1 , wherein the heater element is coated to the aerostructure by a direct write method.
4. The method of claim 1 , wherein the heater element includes one or more materials with positive or negative temperature coefficients of resistance (TCR).
5. The method of claim 1 , wherein the resistance of the heater element is determined from a voltage of the heater element upon driving the sensing current.
6. The method of claim 1 , wherein an Amperage of the sensing current is substantially less than an Amperage of the melting current.
7. The method of claim 1 , wherein the sensing current is driven for a shorter duty cycle than the melting current.
8. The method of claim 1 , wherein one or more additional sensors are additionally used to estimate a temperature of the heating element.
9. The method of claim 8 , wherein the heater element is a first heater element and the one or more additional sensors are part of a second heater element in communication with the first heater element or a control circuit thereof.
10. The method of claim 1 , wherein the heater element comprises a metallic material.
11. The method of claim 1 , wherein the heater element has a resistance approximately equal to a resistance of nickel-chromium (NiCr).
12. The method of claim 1 , wherein the heater element comprises a plurality of parallel lines with a fixed line length, width and spacing.
13. The method of claim 1 , wherein determining whether there is icing at the heater element includes taking into account a present air speed.
14. A method for deicing an aerostructure, comprising:
monitoring a temperature at a heater element coated to an aerostructure using a temperature monitoring device coated to the aerostructure and in close proximity to the heater element;
determining whether there is icing at the heater element using the monitored temperature at the heater element; and
driving a melting current through the heater element when it is determined that there is icing at the heater element,
wherein determining whether there is icing at the heater element comprises determining the temperature of the heater element at a first time based on the monitored temperature of the heater element, determining the temperature of the heater element at one or more second times based on the monitored temperature of the heater element, calculating an instantaneous rate of change of the temperature of the heater element based on the determined temperature at the first time and one or more second times, and determining that there is icing on the heater element when the calculated instantaneous rate of change of the temperature of the heater is within a predetermined threshold.
15. The method of claim 14 , wherein the temperature is monitored by measuring a resistance of the heater element and calculating a temperature from the measured resistance.
16. The method of claim 14 , wherein the heater element comprises a single heater module that is coated to the aerostructure as part of an array of said heater modules.
17. The method of claim 16 , wherein the array of heater elements are connected to each other by copper traces.
18. A system for de-icing an aerostructure, comprising:
a sensing-current driving device for driving a sensing current through a heater element coated to an aerostructure, the heater element having a resistance that is temperature dependent;
a monitoring device for monitoring a resistance of the heater element;
a processing unit for determining whether there is icing at the heater element using the monitored resistance of the heater element; and
a melting-current driving device for driving a melting current through the heater element when it is determined that there is icing at the heater element,
wherein determining whether there is icing at the heater element comprises determining the resistance of the heater element at a first time based on the monitored resistance of the heater element, determining the resistance of the heater element at one or more second times based on the monitored resistance of the heater element, calculating an instantaneous rate of change of the resistance of the heater element based on the determined resistance at the first time and one or more second times, and determining that there is icing on the heater element when the calculated instantaneous rate of change of the resistance of the heater is within a predetermined threshold.
19. A system for detecting ice on a surface of an aerostructure, comprising:
a sensing-current driving device for driving a sensing current through a coil element coated to an aerostructure, the coil element having a resistance that is temperature dependent;
a monitoring device for monitoring a resistance of the coil element; and
a processing unit for determining whether there is icing at the coil element using the monitored resistance of the coil element,
wherein determining whether there is icing at the coil element comprises determining the resistance of the coil element at a first time based on the monitored resistance of the coil element, determining the resistance of the coil element at one or more second times based on the monitored resistance of the coil element, calculating an instantaneous rate of change of the resistance of the coil element based on the determined resistance at the first time and one or more second times, and determining that there is icing on the coil element when the calculated instantaneous rate of change of the resistance of the coil is within a predetermined threshold.