Electrothermal heater
An electrothermal heater for an ice protection system includes a laminated heater mat which comprises a primary heater element layer, a secondary heater element layer, and at least one dielectric layer interposed between the primary and secondary heater element layers, and control apparatus which comprises power supply apparatus and a current detector. The control apparatus is configured to have (i) a first mode in which the power supply apparatus supplies a heater current to the primary heater element layer and does not supply a heater current to the secondary heater element layer and the current detector monitors the secondary heater element layer for detecting a leakage current of the heater current of the primary heater element layer indicative of burn-out of the primary heater element layer and (ii) a second mode in which the power supply apparatus supplies a heater current to the secondary heater element layer and does not supply a heater current to the primary heater element layer. The control apparatus is configured to switch from the first mode to the second mode in response to detection of said leakage current by the current detector.
1. An electrothermal heater for an ice protection system, the heater comprising:
a laminated heater mat comprising a primary heater element layer, a secondary heater element layer, and at least one dielectric layer interposed between the primary and secondary heater element layers; and
a control apparatus comprising a power supply apparatus and a current detector;
wherein the control apparatus is configured to have (i) a first mode in which the power supply apparatus supplies a heater current to the primary heater element layer and does not supply a heater current to the secondary heater element layer, and the current detector monitors the secondary heater element layer for detecting a leakage current of the heater current of the primary heater element layer indicative of burn-out of the primary heater element layer, and (ii) a second mode in which the power supply apparatus supplies a heater current to the secondary heater element layer and does not supply a heater current to the primary heater element layer;
wherein the control apparatus is configured to switch from the first mode to the second mode in response to detection of said leakage current by the current detector; and
wherein the secondary heater element layer functions as a temporary ground plane in the first mode and as a heater in the second mode.
2. The electrothermal heater of claim 1 , wherein:
the secondary heater element layer comprises a plurality of heater elements; and
the control apparatus is arranged, in the first mode, to connect the heater elements together electrically and, when switching from the first mode to the second mode, to re-configure the heater elements as electrically separate heater elements.
3. The electrothermal heater of claim 1 , wherein the control apparatus includes a switch device which, in the first mode, connects the secondary heater element layer to an earth line and, in the second mode, connects the secondary heater element layer to a power supply line of the power supply apparatus.
4. The electrothermal heater of claim 3 , wherein the current detector comprises a sensor positioned to detect leakage current in the earth line.
5. The electrothermal heater of claim 1 , wherein the current detector comprises a Hall-effect current sensor or a current transformer.
6. The electrothermal heater of claim 1 , wherein the power supply apparatus has a first power supply line for supplying power to the primary heater element layer and a second power supply line for supplying power to the secondary heater element layer.
7. The electrothermal heater of claim 6 , wherein a control unit of the control apparatus is configured in the first mode to connect the first power supply line and to disconnect the second power supply line, and in the second mode to disconnect the first power supply line and to connect the second power supply line.
8. The electrothermal heater of claim 1 , wherein the heater mat does not include a ground plane in addition to the secondary heater element layer.
9. The apparatus of claim 1 , wherein the secondary heater element layer, when functioning as a temporary ground plane in the first mode, diverts a leakage current from the primary heater element when the primary heater element layer experiences burn-out.
10. An electrothermal heater for an ice protection system, the heater comprising:
a laminated heater mat comprising a primary heater element layer, a secondary heater element layer, and at least one dielectric layer interposed between the primary and secondary heater element layers; and
a control apparatus comprising a power supply apparatus and a current detector;
wherein:
the control apparatus is configured to have (i) a first mode in which the power supply apparatus supplies a heater current to the primary heater element layer and does not supply a heater current to the secondary heater element layer, and the current detector monitors the secondary heater element layer for detecting a leakage current of the heater current of the primary heater element layer indicative of burn-out of the primary heater element layer, and (ii) a second mode in which the power supply apparatus supplies a heater current to the secondary heater element layer and does not supply a heater current to the primary heater element layer;
the control apparatus is configured to switch from the first mode to the second mode in response to detection of said leakage current by the current detector;
the control apparatus includes a switch device which, in the first mode, connects the secondary heater element layer to an earth line and, in the second mode, connects the secondary heater element layer to a power supply line of the power supply apparatus;
the control apparatus comprises a control unit; and
the switch device comprises a switch and a relay which is configured to be responsive to a command signal of the control unit produced in response to detection of said leakage current by the current detector so as to switch the switch from being in the first mode to being in the second mode.
11. The apparatus of claim 10 , wherein the switch of the switch device connects the secondary heater element layer to an earth line in the first mode and connects the secondary heater element layer to a power supply line of the power supply apparatus in the second mode.
12. An apparatus, comprising:
an aircraft component comprising an aerodynamic external panel and an electrothermal heater, the heater including:
a laminated heater mat comprising a primary heater element layer, a secondary heater element layer, and at least one dielectric layer interposed between the primary and secondary heater element layers; and
a control apparatus comprising a power supply apparatus and a current detector;
wherein the control apparatus is configured to have (i) a first mode in which the power supply apparatus supplies a heater current to the primary heater element layer and does not supply a heater current to the secondary heater element layer, and the current detector monitors the secondary heater element layer for detecting a leakage current of the heater current of the primary heater element layer indicative of burn-out of the primary heater element layer, and (ii) a second mode in which the power supply apparatus supplies a heater current to the secondary heater element layer and does not supply a heater current to the primary heater element layer;
wherein the control apparatus is configured to switch from the first mode to the second mode in response to detection of said leakage current by the current detector;
wherein the secondary heater element layer functions as a temporary ground plane in the first mode and as a heater in the second mode; and
wherein the electrothermal heater mat of the electrothermal heater is bonded to a surface of the external panel.
13. The apparatus of claim 12 , wherein the external panel is an erosion shield.
14. The apparatus of claim 12 , further comprising an aircraft that includes the aircraft component, wherein the aircraft includes an aircraft earth, and the control apparatus is configured so that, in the first mode, the secondary heater element layer is connected to the aircraft earth and, in the second mode, the secondary heater element layer is not connected to the aircraft earth.