Thin film heater configuration for air data probe

Patent metadata

Field	Value
Publication number	US-11745879-B2
Application number	US-202016903686-A
Country	US
Kind code	B2
Filing date	Jun 17, 2020
Priority date	Mar 20, 2020
Publication date	Sep 5, 2023
Grant date	Sep 5, 2023

Abstract

A hybrid heater system for an aircraft air data sensor includes a voltage source and a first hybrid heater set. The first hybrid heater set includes a carbon nanotube (CNT) heater, a first positive temperature coefficient (PTC) heater disposed in parallel with the CNT heater to form a parallel formation, and a second PTC heater disposed in series between the voltage source and the parallel formation.

First claim

The invention claimed is:

1. A hybrid heater system for an aircraft air data sensor, the hybrid heater system comprising:
a voltage source; and
a first hybrid heater set comprising:
a carbon nanotube (CNT) heater;
a first positive temperature coefficient (PTC) heater disposed in parallel with the CNT heater to form a first parallel formation; and
a second PTC heater disposed in series between the voltage source and the first parallel formation;
wherein an electrical resistance of the second PTC heater is greater than an electrical resistance of the first parallel formation at a temperature greater than a set temperature, and wherein the electrical resistance of the second PTC heater is less than the electrical resistance of the first parallel formation at a temperature less than the set temperature.

2. The hybrid heater system of claim 1 , wherein the first PTC heater and the second PTC heater have differing electrical resistivity.

3. The heater system of claim 1 , wherein an electrical resistance of the first parallel formation is less than an individual electrical resistance of each of the CNT heater and the first PTC heater.

4. An air data sensor comprising:
a strut assembly;
a tubular housing assembly, extending from the strut assembly; and
a hybrid heater system comprising:
a voltage source;
a first hybrid heater set comprising:
a first carbon nanotube (CNT) heater;
a first positive temperature coefficient (PTC) heater disposed in parallel with the CNT heater to form a first parallel formation; and
a second PTC heater disposed in series between the voltage source and the first parallel formation; and

a second heater set comprising:
a second CNT heater;
a third PTC heater disposed in parallel with the second CNT heater to form a second parallel formation; and
a fourth PTC heater disposed in series between the voltage source and the second parallel formation, wherein the first hybrid heater set is within the strut assembly, and the second hybrid heater set is within the housing assembly, and wherein the first hybrid heater set and the second hybrid heater set are electrically connected in series.

5. The air data sensor of claim 4 , wherein:
the first CNT heater and the first PTC heater occupy a same layer in the air data sensor, and the same layer occupied by the first CNT heater and the first PTC heater comprises:
a first terminal;
a second terminal;
first PTC heater elements extending between the first and second terminals; and
CNT heater elements interleaved between the first PTC heater elements and extending between the first and second terminals.

6. The air data sensor of claim 4 , further comprising:
an outermost probe surface;
a first film adhesive and insulation layer underlying the outermost probe surface;
a first heater layer underlying the first film adhesive and insulation layer, the first heater layer comprising CNT heater elements of the first CNT heater and first PTC heater elements of the first PTC heater;
a second film adhesive and insulation layer underlying the first heater layer;
a second heater layer underlying the second film adhesive and insulation layer, the second heater layer comprising a second PTC heater;
a third film adhesive and insulation layer underlying the second heater layer; and
a sleeve surface underlying the third film adhesive and insulation layer.

7. The air data sensor of claim 4 , wherein the first CNT heater and the first PTC heater occupy different layers in the air data sensor.

8. The air data sensor of claim 4 , further comprising:
an outermost probe surface;
a first film adhesive and insulation layer underlying the outermost probe surface;
a first heater layer underlying the first film adhesive and insulation layer, the first heater layer comprising the first CNT heater;
a second film adhesive and insulation layer underlying the first heater layer;
a second heater layer underlying the second film adhesive and insulation layer, the second heater layer comprising one of the first or second PTC heaters;
a third film adhesive and insulation layer underlying the second heater layer;
a third heater layer underlying the third film adhesive and insulation layer, the third heater layer comprising the other of the first or second PTC heaters;
a fourth film adhesive and insulation layer underlying the third heater layer; and
a sleeve surface underlying the fourth film adhesive and insulation layer.

9. A hybrid heater system for ice protection of an air data probe on an aircraft, the hybrid heater system comprising:
a voltage source;
a carbon nanotube (CNT) heater comprising CNT heater elements;
a first positive temperature coefficient (PTC) heater disposed in parallel with the CNT heater to form a parallel formation, wherein the first PTC heater comprises first PTC heater elements interleaved with the CNT heater elements in a first air data probe layer; and
a second PTC heater disposed in a second air data probe layer and in series between the voltage source and the parallel formation;
wherein an electrical resistance of the second PTC heater is greater than an electrical resistance of the parallel formation at a temperature greater than a set temperature, and wherein the electrical resistance of the second PTC heater is less than the electrical resistance of the first parallel formation at a temperature less than the set temperature.

10. The hybrid heater system of claim 9 , wherein the second PTC heater establishes the maximum temperature capability for ice protection, and the hybrid heater system operates with an absence of active temperature controls.

11. The hybrid heater system of claim 9 , wherein the first PTC heater and the second PTC heater have differing electrical resistivity.

12. The heater system of claim 9 , wherein an effective electrical resistance of the parallel formation is less than an electrical resistance of each of the CNT heater and the first PTC heater.

13. The hybrid heater system of claim 9 , wherein the first air data probe layer comprises first and second terminals between which the interleaved CNT and first PTC heater elements extend.

14. The hybrid heater system according to claim 9 , wherein the second air data probe layer underlies the first air data probe layer.

15. A method of making a heater for an air data probe comprising:
positioning on the air data probe a first heater layer comprising a carbon nanotube (CNT) heater element and a first positive temperature coefficient (PTC) heater element interleaved with one another;
positioning on the air data probe a second heater layer comprising a second PTC heater element;
wiring the first heater layer so that the CNT heater element and the first PTC heater element are in parallel with one another defining a parallel formation; and
wiring the second heater layer so that the second PTC heater element is in series with the parallel formation and a voltage source.

16. The method of claim 15 , wherein the second PTC heater element establishes a maximum temperature capability for ice protection, and the hybrid heater system operates with an absence of active temperature controls.

17. The method of claim 15 , wherein the first PTC heater element and the second PTC heater element have differing electrical resistivity.

18. The method of claim 15 , wherein an effective electrical resistance of the parallel formation is less than an electrical resistance of each of the CNT heater element and the first PTC heater element.

Assignees

• Rosemount Aerospace Inc

Inventors

• Jacob Robin
• Mahapatra Guru Prasad

Classifications

• B64D15/12 Primary

  by electric heating (heating arrangements specially adapted for transparent or reflecting areas H05B3/84) · CPC title

• H05B3/145

  Carbon only, e.g. carbon black, graphite · CPC title

• H05B2203/013

  Heaters using resistive films or coatings · CPC title

• H05B2203/017

  Manufacturing methods or apparatus for heaters · CPC title

• H05B2203/02

  Heaters using heating elements having a positive temperature coefficient · CPC title