Hybrid acoustic and induction-heating systems and methods for impeding formation of ice

Patent metadata

Field	Value
Publication number	US-10118705-B2
Application number	US-201615183563-A
Country	US
Kind code	B2
Filing date	Jun 15, 2016
Priority date	Jun 15, 2016
Publication date	Nov 6, 2018
Grant date	Nov 6, 2018

Abstract

An airfoil comprises a skin, comprising an external surface and an internal surface, opposite the external surface. The skin is magnetically and electrically conductive. The airfoil also comprises an interior space, formed by the skin. The internal surface faces the interior space. The airfoil additionally comprises a leading edge along the external surface. The airfoil further comprises a hybrid acoustic induction-heating system, configured to impede formation of ice on the external surface. The hybrid acoustic induction-heating system comprises an induction coil within the interior space. At least a portion of the induction coil is sufficiently close to the internal surface to produce an eddy current in the skin when an alternating electrical current is flowing in the induction coil. The hybrid acoustic induction-heating system also comprises at least one magnet within the interior space. At least the one magnet is configured to produce a steady-state magnetic field within the skin.

First claim

What is claimed is:

1. An airfoil, comprising:
a skin, comprising an external surface and an internal surface, opposite the external surface, wherein the skin is magnetically and electrically conductive;
an interior space, formed by the skin, wherein the internal surface of the skin faces the interior space;
a leading edge along the external surface of the skin; and
a hybrid acoustic induction-heating system, configured to impede formation of ice on the external surface of the skin and comprising:
an induction coil within the interior space, wherein at least a portion of the induction coil is sufficiently close to the internal surface of the skin to produce an eddy current in the skin when an alternating electrical current is flowing in the induction coil to inductively heat the skin; and
at least one magnet within the interior space, wherein at least the one magnet is configured to produce a steady-state magnetic field within the skin to interact with the eddy current to generate acoustic vibrations within the skin.

2. The airfoil according to claim 1 , wherein, at a location in the skin, the steady-state magnetic field, produced by at least the one magnet, is transverse to the eddy current.

3. The airfoil according to claim 1 , wherein at least the portion of the induction coil is parallel to the skin.

4. The airfoil according to claim 1 , wherein at least the portion of the induction coil is closer to the leading edge than any other portion of the induction coil and is positioned to heat the leading edge.

5. The airfoil according to claim 1 , wherein at least the portion of the induction coil is transverse to the leading edge.

6. The airfoil according to claim 1 , wherein at least the portion of the induction coil is parallel to the leading edge.

7. The airfoil according to claim 1 , wherein the steady-state magnetic field, produced by at least the one magnet, is transverse to at least the portion of the induction coil.

8. The airfoil according to claim 1 , wherein the steady-state magnetic field, produced by at least the one magnet, is transverse to the skin at the internal surface of the skin.

9. The airfoil according to claim 1 , wherein the steady-state magnetic field, produced by at least the one magnet, is transverse to a portion of the internal surface of the skin that is closest to the leading edge.

10. The airfoil according to claim 1 , wherein the steady-state magnetic field, produced by at least the one magnet, is parallel to the leading edge at a portion of the internal surface of the skin that is closest to the leading edge.

11. The airfoil according to claim 1 , wherein the induction cod has a sheet form.

12. The airfoil according to claim 1 , wherein the induction coil has a volumetric form.

13. The airfoil according to claim 1 , wherein the airfoil is selected from the group consisting of a wing, an erosion shied, an empennage, a horizontal stabilizer, a vertical stabilizer, a winglet, a turbine-engine inlet, an engine nacelle, and a turbine blade.

14. The airfoil according to claim 1 , wherein at least the one magnet is a permanent magnet.

15. The airfoil according to claim 1 , wherein at least the one magnet is an electromagnet.

16. The airfoil according to claim 1 , wherein at least the one magnet is a plurality of magnets.

17. The airfoil according to claim 1 , wherein the steady-state magnetic field, produced by at least the one magnet, has a magnitude greater than 0.1 T (tesla) and less than 100 T.

18. The airfoil according to claim 1 , wherein the skin comprises a nickel-iron alloy.

19. The airfoil according to claim 1 , wherein the skin has a thickness of less than 1 mm and greater than 0.001 mm.

20. The airfoil according to claim 1 , wherein the skin is ferromagnetic.

21. The airfoil according to claim 1 , wherein the skin has relative magnetic permeability of greater than 1,000 and less than 10,000,000.

22. The airfoil according to claim 1 , wherein Curie temperature of the skin is less than 300° C. and greater than 50° C.

23. The airfoil according to claim 1 , further comprising a control system, wherein:
the skin has a controlled region, in which the eddy current is produced when the alternating electrical current is flowing in the induction coil, and
the control system is configured to supply the alternating electrical current to the induction coil to generate inductive heat and acoustic pressure in the controlled region of the skin.

24. The airfoil according to claim 23 , wherein the control system is configured to supply the alternating electrical current to the induction coil based, at least part, on an ambient temperature at an altitude of the airfoil.

25. The airfoil according to claim 23 , wherein the control system is configured to supply the alternating electrical current based, at least in part, on an ambient temperature of a layer of fluid flowing over the external surface of the skin.

26. The airfoil according to claim 25 , further comprising a temperature sensor, configured to measure the ambient temperature of the layer of fluid flowing over the external surface of the skin.

27. The airfoil according to claim 23 , wherein the alternating electrical current generates an alternating magnetic field with an amplitude that is less than a magnitude of the steady-state magnetic field.

28. The airfoil according to claim 27 , wherein a ratio of the amplitude of the alternating magnetic field to the magnitude of the steady-state magnetic field is less than 0.1and greater than 0.0001.

29. The airfoil according to claim 23 , wherein the control system comprises:
a power supply, configured to supply the alternating electrical current to the induction coil; and
a controller, programmed to:
receive signals, representative of first ambient conditions known to cause formation of the ice on the external surface of the skin and second ambient conditions known to impede formation of the ice on the external surface, wherein the first ambient conditions and the second ambient conditions both comprise an ambient temperature of a layer of fluid flowing over the external surface of the skin,
cause the power supply to supply the alternating electrical current to the induction coil to generate inductive heat and acoustic pressure in the controlled region of the skin based upon the first ambient conditions, and
cause the power supply to discontinue supplying the alternating electrical current to the induction coil based upon the second ambient conditions.

30. The airfoil according to claim 29 , wherein the controller is further programmed to cause the power supply to supply the alternating electrical current to the induction coil when the ambient temperature of the layer of fluid flowing over the external surface of the skin is below a first threshold temperature.

31. The airfoil according to claim 30 , wherein the first threshold temperature is above freezing point of water and below 5° C.

32. The airfoil according to claim 30 , wherein the controller is further programmed to cause the power supply to discontinue supplying the alternating electrical current to the induction coil when the ambient temperature of the layer of fluid flowing over the external surface of the skin is above a second threshold temperature.

33. The airfoil

Assignees

• Boeing Co

Inventors

• Hull John Ralph
• Tanielian Minas H

Classifications

• H05B2214/02

  Heaters specially designed for de-icing or protection against icing · CPC title

• H05B6/105

  using a susceptor · CPC title

• B64D15/12 Primary

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

• B64D15/20

  Means for detecting icing or initiating de-icing · CPC title

• B64D15/163

  using electro-impulsive devices · CPC title