Inflatable airfoil device

• US 6,443,394 B1
• Filed: 09/21/2000
• Issued: 09/03/2002
• Est. Priority Date: 09/21/2000
• Status: Expired due to Fees

• Current Assignee: The B.F.Goodrich Company (Rtx Corporation)
• Original Assignee: Goodrich Corporation (Rtx Corporation)
• Inventors: Weisend, Norbert A. Jr.
• Primary Examiner(s): Poon, Peter M.
• Assistant Examiner(s): JAKEL, KEVIN W
• Application Number:
  US09/666,996
• Time in Patent Office: 712 Days
• Field of Search: 244/134.A, 244/134.R, 244/219, 244/214
• US Class Current: 244/134.00A
• CPC Class Codes: B64C 3/46 by inflatable elements
• CPC Class Codes: B64D 15/166 using pneumatic boots
• CPC Class Codes: Y02T 50/10 Drag reduction

Abstract

An airfoil device (10) for attachment to the wing (14) of an aircraft (12). The airfoil device (10) has a chamber (30) which is inflatable to provide a lift-enhancing airfoil geometry to the wing (14) and other chambers (32) which are inflatable to provide deicing forces to remove ice accumulation on the wing (14). When installed on the wing (14), the airfoil device (10) closely conforms to the wing'"'"'s airfoil geometry (e.g., low camber, sharp leading edge) when the lift-enhancing chamber (30) and the deicing chambers (32) are in a deflated condition. The lift-enhancing chamber (30) can be inflated during take-off and landing to provide a high camber and less sharp airfoil geometry. If ice accumulates on the wing (14) during high speed flight, the deicing chambers (32) can be repeatedly inflated/deflated for ice removal purposes.

Claims

1. An airfoil device for attachment to the wing of an aircraft, said airfoil device comprising:

a base layer for attachment to the wing of the aircraft;

a lift-enhancing chamber positioned over said base layer which is inflatable to provide a lift-enhancing airfoil geometry to the wing; and

deicing chambers positioned over said base layer which are inflatable to provide deicing forces to remove ice accumulation on the wing.

2. An airfoil device as set forth in claim 1, wherein the lift-enhancing chamber is shaped so that the lift-enhancing airfoil geometry has a higher camber and less sharp leading edge than an airfoil geometry provided when the lift-enhancing chamber is deflated.

3. An airfoil device as set forth in claim 2, wherein the inflated chamber has a smooth rounded shape adapted for gradual translation into a topside and an underside of the wing.

4. An airfoil device as set forth in claim 1, wherein some of the deicing chambers overlie the lift-enhancing chamber.

5. An airfoil device as set forth in claim 1, comprising a top margin and a bottom margin, and wherein the inflated deicing chambers form a spanwise row arrangement from the top margin to the bottom margin.

6. An airfoil device as set forth in claim 1, comprising a top margin and a bottom margin, and wherein the inflated deicing chambers form a dimpled matrix arrangement from the top margin to the bottom margin.

7. An airfoil device as set forth in claim 1, comprising chamber-defining layers which define the lift-enhancing chamber and the deicing chamber.

8. An airfoil device as set forth in claim 7, wherein the chamber-defining layers are made of coated fabric materials.

9. In combination, the airfoil device of claim 1 and an aircraft, the airfoil device being attached to a wing of the aircraft.

10. A combination as set forth in claim 9, wherein the wing has an airfoil geometry and wherein the airfoil device closely conforms to this airfoil geometry when the lift-enhancing chamber and the deicing chambers are in a deflated condition.

11. A combination as set forth in claim 10, wherein the wing'"'"'s airfoil geometry has a low camber and a sharp leading edge.

12. A combination as set forth in claim 9, wherein the airfoil device provides an airfoil geometry when the lift-enhancing chamber is inflated which has a higher camber and less sharp leading edge than the airfoil geometry of the wing.

13. A combination as set forth in claim 12, wherein the inflated lift-enhancing chamber has a smooth rounded shape which translates gradually into a topside and an underside of the wing, a major portion of the shape being positioned below the leading edge of the wing.

14. A method of operating an aircraft comprising the steps of:

installing the airfoil device of claim 1 on a wing of the aircraft;

inflating the lift-enhancing chamber to enhance lift; and

inflating the deicing chambers to remove ice accumulation.

15. A method as set forth in claim 14, further comprising the step of maintaining the deicing chambers in a deflated condition during inflation of the lift-enhancing chamber and maintaining the lift-enhancing chamber in a deflated condition during inflation of the deicing chambers.

16. A method as set forth in claim 15, further comprising the step of maintaining the deicing chambers in a deflated condition during inflation of the lift-enhancing chamber.

17. A method as set forth in claim 16, wherein said maintaining step comprises applying suction to the deicing chamber to maintain them in the deflated condition.

18. A method as set forth in claim 14, further comprising the step of maintaining the lift-enhancing chamber in a deflated condition during inflation of the deicing chambers.

19. A method as set forth in claim 14, further comprising the step of maintaining the lift-enhancing chamber and the deicing chambers in a deflated condition when said inflating steps are not being performed.

20. A method as set forth in claim 14, wherein said step of inflating the deicing chambers comprises repeatedly inflating and deflating the deicing chambers until ice is removed from the wings of the aircraft.

21. An airfoil device for attachment to the wing of an aircraft, said airfoil device comprising:

a lift-enhancing chamber which is inflatable to provide a lift-enhancing airfoil geometry to the wing;

deicing chambers which are inflatable to provide deicing forces to remove ice accumulation on the wing; and

.

chamber-defining layers which define the lift-enhancing chamber and the deicing chamber;

wherein two of the chamber-defining layers define the lift-enhancing chamber and another two of the chamber-defining layers define the deicing chambers.

22. An airfoil device as set forth in claim 21, wherein the deicing chamber-defining layers overlay the lift chamber-defining layers.

23. An airfoil device as set forth in claim 22, wherein the deicing chamber-defining layers extend beyond the lift chamber-defining layers in a transverse direction.

24. An airfoil device as set forth in claim 21, wherein an outermost one of the lift chamber-defining layers and an innermost one of the deicing chamber-defining layers contact each other.

25. An airfoil device as set forth in claim 24, wherein the outermost lift chamber-defining layer and the innermost deicing chamber-defining layer are unattached to each other in contacting regions overlying the lift-enhancing chamber.

26. An airfoil device as set forth in claim 21, wherein the innermost lift chamber-defining layer is made of a non-stretchable material and the other lift chamber-defining layer is made of a stretchable material.

27. An airfoil device as set forth in claim 26, further comprising a base layer adapted to be secured to the wing, the innermost lift chamber-defining layer being bonded to the base layer.

28. An airfoil device as set forth in claim 26, wherein the lift chamber-defining layers are attached to each other at spanwise perimeter edges of the lift-enhancing chamber with extensible corner pieces.

29. An airfoil device as set forth in claim 28, wherein the extensible corner pieces comprise end portions of the lift chamber-defining layer made of the stretchable material.

30. An airfoil device as set forth in claim 21, wherein the deicing chamber-defining layers are each made of a stretchable material.

31. An airfoil device as set forth in claim 30, further comprising a cover layer made of extensible material and bonded to an outermost one of the deicing chamber-defining layers.

32. An airfoil device for attachment to the wing of an aircraft, said airfoil device comprising:

a lift-enhancing chamber which is inflatable to provide a lift-enhancing airfoil geometry to the wing;

deicing chambers which are inflatable to provide deicing forces to remove ice accumulation on the wing;

chamber-defining layers which define the lift-enhancing chamber and the deicing chamber;

an inner lift chamber-defining layer made of a non-stretchable material and another lift chamber-defining layer made of a stretchable material, the lift chamber-defining layers being joined together to define the lift-enhancing chamber; and

an outer deicing chamber-defining layer made of a stretchable material and another deicing chamber-defining layer also made of a stretchable material, the deicing chamber-defining layers being joined together to define the deicing chambers.

33. An airfoil device for attachment to the wing of an aircraft, said airfoil device comprising:

a lift-enhancing chamber which is inflatable to provide a lift-enhancing airfoil geometry to the wing;

deicing chambers which are inflatable to provide deicing forces to remove ice accumulation on the wing; and

a base layer adapted to be secured to the wing and bonded to the innermost lift chamber-defining layer and a cover layer made of an extensible material and bonded to the outermost deicing chamber-defining layer.

34. An airfoil device as set forth in claim 33, comprising a top margin and a bottom margin, and wherein the base layer and the cover layer extend across the span, and transversely from the top margin to the bottom margin.

35. In combination an airfoil device and an aircraft, the airfoil device being attached to a wing of the aircraft, wherein the airfoil device comprises:

a lift-enhancing chamber which is inflatable to provide a lift-enhancing airfoil geometry to the wing;

deicing chambers which are inflatable to provide deicing forces to remove ice accumulation on the wing;

an inner lift chamber-defining layer made of a non-stretchable material and another lift chamber-defining layer made of a stretchable material, the lift chamber-defining layers being joined together to define the lift-enhancing chamber; and

an outer deicing chamber-defining layer made of stretchable material and another deicing chamber-defining layer also made of a stretchable material, the deicing chamber-defining layers being joined together to define the deicing chambers; and

a base layer bonded to the inner lift chamber-defining layer and attached to the wing.

36. A method of operating an aircraft comprising the steps of:

installing an airfoil device, comprising a lift-enhancing chamber which is inflatable to provide a lift-enhancing airfoil geometry to the wing and deicing chambers which are inflatable to provide deicing forces to remove ice accumulation on the wing, on a wing of the aircraft;

inflating the lift-enhancing chamber to enhance lift;

inflating the deicing chambers to remove ice accumulation; and

maintaining the lift-enhancing chamber in a deflated condition during inflation of the deicing chambers;

wherein said maintaining step comprises applying suction to the lift-enhancing chamber to maintain it in the deflated condition.

37. A method of operating an aircraft comprising the steps of:

installing an airfoil device, comprising a lift-enhancing chamber which is inflatable to provide a lift-enhancing airfoil geometry to the wing and deicing chambers which are inflatable to provide deicing forces to remove ice accumulation on the wing, on a wing of the aircraft;

inflating the lift-enhancing chamber to enhance lift;

inflating the deicing chambers to remove ice accumulation; and

maintaining the lift-enhancing chamber and the deicing chambers in a deflated condition when said inflating steps are not being performed;

wherein said maintaining step comprises applying suction to the lift-enhancing chamber and the deicing chambers to maintain them in their deflated conditions.

38. A method of operating an aircraft comprising the steps of:

installing an airfoil device, comprising a lift-enhancing chamber which is inflatable to provide a lift-enhancing airfoil geometry to the wing and deicing chambers which are inflatable to provide deicing forces to remove ice accumulation on the wing, on a wing of the aircraft;

inflating the lift-enhancing chamber to enhance lift; and

inflating the deicing chambers to remove ice accumulation;

wherein said step of inflating the lift-enhancing chamber is performed during take-off and/or landing and wherein said step of inflating the deicing chambers is performed between take-off and landing.

39. A method of operating an aircraft comprising the steps of:

installing an airfoil device, comprising a lift-enhancing chamber which is inflatable to provide a lift-enhancing airfoil geometry to the wing and deicing chambers which are inflatable to provide deicing forces to remove ice accumulation on the wing, on each of the wings of the aircraft;

inflating the lift-enhancing chambers to enhance lift during take-off while maintaining the deicing chambers in a deflated condition;

deflating the lift-enhancing chamber after take-off; and

inflating the deicing chambers to remove ice accumulation after take-off while maintaining the lift-enhancing chambers in a deflated condition.

40. A method as set forth in claim 39, further comprising the step of inflating the lift-enhancing chambers to enhance lift during landing while maintaining the deicing chambers in a deflated condition.