Lifting surfaces and associated method

• US 10,343,763 B2
• Filed: 12/18/2015
• Issued: 07/09/2019
• Est. Priority Date: 12/19/2014
• Status: Active Grant

• Current Assignee: Airbus Operations Limited (Airbus SE)
• Original Assignee: Airbus Operations Limited (Airbus SE)
• Inventors: Cross, Murray
• Primary Examiner(s): Shanske, Jason D
• Assistant Examiner(s): Adjagbe, Maxime M
• Application Number:
  US14/975,493
• Publication Number:
  US 20160176506A1
• Time in Patent Office: 1,299 Days
• CPC Class Codes: B64C 23/076 the wing tip airfoil devices comprising one or more separate moveable members thereon affecting the vortices, e.g. flaps
• CPC Class Codes: B64C 27/463 Blade tips
• CPC Class Codes: B64C 9/00 Adjustable control surfaces or members, e.g. rudders trimming stabilising surfaces B64C5/10
• CPC Class Codes: F03B 3/123 specially designed as adjustable blades, e.g. for Kaplan-type turbines
• CPC Class Codes: F03D 1/0633 of the blades
• CPC Class Codes: F03D 7/0228 of the blade tips only
• CPC Class Codes: F04D 29/28 for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
• CPC Class Codes: F04D 29/38 Blades for axial flow compressors F04D29/324
• CPC Class Codes: Y02E 10/72 Wind turbines with rotation axis in wind direction
• CPC Class Codes: Y02T 50/10 Drag reduction

Abstract

An arrangement of lifting surfaces including a primary lifting surface having a flexural axis extending in the spanwise direction of the lifting surface, a root, and a tip. A first tip device is attached to the tip and has a first lifting surface. A second tip device is attached to the tip and has a second lifting surface. A control system is coupled to the first and second tip devices for moving the first and second lifting surfaces relative to the tip or for actively controlling circulation of the first and second lifting surfaces. The control system is operable to change a value of torque effective at the primary lifting surface about the flexural axis.

Claims

1. An arrangement of lifting surfaces comprising:

a primary lifting surface including a flexural axis extending in the spanwise direction of the primary lifting surface, a root, and a tip;

a first tip device attached to the tip and including a first lifting surface, and

a second tip device attached to the tip and having a second lifting surface, and

a control system coupled to the first and second tip devices configured to move the first and second lifting surfaces relative to the tip by moving at least one of the first and second tip devices relative to the primary lifting surface or actively control circulation of the first and second lifting surfaces;

wherein the control system is configured to operate in a first mode to operably change a value of torque effective at the primary lifting surface about the flexural axis by actively controlling the first or second lifting surfaces while maintaining a substantially constant value of lift generated by the first and second tip devices.

2. The arrangement according to claim 1, wherein the first lifting surface is configured to be moved mechanically independently of the second lifting surface.

3. The arrangement according to claim 1, wherein the first lifting surface is configured to move relative to the primary lifting surface in a first direction, and the second lifting surface is configured to move relative to the primary lifting surface in a second direction opposite the first direction.

4. The arrangement according to claim 3, wherein the first lifting surface is mechanically linked to the second lifting surface.

5. The arrangement according to claim 1, wherein the control system is operable in a second mode of operation in which the first and second lifting surfaces are actively controlled to change a value of lift generated by the first and second tip devices whilst maintaining a value of torque effective at the primary lifting surface about the flexural axis substantially constant.

6. The arrangement according to claim 1, wherein the first tip device has a leading edge and a trailing edge, and the first lifting surface extends full chord between the leading edge and the trailing edge of the first tip device.

7. The arrangement according to claim 6, wherein the arrangement further comprises an actuator for rotating the first lifting surface relative to the tip.

8. The arrangement according to claim 6, wherein the arrangement further comprises an actuator for morphing the first lifting surface.

9. The arrangement according to claim 1, wherein the first tip device has a leading edge and a trailing edge, the first lifting surface extends only part chord between the leading and trailing edges, and the first tip device has a third lifting surface fixed with respect to the primary lifting surface.

10. The arrangement according to claim 9, wherein the first lifting surface is hinged with respect to the third lifting surface and the first lifting surface rotates bout the hinge.

11. The arrangement according to claim 1, wherein the second tip device has a leading edge and a trailing edge, and the second lifting surface extends full chord between the leading and trailing edges of the second tip device.

12. The arrangement according to claim 11, wherein the arrangement further comprises an actuator for rotating the second lifting surface relative to the tip.

13. The arrangement according to claim 11, wherein the arrangement further comprises an actuator for morphing the second lilting surface.

14. The arrangement according to claim 1, wherein the second tip device has a leading edge and a trailing edge, the second lifting surface extends only part chord between the leading and trailing edges, and the second tip device has a fourth lifting surface fixed with respect to the primary lifting surface.

15. The arrangement according to claim 14, wherein the second lifting surface is hinged with respect to the fourth lifting surface and the second lifting surface rotates about the hinge.

16. The arrangement according to claim 1, wherein the first and second lifting surfaces each include at least one aperture, and the control system is configured to control movement of fluid through the at least one aperture of the first and second lifting surfaces to provide active circulation control.

17. The arrangement according to claim 1, wherein the first tip device is swept forwards and the second tip device is swept backwards.

18. The arrangement according to claim 1, wherein the first tip device is swept backwards and the second tip device is swept backwards.

19. The arrangement according to claim 1, wherein the first tip device is swept forwards and the second tip device is swept forwards.

20. The arrangement according to claim 1, wherein the primary lifting surface is swept backwards.

21. The arrangement according to claim 1, wherein the primary lifting surface is swept forwards.

22. The arrangement according to claim 1, wherein the primary lifting surface is unswept.

23. The arrangement according to claim 1, wherein the first tip device is located forward of the flexural axis and the second tip device is located aft of the flexural axis.

24. The arrangement according to claim 1, wherein the primary lifting surface defines a wing plane, and the first and second tip devices are substantially co-planar with the wing plane.

25. The arrangement according to claim 1, wherein the first and second tip devices are located in different planes.

26. An arrangement according to claim 25, wherein the first and second tip devices are located in intersecting planes.

27. An arrangement according to claim 25, wherein the primary lifting surface, the first tip device and the second tip device are each located in different parallel planes.

28. The arrangement according to claim 27, wherein the first tip device is mounted on a first pylon extending from the tip of the primary lifting surface, and the second tip device is mounted on a second pylon extending from the tip of the primary lifting surface.

29. The arrangement according to claim 1, wherein the primary lifting surface is one of a wing of a fixed wing aircraft, a wing of a rotary wing aircraft, a wind turbine blade, a compressor blade, a propeller or a hydrofoil.

30. A method of controlling an arrangement of lifting surfaces, the arrangement comprising:

a primary lifting surface having a flexural axis extending in a spanwise direction of the primary lifting surface, a root, and a tip;

a first tip device attached to the tip and having a first lifting surface; and

a second tip device attached to the tip and having a second lifting surface, and

a control system coupled to the first and second tip devices;

the method comprising a first mode of operation which includes at least one of a) moving at least one of the first and second lifting surfaces relative to the tip, and b) actively controlling circulation of the first and second lifting surfaces,

wherein the first mode of operation changes a value of torque effective at the primary lifting surface about the flexural axis, while maintaining a substantially constant value of lift generated by the first and second tip devices.

31. The method according to claim 30, comprising moving the first lifting surface mechanically independently of the second lifting surface.

32. The method according to claim 30, comprising moving the first lifting surface relative to the primary lifting surface in a first direction, and moving the second lifting surface relative to the primary lifting surface in a second direction opposite the first direction.

33. The method according to claim 32, wherein the movement of the first lifting surface is mechanically linked to movement of the second lifting surface.

34. The method according to claim 30, further comprising a second mode of operation including moving the first and second lifting surfaces to change a value of lift generated by the first and second tip devices whilst maintaining a value of torque effective at the primary lifting surface about the flexural axis substantially constant.

35. The method according to claim 30, further comprising rotating the first lifting surface relative to the tip.

36. The method according to claim 30, further comprising rotating the second lifting surface relative to the tip.

37. The method according to claim 30, further comprising controlling movement of fluid through at least one aperture in each of the first and second lifting surfaces to provide active circulation control.

38. The method according to claim 30, wherein the arrangement of lifting surfaces is provided at each of a port side and a starboard side of an aircraft, and the method comprises changing a value of torque effective at the respective port and starboard primary lifting surfaces about their flexural axes to effect one or more of:

i) roll control of the aircraft;

ii) yaw control of the aircraft;

iii) pitch control of the aircraft;

iv) tip vortex control; and

v) drag control.