Passively actuated fluid foil

Patent metadata

Field	Value
Publication number	US-11084566-B2
Application number	US-201816220021-A
Country	US
Kind code	B2
Filing date	Dec 14, 2018
Priority date	Dec 18, 2017
Publication date	Aug 10, 2021
Grant date	Aug 10, 2021

Abstract

A fluid foil has a main fixed portion and a tip portion movably mounted at a tip end of the main fixed portion. The main fixed portion has an upper surface and a lower surface, and the tip portion has an upper surface and a lower surface. The fluid foil is operable in: a) a first configuration in which the upper surface of the tip portion is angled downwardly with respect to the upper surface of the main fixed portion; and b) a second configuration in which the tip portion is rotated upwardly with respect to the first configuration such that the upper surface of the tip portion and the upper surface of the main fixed portion are substantially continuous surfaces. The movement of the tip portion with respect to the main fixed portion is exclusively passively actuated by movement of the foil with respect to a surrounding fluid.

First claim

The invention claimed is:

1. An aircraft including a wing, the wing comprising:
a main fixed portion and a tip portion movably mounted at a tip end of the main fixed portion via a flexible element or hinge,
wherein the main fixed portion has an upper surface and a lower surface, and the tip portion has an upper surface and a lower surface, and the aircraft is operable in:
a) a first configuration in which the upper surface of the tip portion is entirely angled downwardly with respect to the upper surface of the main fixed portion; and
b) a second configuration in which the tip portion is rotated upwardly with respect to the first configuration such that the upper surface of the tip portion and the upper surface of the main fixed portion are aligned in a spanwise direction across a junction between the tip portion and the main fixed portion,

wherein the movement of the tip portion with respect to the main fixed portion from the first configuration to the second configuration is exclusively passively actuated by movement of the aircraft with respect to a surrounding air flow, and
wherein the tip portion is biased by the flexible element or hinge towards the first configuration during relative forward movement of the aircraft through the surrounding air flow which is below a predetermined forward air speed.

2. The aircraft according to claim 1 , wherein the aircraft is operable in:
c) a third configuration in which the upper surface of the tip portion is angled upwardly with respect to the upper surface of the main fixed portion.

3. The aircraft according to claim 1 , wherein the wing has a span, and the span increases between the first configuration and the second configuration.

4. The aircraft according to claim 1 , wherein the flexible element or hinge includes a variable spring.

5. The aircraft according to claim 1 , wherein the first configuration corresponds to a downward-most position of the tip portion.

6. The aircraft according to claim 1 , wherein the tip portion includes a first lifting surface having the upper surface and the lower surface of the tip portion, and the tip portion further comprises one or more secondary lifting surfaces.

7. A fluid foil comprising
a main fixed portion and a tip portion movably mounted at a tip end of the main fixed portion,
wherein the main fixed portion has an upper surface and a lower surface, and the tip portion has an upper surface and a lower surface, and the fluid foil is operable in:
a) a first configuration in which the upper surface of the tip portion is angled downwardly with respect to the upper surface of the main fixed portion; and
b) a second configuration in which the tip portion is rotated upwardly with respect to the first configuration such that the upper surface of the tip portion and the upper surface of the main fixed portion are aligned in a spanwise direction across a joint between the tip portion and the main fixed portion,

wherein the movement of the tip portion with respect to the main fixed portion is exclusively passively actuated by movement of the foil with respect to a surrounding fluid, and
wherein the tip portion is configured to rotate about a pitch axis as the tip portion is rotated upwardly with respect to the first configuration.

8. A method of operating an aircraft having a main fixed portion and a tip portion movably mounted at a tip end of the main fixed portion via a flexible element or hinge, wherein the main fixed portion has an upper surface and a lower surface, and the tip portion has an upper surface and a lower surface, and method includes:
moving the tip portion into a first configuration in which the upper surface of the tip portion is entirely angled downwardly with respect to the upper surface of the main fixed portion;
moving the tip portion into a second configuration in which the tip portion is rotated upwardly with respect to the first configuration such that the upper surface of the tip portion and the upper surface of the main fixed portion are aligned in a spanwise direction across a junction between the wing tip portion and the main fixed portion,
wherein the movement of the tip portion with respect to the main fixed portion from the first configuration to the second configuration is exclusively passively actuated by movement of the aircraft with respect to a surrounding air, and
the flexible element or the hinge biasing the tip portion to remain in a downward-most position during relative forward movement of the aircraft through the surrounding air which is below a predetermined forward speed.

9. The method according to claim 8 , further comprising placing the aircraft in:
c) a third configuration in which the upper surface of the tip portion is angled upwardly with respect to the upper surface of the main fixed portion.

10. The method according to claim 8 , further comprising biasing the tip portion towards the first configuration.

11. The method according to claim 10 , further comprising varying a spring force applied by the flexible element or the hinge to the tip portion as the tip portion rotates upwardly with respect to the first configuration.

12. The method according to claim 8 , further comprising rotating the tip portion about a pitch axis as the tip portion is rotated upwardly with respect to the first configuration.

13. The method according to claim 12 , further comprising reducing an angle of incidence of the tip portion as the tip portion is rotated upwardly with respect to the first configuration.

Assignees

• Airbus Sas

Inventors

• Orchard Matthew

Classifications

• B64C3/56 Primary

  Folding or collapsing to reduce overall dimensions of aircraft · CPC title

• B64C23/072

  the wing tip airfoil devices being moveable in their entirety · CPC title

• B63B1/248 Primary

  Shape, hydrodynamic features, construction of the foil · CPC title

• B64C27/473

  Constructional features · CPC title

• B64C3/52

  Warping · CPC title