Rotatable wing tip joint and method of making same

Patent metadata

Field	Value
Publication number	US-9868517-B2
Application number	US-201414458337-A
Country	US
Kind code	B2
Filing date	Aug 13, 2014
Priority date	Aug 13, 2014
Publication date	Jan 16, 2018
Grant date	Jan 16, 2018

Abstract

A joint for coupling a wing tip to a wing base includes a linking member that extends from a first end to a second end. The linking member first end is coupleable to the wing base, and the linking member second end is coupleable to the wing tip. The linking member may be curved and may extend for a fixed distance between the wing tip and the wing base. The linking member defines first second hinge lines that are substantially parallel. The joint also includes at least two actuators. A first end of each actuator is coupled to the linking member, and a second end of each actuator is coupleable to one of the wing base and the wing tip. The actuators are operable to rotate the wing tip about the first and second hinge lines between a first orientation and a second orientation relative to the wing base.

First claim

What is claimed is:

1. A joint for coupling a wing tip to a wing base, said joint comprising:
a linking member that extends from a first end to a second end, said linking member first end is coupleable to the wing base, said linking member second end is coupleable to the wing tip, said linking member has a fixed length extending between the wing tip and the wing base, said linking member defines a first hinge line and a second hinge line, said first hinge line and said second hinge line are substantially parallel; and
at least two actuators, a first end of each of said actuators is coupled to said linking member, a second end of a first actuator of said two actuators is coupleable to one of the wing base and the wing tip and a second end of a second actuator of said two actuators is coupleable to the other one of the wing base and the wing tip, said actuators are operable to rotate the wing tip about said first and second hinge lines between a first orientation and a second orientation relative to the wing base.

2. The joint according to claim 1 , wherein said linking member comprises a curved surface between said first and second ends of said linking member, said curved surface is configured for positioning proximate an inner radius between the wing base and the wing tip in the second orientation.

3. The joint according to claim 2 , wherein said curved surface has a curvature between said first and second ends of said linking member that substantially corresponds to a curvature of the inner radius.

4. The joint according to claim 1 , wherein:
said second end of each of said actuators is linearly extendable relative to the respective first end of said actuator;
said second end of each of said actuators is movable to a first position relative to the respective first end of said actuator to position the wing tip in the first orientation; and
each said second end of each of said actuators is movable to a second position relative to the respective first end of said actuator to position the wing tip in the second orientation.

5. An aircraft comprising:
at least one wing comprising a wing base and a wing tip;
a linking member that extends from a first end to a second end, said linking member comprises a curved surface between said first and second ends, said linking member first end is coupled to said wing base, said linking member second end is coupled to said wing tip, said linking member defines a first hinge line and a second hinge line, said first hinge line and said second hinge line are substantially parallel; and
at least two actuators, a first end of each of said actuators is coupled to said linking member, a second end of a first actuator of said two actuators is coupled to one of the wing base and the wing tip and a second end of a second actuator of said two actuators is coupled to the other one of the wing base and the wing tip, said actuators are operable to rotate said wing tip about said first and second hinge lines between a first orientation and a second orientation relative to said wing base, wherein said curved surface is positioned proximate an inner radius between said wing base and said wing tip in the second orientation.

6. The aircraft according to claim 5 , wherein said linking member has a fixed length extending between said wing tip and said wing base.

7. The aircraft according to claim 5 , wherein said curved surface has a curvature between said first and second ends of said linking member that substantially corresponds to a curvature of said inner radius.

8. The aircraft according to claim 5 , wherein a flexible outer skin of said at least one wing extends between said wing base and said wing tip, a portion of said flexible outer skin defined by said inner radius is substantially smooth when said wing tip is moved between the first orientation and the second orientation.

9. The aircraft according to claim 5 , wherein:
said second end of each of said actuators is linearly extendable relative to the respective first end of said actuator;
said second end of each of said actuators is movable to a first position relative to the respective first end of said actuator to position said wing tip in the first orientation; and
each said second end of each of said actuators is movable to a second position relative to the respective first end of said actuator to position said wing tip in the second orientation.

10. A method of coupling a wing tip and a wing base, said method comprising:
coupling a first end of a linking member to the wing base;
coupling a second end of the linking member to the wing tip, wherein the linking member defines a first hinge line and a second hinge line, said linking member has a fixed length extending between the wing tip and the wing base, and the first hinge line and the second hinge line are substantially parallel;
coupling a first end of each of at least two actuators to the linking member; and
coupling a second end of a first actuator of said two actuators to one of the wing base and the wing tip and coupling a second end of a second actuator of said two actuators to the other one of the wing base and the wing tip, wherein the actuators are operable to rotate the wing tip about the first and second hinge lines between a first orientation and a second orientation relative to the wing base.

11. The method according to claim 10 , wherein the linking member includes a curved surface between the first and second ends of the linking member, said method further comprising coupling the second end of the linking member such that the curved surface is positioned proximate an inner radius between the wing base and the wing tip in the second orientation.

12. The method according to claim 11 , wherein the curved surface has a curvature between the first and second ends of said linking member, said method further comprising coupling the second end of said linking member such that the curvature of the curved surface substantially corresponds to the curvature of the inner radius.

13. The method according to claim 10 , further comprising extending a flexible outer skin between the wing base and the wing tip, wherein a portion of the flexible outer skin defined by an inner radius is substantially smooth when the wing tip is moved between the first orientation and the second orientation.

14. The method according to claim 10 , wherein the second end of each of the actuators is linearly extendable relative to the respective first end of the actuator, said method further comprises coupling the second end of each of the actuators such that:
the second end of each of the actuators is movable to a first position relative to the respective first end of the actuator to position the wing tip in the first orientation; and
the second end of each of the actuators is movable to a second position relative to the respective first end of the actuator to position the wing tip in the second orientation.

Assignees

• Boeing Co

Inventors

• Mcmahon Timothy James
• Kruse John Scott
• Kehrer Adam L

Classifications

• Y02T50/162

  Cross-Sectional Technologies · mapped topic

• B64C3/38 Primary

  Adjustment of complete wings or parts thereof · CPC title

• B64C23/065 Primary

  at the wing tips · CPC title

• B64C5/08

  mounted on, or supported by, wings · CPC title

• B64C23/072

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