Enhancing aerodynamic performance of an aircraft wing assembly

Patent metadata

Field	Value
Publication number	US-2016137285-A1
Application number	US-201615007172-A
Country	US
Kind code	A1
Filing date	Jan 26, 2016
Priority date	Oct 30, 2012
Publication date	May 19, 2016
Grant date	—

Abstract

Disclosed is a method of enhancing aerodynamic performance of an aircraft wing assembly including a fixed section and a foldable section. The foldable section is hinged to the fixed section at a hinge axis. The method includes turning a torque box extending from the foldable section to rotate the foldable section about the hinge axis from a stowed position to a deployed position.

First claim

1 . A method of enhancing aerodynamic performance of an aircraft wing assembly including a fixed section and a foldable section, the foldable section hinged to the fixed section at a hinge axis, the method comprising turning a torque box extending from the foldable section to rotate the foldable section about the hinge axis from a stowed position to a deployed position.

2 . The method of claim 1 , wherein the torque box is hinged to at least one other torque box extending in an outboard direction from the fixed section, and wherein the hinge axis extends through sides of the torque boxes.

3 . The method of claim 1 , further comprising latching the torque box after the foldable section has been rotated to the deployed position.

4 . The method of claim 3 , wherein the torque box extending from the folding section is latched to at least one of the fixed section and the torque box extending from the fixed section.

5 . The method of claim 3 , when latching the torque box includes using latch pins to engage the torque box extending from the foldable section.

6 . The method of claim 3 , when latching the torque box includes extending latch pins through a closeout rib of the fixed section to engage the torque box extending from the foldable section.

7 . The method of claim 1 , wherein the aircraft wing assembly is part of an aircraft, and wherein the foldable section is rotated to the deployed position while the aircraft is on a runway prior to takeoff.

8 . The method of claim 7 , wherein the torque box is turned about the hinge axis to rotate the foldable section back to the stowed position after the aircraft has landed.

9 . The method of claim 7 , wherein the foldable section is in the stowed position while the aircraft is moved from a gate area to the runway.

10 . The method of claim 1 , wherein rotary actuators are used to turn the torque box about the hinge axis.

11 . The method of claim 1 , wherein the foldable section is a raked wing tip.

12 . A method of enhancing aerodynamic performance of an aircraft, wherein the aircraft has a wing assembly including a wing tip having a first torque box, and a fixed section having a second torque box extending outward in a spanwise direction, the first and second torque boxes hinged together about a hinge axis, and wherein enhancing the aerodynamic performance includes:
turning the first torque box about the hinge axis to fold the wing tip from a stowed position to a deployed position; and latching the first torque box after the wing tip has been folded to the deployed position.

13 . The method of claim 12 , wherein the first torque box is latched to the fixed section.

14 . The method of claim 12 , when latching the first torque box includes using latch pins to engage the first torque box.

15 . The method of claim 12 , when latching the first torque box includes extending latch pins through a closeout rib of the wing tip to engage the first torque box.

16 . The method of claim 12 , wherein rotary actuators are used to turn the first torque box about the hinge axis.

17 . The method of claim 12 , wherein the wing tip is folded to the deployed position while the aircraft is on a runway prior to takeoff.

18 . The method of claim 17 , wherein the first torque box is turned about the hinge axis to fold the wing tip back to the stowed position after the aircraft has landed.

19 . The method of claim 17 , wherein the wing tip is in the stowed position while the aircraft is moved from a gate area to the runway.

Assignees

• Boeing Co

Inventors

• Good Mark S
• Walker Steven Paul

Classifications

• B64C3/56 Primary

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

• Y02T50/10

  Drag reduction · CPC title