Aircraft wing with aileron

Patent metadata

Field	Value
Publication number	US-2018099735-A1
Application number	US-201715730285-A
Country	US
Kind code	A1
Filing date	Oct 11, 2017
Priority date	Oct 12, 2016
Publication date	Apr 12, 2018
Grant date	—

Abstract

An aircraft wing having a fixed wing with a wing tip device. The wing tip device is movable between a flight configuration for use during flight, and a ground configuration for use during ground-based operations. The wing has a master flight control surface associated with the fixed wing and a slave flight control surface associated with the wing tip device. An interface between the master flight control surface and the slave flight control surface is arranged to provide a rigid connection between the master flight control surface and slave flight control surface when the wing tip device is in the flight configuration. Moving the master control surface about a control axis causes the slave control surface to be moved about the control axis. The interface is arranged to de-couple the slave and master control surfaces when the wing tip device is moved from the flight configuration into the ground configuration.

First claim

1 . An aircraft wing, the aircraft wing comprising:
a fixed wing with a wing tip device at a tip of the fixed wing, wherein the wing tip device is movable between: a flight configuration for use during flight, and a ground configuration for use during ground-based operations, in which the wing tip device moves from the flight configuration to the ground configuration such that the span of the aircraft wing is reduced, the wing further comprising a master flight control surface associated with the fixed wing and a slave flight control surface associated with the wing tip device, with an interface between the master flight control surface and the slave flight control surface, wherein the interface is arranged to provide a rigid connection between the master flight control surface and slave flight control surface when the wing tip device is in the flight configuration and the master control surface is moved about a control axis common to both of the master flight control surface and the slave flight control surface, such that the slave control surface is also caused to be moved about the control axis, and wherein the interface is further arranged such that the slave control surface decouples from the master control surface when the wing tip device is moved from the flight configuration into the ground configuration.

2 . The aircraft wing as claimed in claim 1 , wherein the flight control surfaces are located at the trailing edge of the wing.

3 . The aircraft wing as claimed in claim 1 , wherein the flight control surfaces are ailerons.

4 . The aircraft wing as claimed in claim 1 , wherein the flight control surfaces are located at a leading edge of the wing.

5 . The aircraft wing as claimed in claim 1 , wherein the flight control surfaces are slats or flaps

6 . The aircraft wing as claimed in claim 1 , wherein the interface between the master flight control surface and slave flight control surface is a passive interface.

7 . The aircraft wing as claimed in claim 1 , wherein the interface is formed by a series of grooves, protrusions, or formations on the master flight control surface and slave flight control surface inter-engaging when the wing tip device is in the flight configuration.

8 . The aircraft wing as claimed in claim 7 , wherein movement of the wing tip device from the flight configuration to the ground configuration results in the series of grooves, protrusions, or formations disengaging.

9 . The aircraft wing as claimed in claim 1 , wherein the fixed wing may comprise one or more actuators associated with the master flight control surface.

10 . The aircraft wing as claimed in claim 1 , wherein the wing tip device and the fixed wing are separable along an oblique cut plane passing through the upper and lower surfaces of the wing, the oblique cut plane being orientated normal to an axis of rotation of the wing tip device.

11 . An aircraft wing as claimed in claim 10 , wherein the interface between the master flight control surface and the slave flight control surface is located in the oblique cut plane.

12 . An aircraft, the aircraft comprising a wing as claimed in claim 1 .

13 . A method of decoupling an interface between a master flight control surface and slave flight control surface of a wing according to claim 1 , the method comprising the step of moving the wing tip device from the flight configuration to the ground configuration.

14 . A method of coupling an interface between a master flight control surface and a slave flight control surface of a wing according to claim 1 , the method comprising the step of moving the wing tip device from the ground configuration to the flight configuration.

15 . An aircraft wing comprising:
a fixed wing; a wing tip device coupled to a tip of the fixed wing by an interface; a slew ring interface coupling the wing tip device to the fixed wing, wherein a pivot axis of the slew ring interface is oblique to a plane defined by a chord and span of the fixed wing and the wing tip device rotates about the pivot axis; a master flight control surface connected to the fixed wing, and configured to move with respect to the fixed wing along a first direction; a slave flight control surface connected to the wing tip device and configured to move with respect to the wing tip device along the first direction; and a male and female assembly interface between a first end of the master flight control surface and a second end of the slave flight control surface, wherein the interface includes a male member attached to one of the first or second ends and a female member attached to the other of the first or second ends, wherein the male member has a curved shape and the curved shape has radial center at the pivot axis; wherein the male member is configured to slide into and out of the female member as the wing tip device turns about the pivot axis, and wherein the slave flight control surface is locked to the master flight control surface at the interface while the male member is in the female member.

16 . The aircraft wing of claim 15 further comprising an actuator attached to the fixed wing and connected to the master flight control surface, wherein the actuator is configured to move the master flight control surface in the first direction and the slave flight control surface moves with the master flight control surface due to the locked relationship between the master flight control surface and the slave flight control surface.

17 . The aircraft wing of claim 15 wherein the male member is a plurality of curved bars arranged in a plane perpendicular to the pivot axis and each of the curved bars has a curvature centered on the pivot axis.

18 . The aircraft wing of claim 17 wherein the curved bars are mounted above an end surface of the tip of the fixed wing, wherein the end surface is in a plane perpendicular to the pivot axis and the plane of the curved bars is offset from the plane of the end surface.

19 . The aircraft wing of claim 15 wherein the master flight control surface and the slave flight control surface form an aileron at trailing edges of the fixed wing and the wing tip device.

20 . The aircraft wing of claim 15 wherein the master flight control surface and the slave flight control surface are mounted, respectively, to leading edges of the fixed wing and the wing tip device.

21 . The aircraft wing of claim 15 wherein the first direction is parallel to a chord of the fixed wing.

Assignees

• Airbus Operations Ltd

Inventors

• KELLY Mark Shaun
• Alexander Stuart

Classifications

• B64C2009/005

  Ailerons · CPC title

• B64C9/10

  one surface adjusted by movement of another, e.g. servo tabs (B64C9/04 takes precedence; adjusting surfaces of different type or function B64C9/12) · CPC title

• B64C9/22

  at the front of the wing · CPC title

• B64C3/00 Primary

  Wings (ornithopter wings B64C33/02) · CPC title

• B64C3/546

  by foldable elements · CPC title