Curved interface between an outer end of a wing and a moveable wing tip device

Patent metadata

Field	Value
Publication number	US-11142298-B2
Application number	US-201816200019-A
Country	US
Kind code	B2
Filing date	Nov 26, 2018
Priority date	Nov 27, 2017
Publication date	Oct 12, 2021
Grant date	Oct 12, 2021

Abstract

An aircraft ( 1002 ) including a wing ( 1001 ), having a fixed wing ( 1005 ) with a wing tip device ( 1003 ) moveably mounted at the outer end thereof. The wing tip device ( 1003 ) is moveable between: a flight configuration; and a ground configuration about an axis of rotation. The wing tip device ( 1003 ) and the fixed wing ( 1005 ) meet along an interfacing cut line ( 1035 ). The interfacing cut line ( 1035 ) includes a curved section ( 1039 ) cent red on the axis of rotation ( 1011 ), the radius of the curved section constantly increasing as the cut line passes around the axis (for example a spiral shape).

First claim

The invention claimed is:

1. An aircraft comprising a wing, the wing having a fixed wing with a wing tip device moveably mounted at the outer end thereof, the wing tip device being moveable between:
(a) a flight configuration for use during flight; and
(b) a ground configuration for use during ground-based operations, in which ground configuration the wing tip device is moved away from the flight configuration such that the span of the aircraft wing is reduced,
wherein the wing tip device is rotatable between the flight and ground configurations, about an axis of rotation inclined with respect to a plane defined by spanwise and chordwise directions of the fixed wing, such that the wing tip device rotates upwards and rearwards when moving from the flight to ground configurations, and
wherein, when the wing tip device is in the flight configuration, an outer end of the fixed wing and an inner end of the wing tip device meet along an interfacing cut line that separates an outer surface of the fixed wing and an outer surface the wing tip device,
the interfacing cut line comprising a curved section, wherein a radius of the curved section is a distance between the axis of rotation and the curved section, and the radius of the curved section continuously increases along the curved section in a direction towards a leading edge of the wing tip device such that adjacent portions of the fixed wing and wing tip device on either side of the interfacing cut line, separate as the wing tip device moves from the flight configuration towards the ground configuration.

2. The aircraft wing according to claim 1 , wherein the wing comprises an upper surface extending from the leading edge, over the wing, to a trailing edge, and the wing comprises a lower surface extending from the leading edge, under the wing, to the trailing edge, and wherein the curved section is on the upper surface of the wing.

3. The aircraft wing according to claim 1 , wherein the interfacing cut line further comprises a first length extending from the curved section to a trailing edge of the fixed wing, and a second length extending from the curved section to the leading edge of the fixed wing.

4. The aircraft wing according to claim 3 , wherein the second length is formed by a cut through the outer surface that extends within a plane containing or parallel to the axis of rotation.

5. The aircraft wing according to claim 1 , wherein the aircraft wing is a first aircraft wing attached to a fuselage of an aircraft and the aircraft includes a second aircraft wing conforming to claim 1 on an opposite side of the fuselage to the first aircraft wing.

6. The aircraft according to claim 1 , wherein the interfacing cut line further comprises:
a leading edge section passing over the upper surface, through the leading edge and onto the lower surface, the leading edge section of the cut line being formed by a cut that extends within a plane containing the axis of rotation,
an upper surface section located on the upper surface and to the rear of the axis of rotation and being offset inboard from the plane containing the axis of rotation; and
the interfacing cut line comprising a lower surface section located on the lower surface to the rear of the axis of rotation and being offset outboard from the plane containing the axis of rotation.

7. The aircraft according to claim 6 , wherein the leading edge section and the upper surface section are linked by the curved section, and the other end of the leading edge section and the lower surface section are linked by a further curved section, the further curved section also being substantially spiral-shaped centered on the axis of rotation, the radius continuously increasing as the cut line passes around the axis such that adjacent portions of the fixed wing and wing tip device either side of the interfacing cut line, separate as the wing tip device moves from the flight configuration towards the ground configuration.

Assignees

• Airbus Operations Ltd

Inventors

• Bishop Benjamin

Classifications

• B64C3/56 Primary

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

• B64C23/065

  at the wing tips · CPC title

• B64C3/40

  Varying angle of sweep · CPC title

• Y02T50/10

  Drag reduction · CPC title

• B64C3/38

  Adjustment of complete wings or parts thereof · CPC title