Arrangement for avoiding clashing on a folding wing tip

Patent metadata

Field	Value
Publication number	US-11772776-B2
Application number	US-202017297827-A
Country	US
Kind code	B2
Filing date	May 14, 2020
Priority date	May 16, 2019
Publication date	Oct 3, 2023
Grant date	Oct 3, 2023

Abstract

An aircraft wing including a fixed wing and a wing tip device rotatable about a hinge at the tip of the fixed wing is disclosed. The wing further includes a hinged panel at the boundary between the wing tip device and the fixed wing. In the flight configuration the panel is closed such that the panel is substantially flush with the upper surface of the wing, and the hinged panel is located in the path of a moveable element (for example part of an actuation mechanism, such as a curved rack). In the ground configuration the panel is hinged open to a position outside the path of the moveable element such that clashing of the moveable element with the stationary structure at the tip of the fixed wing is avoided.

First claim

The invention claimed is:

1. An aircraft wing, the aircraft wing comprising a fixed wing and a wing tip device rotatable about a hinge at the tip of the fixed wing,
wherein the wing tip device comprises a moveable element that moves along a path, relative to a stationary structure at the tip of the fixed wing, when the wing tip device is rotated about a hinge axis of the hinge, between:
(i) a flight configuration for use during flight and (ii) 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 further comprises a hinged panel at the boundary between the wing tip device and the fixed wing, and the wing is arranged such that:
in the flight configuration the hinged panel is closed such that the hinged panel is flush with the upper surface of the wing, and the hinged panel is located in the path of the moveable element,
and in the ground configuration the hinged panel is hinged open to a position outside the path of the moveable element such that clashing of the moveable element with the stationary structure at the tip of the fixed wing is avoided,
wherein the hinged panel is hinged open as a result of the moveable element exerting an opening force against the hinged panel as the wing tip device moves to the ground configuration, and
wherein the wing further comprises an actuation mechanism for moving the wing tip device from the flight configuration to the ground configuration, and the actuation mechanism comprises the moveable element.

2. A wing according to claim 1 , wherein the actuation mechanism comprises a rotary drive, the rotary drive being arranged to drive the moveable element in a curved path to move the wing tip device between the flight configuration and the ground configuration.

3. A wing according to claim 2 , wherein the rotary drive comprises a pinion, and the moveable element comprises a curved rack for being driven along a curved path by rotation of the pinion.

4. A wing according to claim 1 , wherein the hinged panel is rotatable about a panel-hinge axis that is parallel to the hinge axis of the wing tip device.

5. A wing according to claim 1 , wherein the wing tip device comprises an upper cover and in the flight configuration the upper cover of the wing tip device adjoins the hinged panel along an interface, the interface being arranged such that an edge of the upper cover overlaps the adjoining edge of the hinged panel along an overlap region.

6. A wing according to claim 5 , wherein the interface is outboard of the hinge axis of the wing tip device, such that as the wing tip device rotates from the flight configuration to the ground configuration, the upper cover is lifted away from the hinged panel along the overlap region.

7. A wing according to claim 6 , wherein the wing is configured such that during return movement from the ground configuration to the flight configuration, the upper cover and the hinged panel contact each other along the overlap region, such that the upper cover draws the hinged panel back down into the closed position.

8. A wing according to claim 5 , wherein in the ground configuration, the wing tip device is rotated about the hinge such that the edge of the upper cover is inboard of the hinged panel.

9. A wing according to claim 8 , wherein in the ground configuration, the wing tip device is rotated about the hinge such that the edge of the upper cover is inboard of the hinge axis, thereby at least partially enveloping the hinged panel.

10. A wing according to claim 1 , wherein the tip of the fixed wing comprises a wing box having a pair of ribs, a pair of spars and an upper and lower cover, and wherein the root of the wing tip device comprises wing tip box, comprising a pair of wing tip spars, a pair of wing tip ribs and a wing tip upper cover and a wing tip lower cover, and wherein when the wing tip is in the flight configuration, the upper and lower covers of the wing tip box are continuations of the upper and lower covers of the wing box, and the hinged panel is hinged on the upper cover of the wing box such that the hinged panel is flush with the adjoining upper covers.

11. A wing according to claim 10 , wherein the rotary drive is housed in the wing box of the fixed wing.

12. A method of moving a wing tip device from a flight configuration for use during flight, to 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,
the method comprising the steps of
opening a hinged panel from a closed position in which the hinged panel is located in the path of a moveable element of the wing tip device, and is flush with the upper surface of the wing, to an open position in which the hinged panel is located outside the path of the moveable element
wherein the hinged panel is hinged open as a result of the moveable element exerting an opening force against the hinged panel as the wing tip device moves to the ground configuration, and
wherein the wing further comprises an actuation mechanism for moving the wing tip device from the flight configuration to the ground configuration, and the actuation mechanism comprises the moveable element.

13. A method of moving a wing tip device from a ground configuration for use during ground-based operations, to a flight configuration for use during flight in which flight configuration the wing tip device is moved away from the ground configuration such that the span of the aircraft wing is increased,
the method comprising the steps of
closing a hinged panel from an open position, to a closed position in which the hinged panel is flush with the upper surface of the wing,
the closing of the hinged panel being effected by the wing tip device and the hinged panel contacting each other along an overlap region, such that the wing tip device draws the hinged panel back down into the closed position during movement from the ground configuration to the flight configuration.

14. A folding wing tip arrangement for an aircraft wing, the arrangement comprising a fixed wing and a rotatable wing tip device at the tip thereof, the wing tip device being configurable by a wing tip actuator between:
(i) a flight configuration for use during flight and (ii) 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 arrangement comprises a moveable panel at the interface between the wing tip device and the fixed wing,
and wherein the moveable panel is moveable to an open position to accommodate movement of the wing tip actuator as the wing tip actuator moves the wing tip device to the ground configuration,
wherein the moveable panel is located in the path of a moveable element of the wing tip device,
wherein the movable panel is hinged open as a result of the moveable element exerting an opening force against the movable panel as the wing tip device moves to the ground configuration, and
wherein the wing further comprises an actuation mechanism for moving the wing tip device from the flight configuration to the ground configuration, and the actuation mechanism comprises the movable element.

15. An arrangement according to claim 14 , wherein in the flight configuration the moveable panel is closed and occupies a space that would be occupied by the actuator when the wing tip

Assignees

• Airbus Operations Ltd

Inventors

• Horwood Jack
• Morrell Paul
• Harding Matt

Classifications

• B64C3/56 Primary

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

• B64C3/185

  Spars · CPC title

• B64C3/187

  Ribs · CPC title

• B64C3/54

  Varying in area · CPC title

• Y02T50/10

  Drag reduction · CPC title