Aircraft wing with wing tip device

Patent metadata

Field	Value
Publication number	US-11613342-B2
Application number	US-202016832639-A
Country	US
Kind code	B2
Filing date	Mar 27, 2020
Priority date	Mar 29, 2019
Publication date	Mar 28, 2023
Grant date	Mar 28, 2023

Abstract

An aircraft wing having a fixed wing and a wing tip device at the tip of the fixed wing is disclosed. The wing tip device being movable relative to the fixed wing between flight and ground configurations, the aircraft wing having a locking mechanism including a locking bore and a locking pin, the locking mechanism being configurable between a locked configuration, in which the locking pin is received in the locking bore, to lock the wing tip device in one of the flight or ground configurations, and an unlocked configuration in which the locking pin is withdrawn from the locking bore such that the wing tip device is moveable relative to the fixed wing, and wherein the locking pin is configured such that it has a replaceable tip.

First claim

The invention claimed is:

1. An aircraft wing comprising a fixed wing and a wing tip device at the tip of the fixed wing, the wing tip device being movable relative to the fixed wing between:
a flight configuration for use during flight, and
a ground configuration for use during ground-based operations, in which ground configuration the wing tip device is moved relative to the fixed wing such that the span of the wing is reduced,
the aircraft wing having a locking mechanism comprising a locking bore and a locking pin, the locking mechanism being configurable between a locked configuration, in which the locking pin is received in the locking bore, to lock the wing tip device in one of the flight or ground configurations, and an unlocked configuration in which the locking pin is withdrawn from the locking bore such that the wing tip device is moveable relative to the fixed wing,
wherein the locking pin is configured such that it has a replaceable tip, and
wherein the locking pin is floating mounted such that as the locking mechanism is moved to the locked configuration, the locking pin can change its orientation in any direction with respect to the locking bore.

2. An aircraft wing according to claim 1 wherein the locking pin comprises a body and the locking pin is configured such that the tip is detachable from the body and the body is attachable to a replacement tip.

3. An aircraft wing according to claim 2 wherein the body comprises a connector and the locking pin comprises a cooperating connector, wherein the connector and cooperating connector are disengageable and engageable with each other such that the tip is detachable from the body and a replacement tip is attachable to the body by engaging the connector and a corresponding cooperating connector associated with the replacement tip, with each other.

4. An aircraft wing according to claim 1 wherein the locking pin comprises a body and the locking pin is configured such that the tip is releasably attachable to the body.

5. An aircraft wing according to claim 1 wherein the replaceable tip is of a material that is softer than a surface that the tip comes into contact with as the locking pin is received in the locking bore.

6. An aircraft wing according to claim 5 wherein a bush is provided in the locking bore and the replaceable tip is of a material that is softer than the bush.

7. An aircraft wing according to claim 1 wherein the locking pin comprises a body and the tip, the tip being selectively attachable to the body, and wherein the tip is of a material that is softer than that of the body.

8. An aircraft wing according to claim 1 wherein the locking pin and/or locking bore is movably mounted such that as the locking mechanism is moved to the locked configuration, the locking pin or locking bore can align itself with the locking bore or locking pin respectively.

9. An aircraft wing according to claim 1 wherein at least one of the locking pin has a surface, or the locking bore is defined by a surface, that is configured to urge the locking pin and locking bore into alignment, as the locking mechanism is moved to the locked configuration.

10. An aircraft comprising an aircraft wing according to claim 1 .

11. An aircraft wing according to claim 1 in combination with a replacement tip for the locking pin.

12. An aircraft wing comprising a fixed wing and a wing tip device at the tip of the fixed wing, the wing tip device being movable relative to the fixed wing between:
a flight configuration for use during flight, and
a ground configuration for use during ground-based operations, in which ground configuration the wing tip device is moved relative to the fixed wing such that the span of the wing is reduced,
the aircraft wing having a locking mechanism comprising a locking bore and a locking pin, the locking mechanism being configurable between a locked configuration, in which the locking pin is received in the locking bore, to lock the wing tip device in one of the flight or ground configurations, and an unlocked configuration in which the locking pin is withdrawn from the locking bore such that the wing tip device is moveable relative to the fixed wing,
wherein the locking pin comprises a body and a tip that is selectively attachable to the body, and
wherein the locking pin is floating mounted such that as the locking mechanism is moved to the locked configuration, the locking pin can change its orientation in any direction with respect to the locking bore.

13. A kit of parts comprising a fixed wing and a wing tip device configured to be mounted at the tip of the fixed wing and to be movable relative to the fixed wing between:
a flight configuration for use during flight, and
a ground configuration for use during ground-based operations, in which ground configuration the wing tip device is moved relative to the fixed wing such that the span of the wing is reduced,
the kit of parts comprising a locking bore and a locking pin configured to, in use, form a locking mechanism configurable between a locked configuration, in which the locking pin is received in the locking bore, to lock the wing tip device in one of the flight or ground configurations, and an unlocked configuration in which the locking pin is withdrawn from the locking bore such that the wing tip device is moveable relative to the fixed wing,
wherein the locking pin is configured such that it has a replaceable tip,
wherein the locking pin is floating mounted such that as the locking mechanism is moved to the locked configuration, the locking pin can change its orientation in any direction with respect to the locking bore.

14. A kit of parts according to claim 13 wherein the locking pin comprises a body and the locking pin is configured such that the tip is detachable from the body and the body is attachable to a replacement tip.

15. A kit of parts according to claim 14 wherein the tip is detached from the body.

16. A kit of parts according to claim 13 wherein the kit of parts further comprises a replacement tip for the locking pin.

17. A method of locking a wing tip device of an aircraft wing in a flight or ground configuration, the aircraft wing comprising a fixed wing and a wing tip device at the tip of the fixed wing, the wing tip device being moveable relative to the fixed wing between:
a flight configuration for use during flight, and
a ground configuration for use during ground-based operations, in which ground configuration the wing tip device is moved relative to the fixed wing such that the span of the wing is reduced,
the aircraft wing having a locking mechanism comprising a locking bore and a locking pin, the locking mechanism being configurable between a locked configuration, in which the locking pin is received in the locking bore, to lock the wing tip device in one of the flight or ground configurations, and an unlocked configuration in which the locking pin is withdrawn from the locking bore such that the wing tip device is moveable relative to the fixed wing,
wherein the locking pin is configured such that it has a replaceable tip,
wherein the locking pin is floating mounted such that as the locking mechanism is moved to the locked configuration, the locking pin can change its orientation in any direction with respect to the locking bore,
and the method comprises moving the locking mechanism from its unlocked configuration to its locked configuration.

18. A method of unlocking a wing tip device of an aircraft wing from a flight or ground configuration, the aircraft wing comprising a fixed wing and a win

Assignees

• Airbus Operations Ltd

Inventors

• Morrell Paul
• Harding Matt

Classifications

• B64U30/14

  detachable · CPC title

• B64C3/56 Primary

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

• B64C3/38

  Adjustment of complete wings or parts thereof · CPC title

• Y02T50/10

  Drag reduction · CPC title

• B64C3/546

  by foldable elements · CPC title