Wing for an aircraft

Patent metadata

Field	Value
Publication number	US-11897613-B2
Application number	US-202217834341-A
Country	US
Kind code	B2
Filing date	Jun 7, 2022
Priority date	Jun 8, 2021
Publication date	Feb 13, 2024
Grant date	Feb 13, 2024

Abstract

A wing for an aircraft, comprising a main wing and a slat assembly with a slat and a connection assembly with a slat track. The front end of the slat track is mounted to the slat, and the rear end and/or the intermediate portion of the slat track are mounted to the main wing by a roller or slide bearing. The slat track is movable along the track longitudinal axis. The connection assembly includes a drive unit. The drive unit includes a rotary actuator mounted to the main wing and having at least one drive arm rotatably driven about a rotation axis and drivingly engaging the slat track, and one of the drive arm and the slat track has at least one groove and the other one of the drive arm and the slat track comprises at least one spigot drivingly engaging the groove.

First claim

The invention claimed is:

1. A wing for an aircraft, comprising:
a main wing, and
a slat assembly comprising:
a slat, and
at least one connection assembly movably connecting the slat to the main wing, such that the slat is movable between a retracted position and at least one extended position,

wherein the at least one connection assembly comprises an elongate slat track that extends along a track longitudinal axis between a front end and a rear end and has an intermediate portion between the front and rear ends,
wherein the front end of the slat track is mounted to the slat,
wherein the rear end of the slat track, or the intermediate portion of the slat track, or both are mounted to the main wing by a roller or slide bearing such that the slat track is movable along the track longitudinal axis,
wherein the connection assembly comprises a drive unit configured for driving the slat track for movement along the track longitudinal axis,
wherein the drive unit comprises a rotary actuator mounted to the main wing and having at least one drive arm rotatably driven about a rotation axis and drivingly engaging the slat track, and,
wherein one of the at least one drive arm and the slat track comprises at least one groove and the other one of the drive aim and the slat track comprises at least one spigot drivingly engaging the at least one groove,
wherein rotation of the at least one drive arm imparts movement to each of the at least one spigot and the at least one groove.

2. The wing according to claim 1 , wherein the at least one spigot or the at least one groove is provided at a lateral side of the slat track at the intermediate portion of slat track.

3. The wing according to claim 1 , wherein the at least one spigot engages the at least one groove with a predefined play.

4. The wing according to claim 3 , wherein the at least one groove is formed as a slot extending in a radial direction with respect to the rotation axis.

5. The wing according to claim 1 , wherein the at least one groove is open at an outer end of the at least one drive arm.

6. The wing according to claim 1 , wherein the one of the at least one drive arm and the slat track comprising the at least one groove comprises two grooves, and wherein the other one of the at least one drive arm and the slat track comprising the at least one spigot comprises two spigots drivingly engaging the two grooves.

7. The wing according to claim 1 , wherein the at least one drive arm is a first drive arm and wherein the rotary actuator comprises a second drive aim rotatably driven about the rotation axis and drivingly engaging the slat track.

8. The wing according to claim 7 , wherein one of the first drive arm and the slat track comprises a first groove, and the other one of the first drive arm and the slat track comprises a first spigot drivingly engaging the first groove, or
wherein one of the second drive arm and the slat track comprises a second groove and the other one of the second drive aim and the slat track comprises a second spigot drivingly engaging the second groove, or
wherein one of the first drive arm and the slat track comprises a first groove, and the other one of the first drive aim and the slat track comprises a first spigot drivingly engaging the first groove and one of the second drive aim and the slat track comprises a second groove and the other one of the second drive arm and the slat track comprises a second spigot drivingly engaging the second groove.

9. The wing according to claim 8 , wherein the first spigot and the second spigot are formed integrally, or extend coaxially, or are formed integrally and extend coaxially.

10. The wing according to claim 8 , wherein the first spigot is spaced apart from the second spigot.

11. The wing according to claim 1 , wherein the roller or slide bearing comprises a guide rail mounted to the main wing and a first roller unit mounted to the rear end of the slat track and engaging the guide rail, and
wherein the roller or slide bearing comprises a second roller unit that is mounted to the main wing and that engages an engagement surface provided at the intermediate portion of the slat track.

12. The wing according to claim 11 , wherein the slat track has a profile comprising an upper flange portion, a lower flange portion and at least one web portion connecting upper and lower flange portions, and
the second roller unit is arranged in a recess between the upper and lower flange portions and engages the engagement surface provided at the upper flange portion, or at the lower flange portion, or at both the upper and lower flange portions.

13. The wing according to claim 12 , wherein the slat track has such a profile that a first recess is formed between the upper and lower flange portions at a first side of the web portion, and a second recess is formed between the upper and lower flange portions at a second side of the web portion opposite the first side.

14. The wing according to claim 13 , wherein the second roller unit comprises a first roller element and a second roller element,
wherein the first roller element is arranged in the first recess and the second roller element is arranged in the second recess, and
wherein first and second roller elements are arranged coaxially and have the same radius.

15. The wing according to claim 12 , wherein the at least one groove or the at least one spigot is arranged in the web portion.

16. The wing according to claim 1 , wherein the slat track comprises a first track part and a second track part that are formed separate from one another,
wherein each of the first and second track parts is formed integrally and extends along the track longitudinal axis from the rear end to the front end, and
wherein the first and second track parts are mounted to one another and rest against one another along a contact plane spanned by the track longitudinal axis and a wing thickness direction.

17. The wing according to claim 16 , wherein the cross-section of the slat track is formed such that a predefined gap is formed between a portion of the first track part and a portion of the second track part in extension of the contact plane,
wherein the at least one spigot or the at least one groove is arranged in the web portion of the first and second track parts on opposite sides of the gap, and
wherein the at least one drive arm extends inside the gap to engage with the slat track.

18. The wing according to claim 1 , wherein the connection assembly is a first connection assembly,
wherein the wing comprises a second connection assembly connecting the slat to the main wing in a position spaced apart from the first connection assembly in a wing span direction, and
wherein the second connection assembly is formed the same as the first connection assembly.

19. A wing for an aircraft, comprising:
a main wing, and
a slat assembly comprising:
a slat, and
at least one connection assembly movably connecting the slat to the main wing, such that the slat is movable between a retracted position and at least one extended position,

wherein the at least one connection assembly comprises an elongate slat track that extends along a track longitudinal axis between a front end and a rear end and has an intermediate portion between the front and rear ends,
wherein the front end of the slat track is mounted to the slat,
wherein the rear end of the slat track, or the intermediate portion of the slat track, or both are mounted to the main wing by a roller or slide bearing such that the slat track is m

Assignees

• Airbus Operations Gmbh

Inventors

• Schlipf Bernhard
• Lorenz Florian

Classifications

• B64C9/24 Primary

  by single flap · CPC title

• B64C9/02

  Mounting or supporting thereof · CPC title

• B64C13/28

  mechanical · CPC title

• B64C9/22 Primary

  at the front of the wing · CPC title

• B64C3/28

  Leading or trailing edges attached to primary structures, e.g. forming fixed slots · CPC title