Wing arrangement for an aircraft

Patent metadata

Field	Value
Publication number	US-10994827-B2
Application number	US-201815979806-A
Country	US
Kind code	B2
Filing date	May 15, 2018
Priority date	May 18, 2017
Publication date	May 4, 2021
Grant date	May 4, 2021

Abstract

A wing arrangement for an aircraft, comprising a wing having a base section and a tip section pivotably connected to base section such that the tip section is pivotable about a pivot axis between a deployed position and a stowed position. The wing arrangement also comprises a latching arrangement which includes an engagement portion, a latching actuator selectively movable between a first actuator position and a second actuator position, an elastically deformable structure, and a latching element. When the tip section is pivoted from the stowed or deployed position into an engagement position, the elastically deformable structure is initially deformed, and as the tip section pivots further into the deployed or stowed position, the elastic deformation of the elastically deformable structure decreases.

First claim

The invention claimed is:

1. A wing arrangement for an aircraft, comprising:
a wing having
a base section with a first end portion and an opposite second end portion, wherein the first end portion is adapted to be secured to a fuselage of an aircraft, and
a tip section with a third end portion and an opposite fourth end portion, wherein the third end portion is pivotably connected to the second end portion such that the tip section is pivotable about a tip section pivot axis between a first tip section position, which is defined by a first tip section stop mechanism, and a second tip section position, wherein the first tip section position is a deployed position or a stowed position, in which a spanwise length of the wing is smaller than in the deployed position, and the second tip section position is the other one of the deployed position and the stowed position,

a latching arrangement comprising
at least one engagement portion on one of the tip section and the base section,
at least one latching actuator selectively movable between a first actuator position and a second actuator position,
an elastically deformable structure, and
at least one latching element, which has a hook-shaped portion, is secured to the other one of the tip section and the base section to be pivotable with respect thereto about a latching element pivot axis, and is selectively movable between different positions by moving the at least one latching actuator between the first actuator position and the second actuator position, wherein during movement of the at least one latching actuator from the first actuator position into the second actuator position the latching element pivot axis of the at least one latching element moves along a path, so that the at least one latching element carries out a translatory movement defined by the path,
wherein when the at least one latching actuator is in the first actuator position the at least one latching element is in a release position and is positioned such that the tip section is pivotable between the second tip section position and an engagement position, which is located between the second tip section position and the first tip section position or which is equal to the first tip section position,
wherein when the at least one latching actuator is in the second actuator position the at least one latching element is in a latching position in which an engagement surface of each of the at least one latching element engages one of the at least one engagement portion such that the engagement surface applies a force to the respective engagement portion, which biases the tip section against the first tip section stop mechanism, and such that the tip section is prevented from moving towards the second tip section position,
wherein when the tip section is pivoted from the second tip section position into the engagement position with the at least one latching actuator in the first actuator position and the at least one latching actuator is subsequently moved from the first actuator position into the second actuator position the engagement surface of the at least one latching element engages the at least one engagement portion when the at least one latching actuator reaches a third actuator position between the first and second actuator positions, upon further movement of the at least one latching actuator the engagement surface of the at least one latching element applies a force to the respective engagement portion which forces the tip section towards and against the first tip section stop mechanism, wherein over at least part of the movement of the at least one latching actuator from the third actuator position into a fourth actuator position the tip section abuts the first tip section stop mechanism and the force with which the engagement surface biases the tip section against the first tip section stop mechanism increases while the elastically deformable structure is increasingly deformed, and
wherein
the fourth actuator position is equal to the second actuator position, or
the fourth actuator position is between the third and second actuator positions and upon further movement of the at least one latching actuator from the fourth actuator position into the second actuator position the force with which the engagement surface biases the tip section against the first tip section stop mechanism decreases while the elastic deformation of the elastically deformable structure decreases.

2. The wing arrangement according to claim 1 , wherein the latching arrangement comprises a rotatable latching shaft to which the at least one latching element and the at least one latching actuator are coupled, such that when moving the at least one latching actuator between the first and second actuator positions the shaft is rotated, thereby effecting the movement of the at least one latching element between the different positions.

3. The wing arrangement according to claim 1 , wherein at least one of
the elastically deformable structure comprises a separate element provided between the at least one latching element and each of the at least one latching actuator, or
the elastically deformable structure comprises a portion of the tip section or the base section.

4. The wing arrangement according to claim 1 , wherein the path is arranged such that
during movement of the at least one latching actuator from the third actuator position into the fourth actuator position the engagement surface of the at least one latching element moves in a direction of the force applied by the engagement surface to the respective engagement portion and forcing the tip section towards and against the first tip section stop mechanism, and,
if the fourth actuator position is between the third and second actuator positions, during movement of the at least one latching actuator from the fourth actuator position into the second actuator position the engagement surface of the at least one latching element moves in a direction opposite that force.

5. The wing arrangement according to claim 4 , wherein the latching arrangement comprises a rotatable latching shaft to which the at least one latching element and the at least one latching actuator are coupled, such that when moving the at least one latching actuator between the first and second actuator positions the shaft is rotated, thereby effecting the movement of the at least one latching element between the different positions, wherein the at least one latching element is pivotably secured to the latching shaft such that the latching element is pivotable relative to the latching shaft and the latching element pivot axis is parallel to but offset from an axis of rotation of the latching shaft, so that rotation of the latching shaft effects the movement of the latching element pivot axis along the path.

6. The wing arrangement according to claim 1 , wherein the latching arrangement comprises a latching element stop arrangement defining the latching position of the at least one latching element, wherein upon moving the at least one latching actuator from the first actuator position to the second actuator position the at least one latching element abuts the latching element stop arrangement when the at least one latching actuator is between the third and fourth actuator positions or in the fourth actuator position.

7. The wing arrangement according to claim 1 , wherein the engagement portion moves along the engagement surface during at least part of the movement of the at least one latching actuator from the third actuator position into the second actuator position, wherein the engagement surface of the at least one latching element comprises a rising ramp portion which is shaped and arranged such that during at least part of the movement along the engagement surf

Assignees

• Airbus Operations Gmbh
• Airbus Operations Ltd

Inventors

• Winkelmann Christoph
• Ellmers Wilfried
• Briancourt Stephen
• Brakes David

Classifications

• F16B45/034

  the closing member constituting the hook shaped portion of the hook · CPC title

• B64C3/56 Primary

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

• B64C3/546 Primary

  by foldable elements · CPC title

• Y02T50/10

  Drag reduction · CPC title

• F16B45/02

  Hooks with pivoting {or elastically bending} closing member · CPC title