Support stay and support arrangement for supporting a movable part of an aircraft

Patent metadata

Field	Value
Publication number	US-11780558-B2
Application number	US-202117185423-A
Country	US
Kind code	B2
Filing date	Feb 25, 2021
Priority date	Feb 28, 2020
Publication date	Oct 10, 2023
Grant date	Oct 10, 2023

Abstract

A support stay is provided to improve failsafe configurations for movable parts of an aircraft. The support stay supports the movable part with a primary body and a separate secondary body. The primary body and the secondary body provide separate load paths. The secondary body is attached to the primary body by a mechanical connection, e.g., rivets. If one of the bodies becomes structurally compromised, for example by a crack, this configuration does not transfer shear load between the primary and secondary body, so that the other body does not become structurally compromised.

First claim

The invention claimed is:

1. A support stay configured to support a movable part of an aircraft, the support stay comprising:
a primary body providing a primary load path,
a first secondary body providing a first secondary load path, and,
a second secondary body providing a second secondary load path,
wherein the primary body and the first and second secondary bodies are each formed as single unitary members,
wherein the first and second secondary bodies are attached to the primary body by a mechanical connection,
wherein the mechanical connection is configured such that forces causing a structural compromization of the primary body are prevented from being transferred to the first or second secondary bodies in a manner that prevents the first or second secondary bodies from becoming structurally compromised, and vice-versa,
wherein the mechanical connection comprises
a plurality of first mechanical fasteners, with each first mechanical fastener passing through both the primary body and the first secondary body and not the second secondary body, and,
a plurality of second mechanical fasteners, with each second mechanical fastener passing through both the primary body and the second secondary body and not the first secondary body.

2. The support stay according to claim 1 , wherein the primary body and the first and second secondary bodies include facing contact surfaces that are slidable, relative to each other, when at least one of the primary body, the first second body, or the second secondary body is deformed due to a force transferred by at least one of the primary load path or the secondary load path.

3. The support stay according to claim 1 , wherein the mechanical connection is configured to prevent disengagement of the primary body from the secondary body.

4. The support stay according to claim 1 , wherein the mechanical connection is configured to press the primary body against the secondary body.

5. The support stay according to claim 1 , wherein the first and second mechanical fasteners are configured to prevent disengagement of the primary body from the respective first and second secondary bodies along a longitudinal direction of the respective mechanical fastener.

6. The support stay according to claim 1 , wherein the first and second mechanical fasteners are configured to press the primary body against the respective first and second secondary bodies along a longitudinal direction of the respective mechanical fastener.

7. The support stay according to claim 1 ,
further comprising a first mounting portion, configured to be mounted to the movable part, and a second mounting portion configured to be mounted to a structural part of the aircraft,
wherein the first mounting portion and the second mounting portion are spaced apart by means of the primary load path and the secondary load path, so as to transfer forces between the first and second mounting portions.

8. The support stay according to claim 1 , wherein the movable part is chosen from a group consisting of high-lift devices, control surfaces, and combinations of high-lift devices and control surfaces.

9. The support stay according to claim 8 , wherein the high-lift devices comprise flaps and slats.

10. The support stay according to claim 8 , wherein the control surfaces comprise elevators, rudders, ailerons, and combinations thereof.

11. The support stay according to claim 8 , wherein the combinations of high lift devices and control surfaces comprise elevons and flaperons.

12. The support stay according to claim 1 , wherein the primary body and the first and second secondary bodies are made of light metals or light metal alloys.

13. The support stay according to claim 12 , wherein the light metals comprise aluminum or titanium and the light metal alloys comprise aluminum alloys and titanium alloys.

14. The support stay according to claim 1 , wherein the primary body and the first and second secondary bodies are made of different materials.

15. The support stay according to claim 1 ,
wherein the primary body includes a plurality of side portions that are integrally formed with at least one intermediate portion that sets a distance between the side portions, and
wherein the first and second secondary bodies are attached to the side portions.

16. The support stay according to claim 1 , wherein the first and second secondary bodies are each configured to clad the primary body along any side portion of the primary body.

17. A support arrangement configured to support at least one of a movable high-lift device or a movable control surface, the support arrangement comprising:
a primary support,
a secondary support,
a spherical bearing connecting the primary support, the secondary support, or both to the movable high-lift device or the movable control surface, and
a support stay according to claim 1 ,
wherein the support stay is arranged such that at least one of a pivotal or spanwise movement of the primary support is prevented.

18. At least one of a high-lift device or a control surface for an aircraft comprising a movable airfoil supported by a support stay according to claim 1 .

19. An aircraft including a support stay according to claim 1 .

20. A support stay configured to support a movable part of an aircraft, the support stay comprising:
a primary body providing a primary load path, and
a secondary body providing secondary load path,
wherein the primary body and the secondary body are each formed as single unitary members,
wherein the secondary body is attached to the primary body by a mechanical connection,
wherein the mechanical connection is configured such that forces causing a structural compromization of the primary body are prevented from being transferred to the secondary body in a manner that prevents the secondary body from becoming structurally compromised, and vice-versa,
wherein the mechanical connection comprises a plurality of mechanical fasteners, with each mechanical fastener passing through both the primary body and the secondary body,
wherein the primary body includes a plurality of side portions that are integrally formed with at least one intermediate portion that sets a distance between the side portions, and
wherein the secondary body is attached to the side portions.

Assignees

• Airbus Operations Gmbh

Inventors

• Daandels Dort
• Gibbert Markus
• Coskovic Blazenko

Classifications

• B64C9/02 Primary

  Mounting or supporting thereof · CPC title

• B64C3/50

  by leading or trailing edge flaps · CPC title