Linking device connecting an aircraft engine and a primary structure of an aircraft pylon comprising a spreader and a system for limiting the out-of-plane deflection of the spreader, aircraft comprising such a linking device

Patent metadata

Field	Value
Publication number	US-11325715-B2
Application number	US-202016807351-A
Country	US
Kind code	B2
Filing date	Mar 3, 2020
Priority date	Mar 5, 2019
Publication date	May 10, 2022
Grant date	May 10, 2022

Abstract

A linking device connecting an aircraft engine and a primary structure of an aircraft pylon, comprising a support connected to the primary structure, a spreader, extending between first and second ends that has a central part connected to the support by a principal link comprising a principal rotation axis, at least one system for limiting the deflection of the spreader comprising an extension secured to the spreader and also upper and lower stops, secured to a fitting secured to the support, between which the extension is positioned.

First claim

The invention claimed is:

1. A linking device connecting an aircraft engine and a primary structure of an aircraft pylon, comprising:
a support connected to the primary structure,
a spreader, extending between first and second ends, that has a central part connected to the support by a principal link comprising a principal rotation axis,
a first thrust rod comprising a first end connected to the first end of the spreader by a first secondary link and a second end connected to the engine,
a second thrust rod comprising a first end connected to the second end of the spreader by a second secondary link and a second end connected to the engine,
first and second fittings, secured to the support, comprising upper and lower branches, between which the spreader is positioned,
the linking device generating a deflection of the spreader that is configured to pivot about a deflection rotation axis perpendicular to the principal rotation axis and contained in a plane of symmetry passing via the principal rotation axis,
wherein the linking device comprises at least one system for limiting the deflection of the spreader comprising an extension secured to the spreader and also upper and lower stops, secured to the first or second fitting, between which the extension is positioned.

2. The linking device according to claim 1 , wherein the at least one system for limiting the deflection of the spreader is configured such that a sum of distances between the upper stop and the extension and also between the lower stop and the extension is less than or equal to 0.3 mm.

3. The linking device according to claim 1 , wherein the linking device comprises first and second systems for limiting the deflection of the spreader which are secured, respectively, to the first and second fittings.

4. The linking device according to claim 1 , wherein each upper or lower stop comprises a contact face against which the extension is configured to bear, at least one of the contact faces comprising a shock-absorbing covering.

5. The linking device according to claim 1 ,
wherein, for each system for limiting the deflection, the upper and lower stops are out-of-joint with the fitting, and
wherein each device for limiting the deflection comprises a plate, fixed to the fitting, to which the upper and lower stops are connected.

6. The linking device according to claim 5 , wherein the upper stop comprises a first flange placed against an exterior face of the upper branch of the fitting and wherein the lower stop comprises a second flange configured such as to be placed against an exterior face of the lower branch of the fitting.

7. The linking device according to claim 1 , wherein, for each system for limiting the deflection, the upper and lower stops are out-of-joint with the fitting and independent of one another, the upper stop being connected to the upper branch of the fitting and the lower stop being connected to the lower branch of the fitting.

8. The linking device according to claim 7 , wherein each upper or lower stop comprises:
a body that has a first face forming a contact face against which the extension is able to bear and a second face, parallel to the first face, placed against an interior face of the upper or lower branch of the fitting, and
a flange made as a single piece with the body, placed against a lateral face of the upper or lower branch of the fitting.

9. The linking device according to claim 8 , wherein the flange comprises a stud interacting with a notch provided at the lateral face of the upper or lower branch of the fitting.

10. The linking device according to claim 1 , wherein, for each system for limiting the deflection, the upper stop is integrated into the upper branch of the fitting and the lower stop is integrated into the lower branch of the fitting.

11. The linking device according to claim 10 , wherein the upper branch comprises an upper flange, projecting from an interior face of the upper branch, which has an interior face against which the extension is able to bear and wherein the lower branch comprises a lower flange, projecting from an interior face of the lower branch, which has an interior face against which the extension is able to bear.

12. An aircraft comprising a linking device according to claim 1 .

Assignees

• Airbus Operations Sas

Inventors

• Deforet Thomas
• Lansiaux Rémi
• Dubois Olivier
• Mertes Anthony
• Alric David
• Nogues Stéphane

Classifications

• B64D27/404

  Suspension arrangements specially adapted for supporting vertical loads · CPC title

• B64D27/406 Primary

  Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links · CPC title

• B64D27/18

  within, or attached to, wings · CPC title

• B64D2027/268

  Operations & Transport · mapped topic

• B64D27/26 Primary

  Operations & Transport · mapped topic