Primary structure of a strut for bearing an aircraft power plant, the rear part of which is formed by a set of connecting rods

Patent metadata

Field	Value
Publication number	US-11332255-B2
Application number	US-201916352332-A
Country	US
Kind code	B2
Filing date	Mar 13, 2019
Priority date	Mar 15, 2018
Publication date	May 17, 2022
Grant date	May 17, 2022

Abstract

A primary structure of a strut for bearing an aircraft power plant including a front part intended to be joined to an aircraft power plant and a rear part intended to be joined to a structure of the aircraft, the front part being formed from a box including an upper longitudinal member, a lower longitudinal member, and lateral panels. A main rib is located at an interface between the front part and the rear part. The rear part is formed from a set of four connecting rods. The first end of each connecting rod is joined to the front part of the primary structure and the second end of each connecting rod is joined to a separate interface for fastening to the structure of the aircraft. This allows a substantial simplification of the primary structure of a strut for bearing an aircraft power plant, which can have advantages in particular in terms of cost, mass, and simplicity of implementation and integration.

First claim

The invention claimed is:

1. A primary structure of a strut for bearing an aircraft power plant comprising:
a front part to be joined to an aircraft power plant and a rear part to be joined to a structure of the aircraft;
the front part having a box shape including an upper longitudinal member, a lower longitudinal member, and lateral panels;
the primary structure including a main rib located at an interface between the front part and the rear part;
wherein the main rib extends vertically beyond the upper longitudinal member of the front part of the primary structure to form a plane for fastening to the structure of the aircraft;
wherein the rear part is formed from a set of connecting rods, each connecting rod including a first end and a second end, the first end of each connecting rod being joined to the front part of the primary structure and the second end of each connecting rod being joined to a separate interface for fastening to the structure of the aircraft; and
wherein there are four connecting rods, an intersection of the main rib with the front part of the primary structure forming a quadrilateral including four corners, one connecting rod being joined to the front part substantially at each of the corners.

2. The primary structure according to claim 1 , wherein each connecting rod is joined using a hinged or ball joint to the front part, at separate joining points.

3. The primary structure according to claim 1 , wherein each connecting rod is, over at least the majority of the length thereof, formed either from a flat bar, or from two parallel flat bars, or from a tube with a triangular, square, rectangular or round section.

4. The primary structure according to claim 1 , wherein the set of connecting rods comprises lower connecting rods and upper connecting rods, and wherein the lower connecting rods and the upper connecting rods have, over at least the majority of a length thereof, different sections, respectively.

5. The primary structure according to claim 1 , wherein the set of connecting rods comprises lower connecting rods and upper connecting rods, and wherein the lower connecting rods have a length that is different to a length of the upper connecting rods.

6. The primary structure according to claim 1 , wherein an intersection of the main rib with a plane parallel to the lower longitudinal member is inclined with respect to a transverse direction, which is orthogonal in the plane to a longitudinal direction corresponding to an extension direction of the front part of the primary structure.

7. The primary structure according to claim 1 , wherein the lateral panels of the front part each include an extension, beyond the main rib, each extension including at least one eyelet for fastening a connecting rod.

8. The primary structure according to claim 1 , wherein each interface for fastening to the aircraft structure, joined to the second end of a connecting rod, includes a hinged or ball joint with the second end of the connecting rod, and a plate for joining to the structure of the aircraft.

9. An aircraft comprising at least one wing, at least one power plant being fitted under the wing, wherein the power plant is joined to a mechanical structure of the wing by a bearing strut including a primary structure according to claim 1 .

Assignees

• Airbus Operations Sas

Inventors

• Pautis Olivier
• Colmagro Jérôme
• Blanc Jonathan

Classifications

• B64D27/402 Primary

  comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant · CPC title

• B64D2027/264

  Operations & Transport · mapped topic

• B64D27/26 Primary

  Operations & Transport · mapped topic

• B64D27/40 Primary

  Arrangements for mounting power plants in aircraft · CPC title