Invention Grant
- Patent Title: Primary structure of a strut for bearing an aircraft power plant, the rear part of which is formed by a set of connecting rods
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Application No.: US16352332Application Date: 2019-03-13
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Publication No.: US11332255B2Publication Date: 2022-05-17
- Inventor: Olivier Pautis , Jérôme Colmagro , Jonathan Blanc
- Applicant: Airbus Operations (S.A.S.)
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations (S.A.S.)
- Current Assignee: Airbus Operations (S.A.S.)
- Current Assignee Address: FR Toulouse
- Agency: Jenkins, Wilson, Taylor & Hunt, P.A.
- Priority: FR1852228 20180315
- Main IPC: B64D27/26
- IPC: B64D27/26

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.
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