- Patent Title: Aircraft propulsion assembly comprising links of a front engine mount that are directly connected to a front transverse reinforcement of a primary structure of an aircraft pylon
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Application No.: US17407251Application Date: 2021-08-20
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Publication No.: US11542025B2Publication Date: 2023-01-03
- Inventor: Michael Berjot , Thomas Deforet , Jacky Puech
- Applicant: Airbus Operations SAS
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations SAS
- Current Assignee: Airbus Operations SAS
- Current Assignee Address: FR Toulouse
- Agency: Greer, Burns & Crain, Ltd.
- Priority: FR2008634 20200824
- Main IPC: B64D27/26
- IPC: B64D27/26

Abstract:
A propulsion assembly including a primary structure of a pylon having right and left extensions projecting with respect to right and left lateral panels of the primary structure and also right and left brackets, each having a first flank connected to the right or left lateral panel of the primary structure and a second flank pressed against the right or left extension, a front engine mount having first and second links, each connected to an engine and directly to the front transverse reinforcement by a first or second reinforcement connection pin passing through the right or left extension and the second flank of the right or left bracket.
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