- Patent Title: 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
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Application No.: US16807351Application Date: 2020-03-03
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Publication No.: US11325715B2Publication Date: 2022-05-10
- Inventor: Thomas Deforet , Rémi Lansiaux , Olivier Dubois , Anthony Mertes , David Alric , Stéphane Nogues
- 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: FR1902219 20190503
- Main IPC: B64D27/26
- IPC: B64D27/26
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.
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