Invention Grant
- Patent Title: Rear engine fastener for an aircraft having reduced volume widthwise and an aircraft comprising at least one such rear engine fastener
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Application No.: US16819941Application Date: 2020-03-16
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Publication No.: US11459115B2Publication Date: 2022-10-04
- Inventor: Julien Cayssials , Michael Berjot
- 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: FR1902776 20190318
- Main IPC: B64D27/26
- IPC: B64D27/26

Abstract:
A rear engine fastener for an aircraft connecting a primary structure and an engine of an aircraft, the rear engine fastener comprising a support configured to be connected to the primary structure, at least one main shackle connected to the support by first and second support link pins, which are symmetrical relative to a vertical longitudinal plane, and to the engine by a first lateral engine link pin and by a central engine link pin, and at least one secondary shackle connected to the engine by a second lateral engine link pin and to the main shackle by a secondary link pin.
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