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.
REAR ENGINE FASTENER FOR AN AIRCRAFT HAVING REDUCED VOLUME WIDTHWISE AND AN AIRCRAFT COMPRISING AT LEAST ONE SUCH REAR ENGINE FASTENER
2020-09-24
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2022
|European Patent Office | 2022
|European Patent Office | 2020
|