A front engine attachment system for an engine having an engine pylon with a nose having a main female clevis and a cylindrical housing, a main rod fastened to the engine by a secondary ball joint connection about a secondary axis, a main shaft realizing a main ball joint connection of the main rod in the main female clevis about a main axis, wherein the main axis and the secondary axis are in the same vertical plane, a hollow outer cylinder with a vertical axis, of which a first end is fastened in the cylindrical housing and of which a second end is mounted so as to be able to move, via an annular linear connection, with respect to the front casing and an inner cylinder threaded and fastened in the outer cylinder.
FRONT ENGINE ATTACHMENT SYSTEM FOR AN AIRCRAFT ENGINE, WHICH HAS A COMPACT STRUCTURE
2025-01-02
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
FRONT ENGINE ATTACHMENT SYSTEM FOR AN AIRCRAFT ENGINE, WHICH HAS A COMPACT STRUCTURE
European Patent Office | 2023
|Front engine attachment system for an aircraft engine, which has a compact structure
European Patent Office | 2024
|Front engine attachment system for aircraft engine having compact structure
European Patent Office | 2023
|Front engine attachment system intended for aircraft engine and having compact structure
European Patent Office | 2024
|FRONT ENGINE ATTACHMENT SYSTEM INTENDED FOR AN AIRCRAFT ENGINE AND HAVING A COMPACT STRUCTURE
European Patent Office | 2025
|