A front engine attachment system having an engine pylon having a frontal rib fastened against a front face, a front engine attachment having a beam fastened to the frontal rib, two rods articulated to the beam respectively via two connection points and one connection point, and a front casing of an engine, wherein the first rod is articulated to the front casing via a connection point and wherein the second rod is articulated to the front casing via a connection point, wherein each point of connection of a rod to the beam is positioned inside a volume that extends the front face of the engine pylon towards the front. Such a front engine attachment system has reduced bulk and therefore less drag.
FRONT ENGINE ATTACHMENT SYSTEM FOR AN AIRCRAFT ENGINE, WHICH HAS A COMPACT STRUCTURE
2023-03-09
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 | 2024
|Front engine attachment system for aircraft engine having compact structure
European Patent Office | 2023
|FRONT ENGINE ATTACHMENT SYSTEM FOR AN AIRCRAFT ENGINE, WHICH HAS A COMPACT STRUCTURE
European Patent Office | 2025
|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
|