A connection for mounting an aircraft engine to an aircraft pylon includes a plate to be connected to a portion of an engine, and a body that extends rearward from the plate. A back-up connection, including a pin positioned within a slotted hole, is provided between the portion of the engine and the body. When there is a normal connection between the plate and the body, there is clearance between the pin and the slotted hole.
GAS TURBINE ENGINE MOUNTING STRUCTURE WITH SECONDARY LOAD PATHS
MONTAGESTRUKTUR MIT SEKUNDÄREN LASTPFADEN FÜR EINEN GASTURBINENMOTOR
STRUCTURE DE MONTAGE DE MOTEUR À TURBINE À GAZ DOTÉE DE CHEMINS DE CHARGE SECONDAIRES
2016-12-21
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Gas turbine engine mounting structure with secondary load path
European Patent Office | 2017
|GAS TURBINE ENGINE MOUNTING STRUCTURE WITH SECONDARY LOAD PATH
European Patent Office | 2018
|