A connection for mounting an aircraft engine (20) to an aircraft pylon (62) has a plate (102) to be bolted to a portion (60) of an aircraft engine (20), and a body (104) extending rearwardly from the plate (102). The body (104) has a main pivot attachment (106) to a balance beam (108), which has thrust links (110) pivotally attached to the balance beam (108). A back-up connection (112) is included between the balance beam (108) and the body (104) such that the back-up connection (112) allows normal pivoting movement of the balance beam (108) relative to the body (104) without contact at the back-up connection (112).
GAS TURBINE ENGINE MOUNTING STRUCTURE WITH SECONDARY LOAD PATH
GASTURBINENMOTORMONTAGESTRUKTUR MIT SEKUNDÄREM LASTPFAD
STRUCTURE DE MONTAGE DE MOTEUR À TURBINE À GAZ AVEC TRAJET DE CHARGE SECONDAIRE
2018-07-11
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
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