An engine mounting arrangement (22) comprising thrust struts (26), a balance yoke (58), and primary (30) and secondary (32) mount blocks, the thrust struts (26) being connected to the balance yoke (58) and the primary mount block (30) comprising at least one thrust load connection (42) connectable to the balance yoke (58) for transferring thrust loads from an engine (210) during normal operation of the engine mounting arrangement (22), characterised in that the secondary mount block (32) is connected to the balance yoke (58) via at least one thrust load catcher connection (76), the at least one thrust load catcher connection (76) being arranged to be unloaded during normal operation of the engine mounting arrangement (22) and to transfer the thrust loads from the engine (210) in the event of a failure condition of the primary mount block (30).
Engine mounting arrangement
Triebwerkmontageanordnung
Agencement d'assemblage de moteur
2017-03-01
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2021
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