An aircraft engine assembly includes a dual-flow turbine engine, a pylon for mounting the turbine engine, thrust-absorbing rods connecting the turbine engine to the pylon, and an inter-flow compartment housing a lubricant tank. In order to facilitate the filling of the tank, a lubricant supply path is fluidly connected to the tank, this path passing through an inner hollow region of at least one of the two thrust-absorbing rods.
AIRCRAFT ENGINE ASSEMBLY WITH A SUPPLY PATH TO AN INTER-FLOW COMPARTMENT TANK OF TURBINE ENGINE
2021-04-22
Patent
Elektronische Ressource
Englisch
Aircraft engine assembly with a supply path to an inter-flow compartment tank of turbine engine
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