Aircraft`s engine assembly, has external skins forming part of aerodynamic surface of nacelle, and pylon with front engine mounts fixed to fan casing and bearing thrust force, where pylon is located remote from heat part of turbojet engine

摘要

The assembly has a pylon (4) located remote from a heat part of a turbojet engine and comprising a rigid structure with lateral cases (24a, 24b) integrated to a longitudinal case. External skins (44a, 44b) respectively close the lateral cases and form a part of an external aerodynamic surface (33) of a nacelle (3). The pylon has front engine mounts fixed to a fan casing and arranged on the respective lateral cases, where the mounts bear thrust force generated by the engine. The pylon has a rear engine mount fixed on a central case of the engine.