| 摘要 |
Propulsion system with integrated pylon Propulsion system comprising a bypass turbojet and a nacelle ( 10 ) a downstream cylindrical part ( 20 ) of which is rigid and is attached at its upstream end to an intermediate case of the engine, this downstream cylindrical part ( 20 ) also comprising a longitudinal beam ( 26 ) for attaching rods ( 28 ) for securing the engine to part ( 22 ) of an airplane.
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