Propulsion assembly for an aircraft having a turbojet with a non-ducted fan and an attachment pylon
A propulsion assembly for an aircraft, the assembly including a turbojet having at least one unducted propulsive propeller, and an attachment pylon for attaching the turbojet to a structural element of the aircraft, the pylon being positioned on the turbojet upstream from the propeller and having a...
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Main Authors | , |
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Format | Patent |
Language | English |
Published |
11.08.2020
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Subjects | |
Online Access | Get full text |
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