In order to further benefit from the principle of boundary layer ingestion by engines of an aircraft assembly, the rear portion of the fuselage of this aircraft assembly includes a front portion which splits up into at least two distinct rear portions, spaced apart from each other, and each integrating the rotary ring of the receiver of one of the engines.
ASSEMBLY FOR AIRCRAFT COMPRISING ENGINES WITH BOUNDARY LAYER PROPULSION BY INJECTION
2017-12-21
Patent
Electronic Resource
English
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