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
21.12.2017
Patent
Elektronische Ressource
Englisch
Assembly for aircraft comprising engines with boundary layer ingestion propulsion
Europäisches Patentamt | 2020
|Aircraft propulsion assembly and aircraft comprising such aircraft propulsion assembly
Europäisches Patentamt | 2023
|Aircraft propulsion assembly and aircraft comprising such propulsion assembly
Europäisches Patentamt | 2024
|AIRCRAFT PROPULSION ASSEMBLY COMPRISING A FAN CONJOINTLY DRIVEN BY TWO ENGINES
Europäisches Patentamt | 2018
|Aircraft propulsion assembly and aircraft comprising such assembly
Europäisches Patentamt | 2024
|