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US 2017/0361939 A1Published application
Assembly for aircraft comprising engines with boundary layer propulsion by injection
AssigneeAirbus Operations GmbH
InventorsCamil NEGULESCU, Jean-Michel ROGERO, Renaud FAURE
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Abstract
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.
Claims17
An assembly for aircraft comprising:
- a rear portion of a fuselage,
- at least two engines with propulsion by boundary layer ingestion circulating on the rear portion of fuselage,
- each engine comprising a receiver equipped with a rotary ring from which bladed elements project radially to the outside,
- said rear portion of the fuselage including a front portion which splits up into at least two distinct rear portions, spaced apart from each other, and each rear portion integrating the rotary ring of one of said engines.
1 more element
Dependencies are inferred from the claim text.