An aircraft nacelle comprising an air intake configured to channel an air flow in the direction of an engine assembly which comprises a fan with an axis of rotation, said air intake comprising, according to a flow direction of the air flow, a lip with a leading edge and an internal conduit which extends said lip towards the fan, wherein the air intake comprises a plurality of protrusions distributed over the circumference of the air intake and following each protrusion, a concave form configured in order to achieve compression of the air flow.
NACELLE D'AERONEF COMPRENANT UNE ENTREE D'AIR
AIRCRAFT NACELLE INCLUDING AN AIR INTAKE
LUFTFAHRZEUGGONDEL, DIE EINEN LUFTEINLASS UMFASST
04.01.2017
Patent
Elektronische Ressource
Französisch
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