FIELD: transport.
SUBSTANCE: bypass turbojet engine cowling air intake with front suction branch pipe comprises top and bottom parts, inner (closer to fuselage) lateral side (115int) and outer lateral side (115ext) that define front edge (115) between cowling outer wall (111) and inner wall (113) that forms engine air feed channel. Front edge of external lateral wall (115ext) is arranged behind relative to front edge of inner lateral side (115int). Bypass turbojet engine may be equipped with such air intake.
EFFECT: reduced noise.
7 cl, 4 dwg
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