Propulsive assembly with enhanced engine cowl articulated in rotation on an axis of rotation positioned above top face of engine pylon, and aircraft comprising such an assembly

Abstract

An aircraft propulsive assembly including an engine pylon having a top face, an internal engine part, a possible fixed top cowling of the engine pylon and at least one engine cowl articulated in rotation on an axis of rotation defined by at least two articulation hinges. The axis of rotation of the at least two articulation hinges is positioned above the top face of the engine pylon. It is possible to assemble a nacelle fairing around the internal part of the engine, in the absence of the external part composed of the fan fairing, and without modifying the structure of the engine pylon except with respect to the arrangement of the hinge fittings of the movable engine cowls.

Dependencies are inferred from the claim text.