The invention relates to a fixed interior structure (200) for a nacelle comprising end panels (200a), an intermediate semi-cylindrical panel (200c) between the end panels (200a), splice plates (210a) between the intermediate panel (200c) and each end panel...

L'invention a pour objet un ensemble de propulsion d'aéronef comportant un moteur (62), une nacelle (66) positionnée autour du moteur (62), un conduit annulaire (68) délimité par le moteur (62) et la nacelle (66) dans laquelle s'écoule un flux seconda...

A nacelle (116) is configured to be coupled to an underside of a wing (114) and forms a clearance space (154) between the nacelle (116) and a leading edge slat (122) of the wing (114). A portion of an outlet cowling (150) moves longitudinally aft when a re...

A nacelle (22) for a turbofan propulsion system is provided that extends along a centerline (24) and includes a forward cowling (36) and an aft cowling (38). To improve the fit of a turbofan propulsion system in the space between the wing and ground of a f...

An aircraft comprising an aeroengine (10) and a noise reflective surface (33), the aeroengine (10) capable of generating a hot exhaust jet (30) and noise characterised in that the reflective surface (33) is profiled to reflect noise from the aeroengine (10...