Airbus Operations (s.a.s.)

Antoine Claveyrollas

Thomas Deforet

Mathieu Kaleta

Mathieu Mahe

Eric Renaud

Frédéric Journade

Ginesa Torres Lopez

A propulsion assembly for an aircraft, the propulsion assembly having a jet engine having a fan casing and a central casing around a longitudinal axis and having a vertical median plane passing through the longitudinal axis, an attachment pylon having a rigid structure that takes the form of a box that has a front wall and an upper spar extending forwardly in respect to the front wall, a front engine attachment fixed between an upper area of the central casing and a lower end of the front wall, and a complementary front engine attachment fixed between an upper area of the fan casing and a front end of the upper spar.

Aircraft propulsion assembly having a jet engine, a pylon and means for attaching the jet engine to the pylon

A propulsion assembly comprising a fan casing and a nacelle which comprises an air inlet which is connected to the front end of the fan casing, an intermediate portion which is positioned around the fan casing and a rear portion which cooperates with the rear end of the fan casing. The intermediate portion comprises at least one aerodynamic panel which extends from a front edge which is attached to the air inlet as far as a rear edge which is attached to the rear portion and at least one intermediate radial support comprising an internal edge which is connected to the fan casing and an external edge which is connected to the aerodynamic panel, this panel comprising a front edge which is connected to the air inlet by a first connection system. Also an aircraft with such a propulsion assembly.

Aircraft propulsion assembly comprising at least one aerodynamic panel which is supported by at least one intermediate radial support, aircraft comprising at least one such propulsion assembly

Growing community of inventors

TOULOUSE, France

Antoine Claveyrollas