Airbus Operations (s.a.s.)

Airbus Operations Gmbh

Frédéric Journade

Lionel Czapla

Laurent Lafont

Jean Geliot

Thomas Deforet

Frédéric Vinches

Julien Cayssials

Laurent Cazeaux

Eric Bouchet

Rémi Amargier

Delphine Jalbert

Eric Renaud

Christophe Labarthe

Kotaro Fukasaku

Franck Alvarez

Pierre Charon

Pascal Gougeon

Mathieu Bonnet

Esteban Quiroz-Hernandez

Emmanuel Vardelle

Jean-Michel Saucray

Mathieu Kaleta

Laurent Agostini

Mathieu Mahe

Robert Brunet

Antoine Claveyrollas

Nicolas Grosseau

Antoine Mutin

Jérôme Huber

Etienne Bardou

Jérôme Journade

Jérôme Antypas

Jean Michel Saucray

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 system includes a bypass turbine engine and a pylon. The turbine engine includes an engine, two internal cowls, two outer cowls, a first lock for locking the internal cowls to the engine, cascades of vanes fixed to the outer cowl via hooping, wherein the outer cowls are movable in translation with respect to the engine, in which each outer cowl is able to slide parallel to a direction of translation on an internal cowl via a top guideway connection and a bottom guideway connection, and in which each outer cowl is mounted with the ability to slide parallel to the direction of translation on the pylon via an upper guideway connection. The propulsion system makes it possible during maintenance operations to move the outer cowl and the internal fixed structure towards the rear and therefore away from the front cowls to get at the engine.

Aircraft propulsion system comprising a mobile articulated cowl

An aircraft engine assembly including an attachment mechanism of a turbojet onto a rigid structure of a mounting strut, including a first, second, and third forward engine attachment for taking up thrust loads brought onto the fan frame, and arranged such that the third attachment passes through a first diametrical plane of the turbojet, the first and second attachments being disposed on one side and another of the first plane. The first and second forward engine attachments are respectively brought to the fan frame at two points, situated beyond the second diametrical plane of the turbojet, orthogonal to the first diametrical plane, with respect to the third attachment.

Engine assembly for an aircraft comprising attachments for engines offset below on the fan frame

An aircraft engine assembly including an annular structure surrounding a central casing and mechanically connected to the central casing by the intermediary of a mounting mechanism. To each of the first and second engine mounts is associated a reinforcing structure forming a shear plane, fixedly connected: in an area of the annular structure at a first anchoring point; in an area of the fan casing at a second anchoring point; and in an area of a structural arm or of the intermediate casing at a third anchoring point. The structure extends along a radial imaginary plane passing through an anchoring point of the mount on the fan casing.

Aircraft engine assembly comprising a turbojet engine with reinforcing structures connecting the fan casing to the central casing

This invention relates to an aft pylon fairing for the suspension system of an aircraft engine, comprising a main structure extending along a longitudinal direction of said fairing and integrating two side panels connected to each other, the fairing also comprising a heat protection deck mounted on said main structure through connection means comprising tabs designed to deform to accompany displacement of the deck relative to the main structure, if there is differential thermal expansion between these two entities.

Aft pylon fairing for aircraft engine suspension system, comprising a heat shield capable of expanding freely

An aircraft engine assembly with an annular load-transfer structure surrounding the central casing () and mechanically connected to a plurality of substantially planar reinforcing structures (-) arranged externally with respect to the annular load-transfer structure, and biasing it at a plurality of load application points (). At least one connecting rod is associated with a load application point, with the connecting rod positioned tangentially with respect to the casing (), and having an inner end () connected to this casing, as well as an outer end () connected to the annular load-transfer structure () so that the outer end of the connecting rod is in an imaginary plane () in which the annular load-transfer structure is located and which extends through the load application point.

Aircraft engine assembly comprising an annular load-transfer structure surrounding the central casing of a turbojet engine

A device for locking an engine on a pylon includes two systems attaching the engine to the pylon, located in attachment regions spaced out in a longitudinal direction of the engine. A second region is adjacent to a center of gravity plane of the engine and closer to a fan than a first region. A first system attaching to the first region is rigid towards torsional, transverse and vertical engine forces. The first region is located at a separation between two compressors of the engine or two turbines, whether the fan is at a rear or front of the engine respectively, the separation being adjacent to a node of a first engine flexural mode. A second system attaching to the second region is rigid towards transverse and vertical forces but less rigid than the first system. The device also includes a third system withstanding thrust forces in the longitudinal direction.

Device for locking an engine on an aircraft pylon

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Toulouse, France

Frédéric Journade