Aircelle Limited

Snecma

Francois Conte

Guillaume Lefort

Guy Bernard Vauchel

Pierre-Alain Jean-Marie Philippe Hugues Chouard

Jerome Collier

Nicolas Hillereau

Pierre-Alain Chouard

Patrice Dhainault

Andre Bruno Denis Baillard

The nacelle () comprises an air intake () upstream of the turbojet engine (), a middle section () an internal casing () of which is intended to surround a fan () of the turbojet engine (), and a downstream section () comprising an external structure (which is rigidly connected to a downstream part of the casing () of the fan () so as to support the turbojet engine () and has means of attachment to a strut () intended to be connected to a fixed structure () of an aeroplane.

Bypass turbojet engine nacelle

A turbojet suspended from an aircraft mast is disclosed. The turbojet includes a front fan, an intermediate casing downstream of the fan with an outer shroud and a hub connected together by radial arms, and an exhaust casing with an outer shroud, the two casings being aligned on one and the same axis XX. The mast includes a structural strut assembly of elongated shape. The strut assembly is attached upstream rigidly to the outer shroud of the intermediate casing by a front attachment including a device for transmitting the axial and lateral forces and downstream by a rear attachment to the exhaust casing.

Turbojet suspended from an aircraft mast

Growing community of inventors

Tournefeuille, France

Francois Conte