Snecma

Baghdad Achbari

Mario Cesar De Sousa

Nicolas Pommier

Frederic Noel

Gregory Ghosarossian-Prillieux

Benoit Argemiro Matthieu Debray

Luc Henri Claude Daguenet

Mathieu Ange Poisson

Audrey Charrie

Arthur Cohin

Aurélien René-Pierre Massot

Benoit Debray

Sylvain Pichon

An assembly including an exhaust casing and an exhaust cone for a gas turbine engine, each including an axial annular flange, the two flanges being inserted into one another, one being radially external and the other radially internal, and held together by a mechanical attachment, and the assembly further including a guide by which, during operation of assembling the annular flanges to each other, the exhaust cone is in a predetermined angular position relative to the exhaust casing.

Gas turbine engine comprising an exhaust cone attached to the exhaust casing

A cooling device for the casing of a jet engine, includes a cooling tube and a supporting device, the supporting device including an attachment plate and an attachment clamp, the attachment clamp including a clamp body surrounding the cooling tube and an attachment element attached to the attachment plate, wherein the attachment plate includes: an opening; and an attachment tab secured to the main wall of the attachment plate and arranged on at one portion of the periphery of the opening, the attachment clamp passing through the opening, and the attachment element of the attachment clamp being attached to the attachment tab.

Cooling device for the casing of an aircraft jet engine comprising a supporting device

A method for assembling a nozzle and an exhaust case of a turbomachine is disclosed. The exhaust case includes a hub and an outer ferrule connected to each other by a plurality of arms. The nozzle is attached to the outer ferrule of the exhaust case substantially at the trailing edges of the arms.

Method for assembling a nozzle and an exhaust case of a turbomachine

Growing community of inventors

Montereau Fault Yonne, France

Baghdad Achbari