Safran Aircraft Engines

Christophe Lima

Alain Dominique Gendraud

Gael Evain

Florence Irène Noëlle Leutard

Giuliana Elisa Rossi

Boucif Bensalah

Eddy Stéphane Joël Fontanel

Alberto Martin Matos

Gaël Evain

Sebastien Bourget

Sébastien Bourget

Valentin Olivier Jean-Jacques Quesnel

Jérémy Lucien Jacques Bioud

Eddy Stephane Fontanel

Florence Irene Leutard

Jeremy Lucien Bioud

A turbomachine module with a longitudinal axis comprising an unducted propeller rotated about the longitudinal axis and at least one straightener. The module includes a plurality of unducted variable-pitch stator blades extending along a radial axis, perpendicular to the longitudinal axis, from a fixed casing. The module includes a first stator blade pitch-changing system. The pitch-changing system includes at least one first control that includes a first fixed body connected to the fixed casing and a first body which is axially mobile in relation to the first fixed body and at least one first joining mechanism joining each stator blade to the first mobile body of the first control. The first joining mechanism includes: a joining ring centered on the longitudinal axis, joined to the feet of each stator blade and at least one lever joined, on one hand, to the joining ring and, on the other hand, to the first mobile body of the first control.

Turbomachine module equipped with a blade pitch-changing system of a stator vane

A system for the axial retention of a holding ring for a bearing for guiding in rotation a rotary shaft of a turbomachine is disclosed. The system includes an annular bearing support and a bearing holding ring that is borne by the annular bearing support. The bearing holder ring includes an upstream ring configured to be brought into contact with the bearing support and a downstream ring that is elastically deformable. The bearing support has a first axial retention element, and the bearing holding ring has a second axial retention element. The first and second axial retention elements are configured to cooperate with one another to axially retain the bearing holding ring in the event of damage to the downstream ring.

System for the axial retention of a rolling element bearing

A turbomachine bearing housing comprising a fixed wall, a rotating shaft, first and second seals between the wall and the shaft, and a chamber between the fixed wall and a stator element supplied with air via an opening close to the shaft. An air guide is arranged along the surface of the wall of the housing, outside same, such that at least a portion of the air exiting the guide passes between the first seal and the shaft, the air guide being supplied with air by an air intake separated radially from the shaft, the air from the air intake being at a higher pressure than at the shaft.

Turbomachine bearing housing

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Moissy-Cramayel, France

Christophe Lima