Snecma

Safran Aircraft Engines

Sylvain Dousseaud

Gregory Nicolas Gerald Gillant

Stéphane Clemot

Grégory Nicolas Gérald Gillant

Gregory Nicolas Gillant

A part to modify the profile of an aerodynamic jet, including: a first face configured to be secured on the aerodynamic jet, and a second face defining a modified aerodynamic jet profile, configured to modify an initial profile of the aerodynamic jet.

Part to modify the profile of an aerodynamic jet

The invention relates to an insert for a turbine engine test vane including the insert and a vane body. The insert includes at least two external surfaces. The insert is configured to fit into the vane body, such that the external surfaces are vane aerodynamic surfaces each forming part of a vane aerodynamic profile.

Growing community of inventors

Savigny-Le-Temple, France

Sylvain Dousseaud