Safran Aero Boosters Sa

Théo Robin Thomas Bour

Christophe Joseph Richard Gillain Remy

Matthieu Edouard Henri Droeller

A stator vane assembly for a compressor of an aircraft turbine engine includes an inner shroud, an outer shroud, and stator vanes. The stator vanes are attached only to the inner shroud and are in non-immobilizing mechanical contact with the outer shroud.

Stator vane assembly for an aircraft turbine engine compressor

A group of stator vanes for a row of stator vanes of a stage of a turbomachine compressor, the vanes of the group of stator vanes being close together and affording easy assembly. The group of stator vanes include a platform of a first vane having an aperture for accommodating the head of a second vane, the outer surface of the platform of the first vane being in contact with the inner surface of the platform of the second vane.

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Herstal, Belgium

Théo Robin Thomas Bour