Aircelle Limited

Stéphane Bardin

Florent Bouillon

Bertrand Desjoyeaux

Alexandre Bellanger

Laurent Dubois

John Moutier

Christophe Thorel

A unit for an aircraft thruster is provided that includes a first ferrule configured to be attached to a second ferrule and a first connection flange configured to be secured to a second corresponding connection flange secured to the second ferrule. The connection flange includes a portion forming a plane extending along a radial direction with respect to the first ferrule. A link between the first ferrule and the corresponding connection flange is offset to a distance from said plane corresponding to a length for damping a shear-generating flexural moment, generated by fluxes of forces passing through the first ferrule.

Unit for an aircraft thruster

A stub frame for a cascade vane thrust reverser structure of an aircraft nacelle is attached to one or more cascade vanes. The stub frame includes an integral primary structure with a C-shaped longitudinal section, a secondary structure acting as a cascade edge and attached to the primary structure at one end, and transverse stiffeners connecting the two ends of the primary structure.

Stub frame for a cascade thrust reverser structure

Growing community of inventors

Le Havre, France

Stéphane Bardin