Safran Aircraft Engines

Yann Christophe Maurice Sarazin

Patrick Jean-Louis Reghezza

Simon Pierre Claude Charbonnier

Julien Roset

An intermediate casing for a turbine engine, comprising at least one central hub and one shroud () which are positioned concentrically, and mutually mechanically connected by structural arms (), with such casing comprising at least one sealing part () attached between the shroud () and a structural arm (), with the sealing part () including at least one metal core and one seal.

Intermediate casing of a turbine engine, provided with a sealing part at the arm/shroud interface

An attachment system intended to equip a wall, the system including a nut intended to receive a screw of which the orientation is normal to the wall, the screw passing through an element such as an outer panel in order to attach the element to the wall. The attachment system comprises a socket having a threaded cylindrical outer face intended to be screwed into a hole passing through the wall and having dimensions greater than the dimensions of the fastener that the repair socket replaces, the socket carrying, in the central region of same, a nut receiving the screw.

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Moissy-Cramayel, France

Yann Christophe Maurice Sarazin