Snecma

Safran Aircraft Engines

Olivier Chantoiseau

Jean-Baptiste Mottin

Laurent Gilles Dezouche

Stéphane Roger Mahias

Beryl Cassandre Anne Mereaux

Thomas Vilaro

Sebastien Rix

Sophie Martine Jobez

Bruno Le Razer

Beryl Cassandre Mereaux

The invention relates to a turbomachine blade comprising a vane. The vane comprises a leading edge, a trailing edge, a pressure face and a suction face spaced apart from each other and connecting the leading edge to the trailing edge. The vane further comprises at least one internal cavity between the pressure face and the suction face, wherein air is intended to flow. The vane comprises intersecting transverse partitions, downstream of the cavity, so that air can flow from the cavity in the direction of the trailing edge between the intersecting partitions.

Turbomachine blade, comprising intersecting partitions for circulation of air in the direction of the trailing edge

A method provides a device having a feeder vessel, a building vessel with a bottom and a fabrication plate that is movable in vertical translation, a transfer system suitable for depositing powder from the feeder vessel to the building vessel as a powder layer of constant thickness, and a high energy beam optical system suitable for scanning the surface of the deposited powder layer. A powder is placed in the feeder vessel. A first series of powder layers is deposited on the fabrication plate. The particles of powder are melted or sintered to form a plurality of columns of material that are separated from one another by particles of powder. A second series of layers of powder is deposited on the first series of layers of powder particles to form a single-piece element. A thermal insulation platform is formed between the fabrication plate and said single-piece element.

Method of fabricating a part by selective melting or selective sintering of powder beds by means of a high energy beam

A method of fabricating a metal part by selectively melting a powder, the method including: building up layer by layer on a plate and simultaneously with the part, at least one holder and support element for the part, the element being spaced apart and distinct from the part and being separated therefrom by a gap filled with non-melted powder; after the part has been made completely, removing at least some of the powder remaining in the gap between the part and the element, for example by suction, blowing, or vibration; and separating the part from the plate.

Process for manufacturing a metal part by selectively melting a powder

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Livry sur Seine, France

Olivier Chantoiseau