Method for the powder-based additive manufacturing of a part, notably a lining blade for a tire mould, with an associated reinforcing element

Patent metadata

Field	Value
Publication number	US-10518326-B2
Application number	US-201515329709-A
Country	US
Kind code	B2
Filing date	Jul 24, 2015
Priority date	Jul 28, 2014
Publication date	Dec 31, 2019
Grant date	Dec 31, 2019

Abstract

Process for the additive manufacturing of at least one part by powder sintering or melting using at least one beam of energy. A step of deposition and selective melting of stacked layers of powder manufactures at least one intermediate element comprising the part and at least one local reinforcing element having a split tubular shape that surrounds one of the lateral end faces of the part and that face each of the frontal faces of said part adjacent to said end face, said reinforcing element extending in a direction substantially parallel to the stacking direction of the layers. The part and the local reinforcing element are separated.

First claim

The invention claimed is:

1. A process for the additive manufacturing of at least one part by powder sintering or melting using at least one beam of energy, said part comprising at least two opposite frontal faces and at least two lateral end faces, the process comprising the following steps:
a) manufacture, by deposition and selective melting of stacked layers of powder, of at least one intermediate element comprising the part and at least one local reinforcing element having a split tubular shape that surrounds one of the lateral end faces of the part and that face each of the frontal faces of said part adjacent to said end face, a portion of the part extending through the slit of the local reinforcing element and into said reinforcing element, the other portion of the part protruding outside of the reinforcing element, said reinforcing element extending in a direction substantially parallel to the stacking direction of the layers,
wherein during the manufacturing step, for each fused layer of powder of the part and each fused layer of powder of the local reinforcing element, the deposited powder present between each frontal face of said fused powder layer of the part and the facing end face of said fused powder layer of the reinforcing element is completely or partially fused by heat diffusion and not directly by the beam of energy, and
b) after manufacture, gripping said other portion of the part protruding outside of the reinforcing element separation of the part and of the local reinforcing element by pulling along a direction perpendicular to the stacking direction of the layers.

2. A process according to claim 1 , wherein the fused powder layers of the part and of said local reinforcing element are joined to one another during the manufacturing step.

3. A process according to claim 1 , wherein said local reinforcing element is configured so as to reinforce the part at least in a direction substantially perpendicular to the stacking direction of the layers.

4. A process according to claim 1 , wherein unfused powder fills a space that exists between an inner surface of said local reinforcing element and the part before the separation step.

5. A process according to claim 1 , wherein according to a modelled melting of a layer of powder of the local reinforcing element and of a layer of powder of the part, a gap is provided between each end face of the layer of the reinforcing element and the frontal face of the layer of the part which is facing said end face, said gap being between 0.01 mm and 1 mm.

6. A process according to claim 1 , wherein said local reinforcing element extends over the entire height of the part.

7. A process according to claim 1 , wherein a plurality of intermediate elements is manufactured simultaneously at least as a matrix of columns and rows.

8. A process according to claim 7 , wherein the reinforcing elements of at least one column or of at least one row are produced as one piece.

9. Intermediate element obtained by implementation of the process according to claim 1 .

10. A process according to claim 1 , wherein according to a modelled melting of a layer of powder of the local reinforcing element and of a layer of powder of the part, a gap is provided between each end face of the layer of the reinforcing element and the frontal face of the layer of the part which is facing said end face, said gap being less than or equal to 0.1 mm.

Assignees

• Michelin & Cie
• Michelin Rech Tech

Inventors

• Pays Pierre
• Nigaize Bruno

Classifications

• B29D2030/0613

  Means, e.g. sipes or blade-like elements, for forming narrow recesses in the tyres, e.g. cuts or incisions for winter tyres · CPC title

• B29C64/153

  using layers of powder being selectively joined, e.g. by selective laser sintering or melting · CPC title

• B23K26/342

  Build-up welding · CPC title

• B23K15/0086

  welding for purposes other than joining, e.g. build-up welding · CPC title

• B33Y80/00

  Products made by additive manufacturing · CPC title