Laser sintering method for manufacturing a tread molding element

Patent metadata

Field	Value
Publication number	US-10688562-B2
Application number	US-201515537235-A
Country	US
Kind code	B2
Filing date	Dec 16, 2015
Priority date	Dec 18, 2014
Publication date	Jun 23, 2020
Grant date	Jun 23, 2020

Abstract

The disclosure relates to a selective laser sintering method of manufacturing a tread molding element, said tread molding element including at least a fine lamella adapted to mold a shallow sipe in a tire tread, the fine lamella having a length (L2). The fine lamella is sintered in a plurality of portions (p2) at different layers (N), in each layer (N) the laser beam sinters the portion (p2) of the fine lamella in only one passage in the length (L2) of the fine lamella without round-trip passage of the laser beam, the direction (D1) of this passage being the same at the different layers (N) for building the different portions (p2) of the fine lamella. The thickness (w) of the fine lamella is smaller than 0.2 mm, and the height (h) of the fine lamella is smaller than or equal to 2 mm.

First claim

The invention claimed is:

1. A selective laser sintering method of manufacturing a tread molding element, said tread molding element comprising:
at least a fine lamella to mold a shallow sipe in a tire tread, the fine lamella having a length (L 2 ), wherein
the fine lamella is sintered in a plurality of portions at different layers (N), in each layer a laser beam (B) sinters the portion (p 2 ) of the fine lamella ( 20 ) in only one passage in the length (L 2 ) of the fine lamella without round-trip passage of the laser beam (B),
the direction (D 1 ) of this passage being the same at the different layers (N) for building the different portions (p 2 ) of the fine lamella, and
the thickness (w) of the fine lamella is smaller than 0.2 mm, and the height (h) of the fine lamella 20 is smaller than or equal to 2 mm.

2. The selective laser sintering method according to claim 1 , wherein the fine lamella has a complex shape in its length (L 2 ), including but not limited to a wavy, sinusoidal or zig-zag shape or a combination thereof.

3. The selective laser sintering method according to claim 1 , wherein the characteristics of the laser beam (B) are the same at the different layers (N) for building the different portions (p 2 ) of the fine lamella ( 20 ).

4. The selective laser sintering method according to claim 1 , wherein the fine lamella has a height (H) exhibiting a complex shape, including but not limited to, a wavy, sinusoidal or zig-zag shape or a combination thereof, in its height.

5. The selective laser sintering method according to a claim 1 , wherein the tread molding element comprises a least two adjacent fine lamellas, in each layer (N) the laser beam (B) sinters portions (p 2 ) of the two fine lamellas in one round-trip passage of the laser beam (B).

6. A tread molding element, comprising:
a plurality of ribs;
and a plurality of fine lamellas, wherein said tread molding element is manufactured by the selective laser sintering method according to claim 1 .

7. At least one programmable controller for executing the selective laser sintering method according to claim 1 .

8. The selective laser sintering method according to claim 1 , wherein the tread molding element comprises a plurality of fine lamellas and a least one rib.

9. The selective laser sintering method according to claim 8 , wherein the rib is sintered in a plurality of portions (p 1 ) at the different layers (N), in each layer (N) the laser beam (B) sinters the portion (p 1 ) of the rib in a plurality round-trip passages of the laser beam.

10. The selective laser sintering method according to claim 8 , wherein for a same layer (N), the sintering of the fine lamella is along a first path (Pth 1 ) and the sintering of the rib is along a plurality of parallel second paths (Pth 2 ) different from the first path (Pth 1 ).

11. The selective laser sintering method according to claim 8 , wherein the laser sintering method uses a laser and further comprises the modification of the characteristics of the laser beam (B) according to the ribs or to the fine lamellas to be sintered.

12. The selective laser sintering method according to claim 10 , wherein for two consecutive layers, the characteristics of the second paths (Pth 2 ) for sintering two portions (p 1 ) of the rib are different.

Assignees

• Michelin & Cie
• Michelin Rech Tech

Inventors

• Blanchet Etienne
• Khaoyabut Supradit

Classifications

• B22F10/366

  Scanning parameters, e.g. hatch distance or scanning strategy · CPC title

• B22F10/28

  Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title

• B22F10/00 Primary

  Additive manufacturing of workpieces or articles from metallic powder (apparatus or devices therefor B22F12/00) · CPC title

• Y02P10/25

  Process efficiency · CPC title

• B29D2030/0616

  Surface structure of the mould, e.g. roughness, arrangement of slits, grooves or channels · CPC title