IP Library Granted Patent US 10,688,562
Granted Patent B2
US 10,688,562 · App. 15/537,235 · Granted Jun 23, 2020

Laser sintering method for manufacturing a tread molding element

Inventors: Etienne Blanchet (Clermont-Ferrand, FR); Supradit Khaoyabut (Clermont-Ferrand, FR)
Assignees: COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN; MICHELIN RECHERCHE ET TECHNIQUE, S.A.
B22F5/007B22F3/1055B29C64/153B29D30/0606B29D30/66B33Y10/00B33Y80/00B22F2003/1057B29D2030/0613B29D2030/0616Y02P10/292Y02P10/295
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Quick Facts
Patent No.
US 10,688,562
App. No.
15/537,235
Granted
Jun 23, 2020
Kind
B2
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 (L 2 ). The fine lamella is sintered in a plurality of portions (p 2 ) at different layers (N), in each layer (N) the laser beam sinters the portion (p 2 ) of the fine lamella in only one passage in the length (L 2 ) of the fine lamella without round-trip passage of the laser beam, 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. 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.

Claims (18)

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.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 8, 2020
From: MICHELIN RECHERCHE ET TECHNIQUE S.A.
To: COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN
Reel/Frame 052863/0624 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 26, 2018
From: BLANCHET, ETIENNE; KHAOYABUT, SUPRADIT
To: COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN; MICHELIN RECHERCHE ET TECHNIQUE, S.A.
Reel/Frame 046470/0401 →