# US 11,897,033 B2 · Process for the additive manufacturing of a three-dimensional metal part

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- Number: US 11,897,033 B2
- Document ID: US11897033B2
- Status: Granted
- Kind: B2
- Application number: 17/048,790
- Filed: 2019-04-17
- Published: 2021-05-20
- Granted: 2024-02-13
- Earliest claimed: 2018-04-19
- Assignees: Compagnie Generale Des Etablissements Michelin
- Applicants: Compagnie Generale Des Etablissements Michelin
- Inventors: Pierre Pays
- Web page: https://patentgrep.com/patent/US11897033B2

## CPC

- B22F 12/49: Scanners
- B22F 3/105: by using electric current {other than for infrared radiant energy}, laser radiation or plasma (B22F3/11 takes precedence){; by ultrasonic bonding (B22F3/115 takes precedence)}
- B22F 5/007: {of moulds}
- B22F 10/28: Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
- B22F 10/366: Scanning parameters, e.g. hatch distance or scanning strategy
- B22F 12/41: characterised by the type, e.g. laser or electron beam
- B33Y 10/00: Processes of additive manufacturing
- B33Y 50/02: for controlling or regulating additive manufacturing processes
- B22F 2207/17: density or porosity gradients
- B22F 2999/00: Aspects linked to processes or compositions used in powder metallurgy
- B29C 33/00: Moulds or cores; Details thereof or accessories therefor
- B29C 64/153: using layers of powder being selectively joined, e.g. by selective laser sintering or melting
- B29C 64/393: for controlling or regulating additive manufacturing processes
- B29D 30/06: Pneumatic tyres or parts thereof {(e.g. produced by casting, moulding, compression moulding, injection moulding, centrifugal casting)}
- B29L 2031/757: {Moulds, cores, dies}
- B33Y 80/00: Products made by additive manufacturing
- Y02P 10/25: Process efficiency
- B22F: WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER (making alloys by powder metallurgy C22C); APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B33Y: ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B29C: SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING (making preforms B29B11/00; making laminated products by combining previously unconnected layers which become one product whose layers will remain together B32B37/00 - B32B41/00)
- B29D: PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE (making granules B29B9/00; making preforms B29B11/00)
- B29L: INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- Y02P: CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS

## Abstract

A process for the additive manufacturing of a three-dimensional metal part consists of successively solidifying successively deposited layers of metal powder by melting with a laser beam (120), and defining in each of these successive layers at least one core region (210) and/or at least one shell region. The melting of said core regions (210) is effected with said laser beam (120) so as to form weld beads (211) that have identical widths (L), are mutually parallel and are juxtaposed or spaced apart or overlap over a distance less than X % of their width, and the melting of said shell regions is effected similarly to form weld beads that have identical widths to one another and to the weld beads of the core, are mutually parallel and that overlap over a distance greater than X % of their width, X being greater than 0 and less than 100.

## Claims

### Claim 1

A process for the additive manufacturing of a three-dimensional metal part having at least one monolithic part, the at least one monolithic part comprising an inner core part surrounded by an outer shell part, the process comprising:
successively solidifying successively deposited layers of metal powder by melting using a laser beam; and
defining in each of the successive layers of metal powder either at least one shell region, which constitutes a portion of the shell part or at least one core region, surrounded by a shell region, the core region constituting a portion of the inner core part,
wherein the melting of the at least one core region is effected by scanning with the laser beam so as to form longitudinal weld beads that have identical widths, are mutually parallel, and that are either juxtaposed or spaced apart from one another by a distance L2 less than X % of a width L of the weld beads, or overlap over a distance L1 less than X % of the width L,
wherein the melting of the at least one shell region is effected by scanning with the laser beam so as to form longitudinal weld beads that have identical widths L and an identical width to the weld beads of the at least one core region, are mutually parallel, and that overlap over a distance L3 greater than X % of the width L,
wherein X is greater than 0 and less than 100,
wherein the density of the inner core part of the manufactured three-dimensional metal part is less than the density of the outer shell part of the manufactured three-dimensional metal part,
wherein at least one core region of a layer of metal powder comprises at least two zones,
wherein, among the at least two zones, the scanning of at least one zone with the laser beam is effected such that displacement vectors of the laser beam have an orientation angle with respect to a trigonometric coordinate system that is different from an orientation angle of displacement vectors of the laser beam in a zone contiguous with the at least one zone,
wherein at least one shell region of a layer of metal powder comprises at least two zones,
wherein, among the at least two zones, the scanning of at least one zone with the laser beam is effected such that displacement vectors of the laser beam have an orientation angle with respect to a trigonometric coordinate system that is different from an orientation angle of displacement vectors of the laser beam in a zone contiguous with the at least one zone,
wherein the at least two zones of the at least one core region are square and disposed in a form of a checkerboard, the checkerboard comprising at least two rows designated as even and odd,
wherein the at least two zones of the at least one shell region are square and disposed in a form of a checkerboard, the checkerboard comprising at least two rows designated as even and odd,
wherein in each core region and each shell region the melting of at least one layer of metal powder is effected by scanning, with the laser beam, the zones of odd rows and of odd columns as first zones at a first orientation angle, the zones of odd rows and of even columns as second zones at a second orientation angle, the zones of even rows and of odd columns as third zones at a third orientation angle, and the zones of even rows and of even columns as fourth zones at a fourth orientation angle, the four orientation angles with respect to a trigonometric coordinate system being different,
wherein the orientation angles of the displacement vectors of the laser beam in the first, second, third and fourth zones, respectively, of the core region of one layer exhibit an angular variation of 35° with the orientation angles of the displacement vectors of the laser beam in the first, second, third and fourth zones, respectively, of the core region of the layer situated thereabove,
wherein the orientation angles of the displacement vectors of the laser beam in the first, second, third and fourth zones, respectively, of the shell region of one layer exhibit an angular variation with the orientation angles of the displacement vectors of the laser beam in the first, second, third and fourth zones, respectively, of the shell region of the layer situated thereabove, and
wherein the annular variation in the core region and the angular variation in the shell region are different.

### Claim 2 (depends on 1)

The process according to claim 1, wherein X is equal to 30.

### Claim 3 (depends on 1)

The process according to claim 1, wherein the melting of the at least one shell region is effected by scanning with the laser beam so as to form weld beads that overlap over the distance L3 greater than 30% and less than or equal to 60% of the width L of the weld beads.

### Claim 4 (depends on 1)

The process according to claim 1, wherein the inner core part and the outer shell part overlap over a width of between 0.01 mm and 0.40 mm.

### Claim 5 (depends on 1)

The process according to claim 1, wherein the inner core part of the metal part comprises n successive superposed layers, and
wherein the square core zones of one layer are offset by 1/q step, q being an integer, laterally, longitudinally, or both laterally and longitudinally, with respect to the square core zones of the layer situated immediately thereabove.

### Claim 6 (depends on 1)

The process according to claim 1, wherein the outer shell part of the metal part comprises n successive superposed layers, and
wherein the square shell zones of one layer are offset by 1/q step, q being an integer, laterally, longitudinally, or both laterally and longitudinally, with respect to the square shell zones of the layer situated immediately thereabove.

### Claim 7 (depends on 1)

The process according to claim 1, wherein the melting of the at least one core region is effected by scanning with the laser beam so as to form adjacent weld beads that are spaced apart from one another by the distance L2 less than 20% of the width L of the weld beads.

### Claim 8 (depends on 1)

The process according to claim 1, wherein the melting of the at least one core region is effected by scanning with the laser beam so as to form weld beads that overlap over the distance L1 less than 20% of the width L of the weld beads.