Patent ID: 11897033
Assignee: COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN
Field: Other special machines (Mechanical engineering)
Classification: CPC B  Y | IPC B

Claim 0:
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.