Method for Manufacturing a Component by Means of Layered Construction
20240263339 ยท 2024-08-08
Assignee
Inventors
Cpc classification
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B23K2103/26
PERFORMING OPERATIONS; TRANSPORTING
B22F2203/11
PERFORMING OPERATIONS; TRANSPORTING
C30B13/06
CHEMISTRY; METALLURGY
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
C30B11/003
CHEMISTRY; METALLURGY
B23K26/0006
PERFORMING OPERATIONS; TRANSPORTING
B22F12/44
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B22F10/38
PERFORMING OPERATIONS; TRANSPORTING
B23P6/007
PERFORMING OPERATIONS; TRANSPORTING
C22C1/0458
CHEMISTRY; METALLURGY
B22F10/28
PERFORMING OPERATIONS; TRANSPORTING
B22F2998/10
PERFORMING OPERATIONS; TRANSPORTING
B22F10/25
PERFORMING OPERATIONS; TRANSPORTING
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
B22F2203/11
PERFORMING OPERATIONS; TRANSPORTING
International classification
C30B13/06
CHEMISTRY; METALLURGY
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B22F10/28
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The invention relates to a method for producing a component by means of layered construction, by combining a plurality of crystallites of a metallic material to form a single crystal. The single crystal is formed by thermomechanically activated successive anisotropic plastic deformation. The metallic material is heated during the construction of a new layer, with the result that the metallic material is melted in a linear region. The linear region is moved in order to construct the new layer.
Claims
1. A method for producing a component (1) by means of layered construction, comprising combining a plurality of crystallites of a metallic material to form a single crystal, wherein the single crystal is formed by thermomechanically activated successive anisotropic plastic deformation, wherein the metallic material is heated during the construction of a new layer, with the result that the metallic material is melted in a linear region, wherein mechanical stresses occur during melting and subsequent cooling, in particular solidification, of the metallic material, wherein the plastic deformation of the metallic material is caused by these mechanical stresses, wherein the mechanical stresses have a preferred direction because of the linear design of the melted linear region, whereby the anisotropic plastic deformation results, and wherein the new layer is gradually constructed by being traversed by the melted linear region, wherein the component is constructed layer by layer in a construction direction, wherein the linear region has a length (L) along its extension direction and a width (B) and a depth (D) which are both perpendicular to the extension direction of the linear region, wherein the ratio of length (L) and width (B) is at least 5:1, wherein the ratio of width (B) and depth (D) lies in a range of from 1:2 to 10:1, wherein the linear region is moved in order to construct the new layer, and wherein the linear region is subjected to a lateral movement perpendicular to its extension direction with a lateral speed v.sub.lat while maintaining its extension direction.
2. The method according to claim 1, wherein the ratio of length (L) and width (B) is at least 20:1.
3. The method according to claim 1, wherein the ratio of width (B) and depth (D) lies in a range of from 2:1 to 4:1.
4. The method according to claim 1, wherein the depth (D) of the linear region is in the range from 50 ?m to 1000 ?m.
5. The method according to claim 1, wherein the component is produced layer by layer by at least one of local melting of a powder layer of the metallic material or local application of the metallic material.
6. The method according to claim 1, wherein the metallic material in the linear region is melted by at least one of a laser or an electron beam.
7. The method according to claim 1, wherein the component or an installation space containing the component is additionally heated.
8. The method according to claim 1, wherein at least one of the metallic material, the component or the installation space is heated to a temperature (T) in the range of from 300? ? C. to 1200? C.
9. The method according to claim 1, wherein the layered construction is effected along a construction direction (4) and layers with thicknesses in the range of between 10 ?m and 500 ?m are generated.
10. The method according to claim 1, wherein the metallic material is formed of at least one of a nickel-based alloy, a nickel-titanium alloy or a copper alloy.
11. The method according to claim 1, wherein the lateral speed v.sub.lat is between 0.1 mm/s and 100 mm/s.
12. The method according to claim 11, wherein a crystal orientation of the single crystal is adjusted in a defined manner by adjustment of extension direction and lateral movement of the linear region in successive layers.
13. The method according to claim 1, wherein the extension direction of the linear region in successive layers is the same or is rotated by an angle corresponding to a rotational symmetry of the crystal lattice.
14. The method according to claim 1, wherein the direction of the lateral movement of the linear region in successive layers is the same or is rotated by an angle corresponding to a rotational symmetry of the crystal lattice.
15. The method according to claim 1, wherein the extension direction and the direction of the lateral movement of the linear region in successive layers, or in each case after a particular number of layers, are rotated by an equal angle value.
16. The method according to claim 1, further comprising at least one of the following: varying the extension direction of the linear region during the construction of the new layer, varying the lateral movement of the linear region during the construction of the new layer, varying the extension direction of the linear region in the construction direction, or varying the lateral movement of the linear region in the construction direction.
17. The method according to claim 1, wherein a linear region is melted only in subregions of the component.
18. The method according to claim 1, wherein monocrystalline and polycrystalline regions are produced in the component.
19. The method according to claim 1, wherein a continuous change in the crystal orientation is produced in the component.
20. A component comprising a single crystal with exactly adjusted primary and secondary crystal orientation, produced by a means of layered construction, comprising combining a plurality of crystallites of a metallic material to form a single crystal, wherein the single crystal is formed by thermomechanically activated successive anisotropic plastic deformation, wherein the metallic material is heated during the construction of a new layer, with the result that the metallic material is melted in a linear region, wherein mechanical stresses occur during melting and subsequent cooling, in particular solidification, of the metallic material, wherein the plastic deformation of the metallic material is caused by these mechanical stresses, wherein the mechanical stresses have a preferred direction because of the linear design of the melted linear region, whereby the anisotropic plastic deformation results, and wherein the new layer is gradually constructed by being traversed by the melted linear region, wherein the component is constructed layer by layer in a construction direction, wherein the linear region has a length (L) along its extension direction and a width (B) and a depth (D) which are both perpendicular to the extension direction of the linear region, wherein the ratio of length (L) and width (B) is at least 5:1, wherein the ratio of width (B) and depth (D) lies in a range of from 1:2 to 10:1, wherein the linear region is moved in order to construct the new layer, and wherein the linear region is subjected to a lateral movement perpendicular to its extension direction with a lateral speed v.sub.lat while maintaining its extension direction.
Description
[0091] The invention will now be explained in more detail with reference to embodiment examples. There are shown in
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[0098] The metallic material is melted in the linear region 2 by selective electron beam melting. The linear region 2 has a length L along its extension direction and a width B and a depth D which are each perpendicular to its extension direction. The depth D of the linear region is for example 500 ?m. The linear region 2 thus also penetrates into the ten layers produced directly before the new layer. The width B of the linear region is for example 1.5 mm. The length L of the linear region is for example 15 mm. The linear region 2 is surrounded by a heat-affected zone 3. The metallic material in the heat-affected zone 3 is not melted, more precisely is in part not yet melted, in part no longer melted. In the heat-affected zone 3, a temperature field generated by the electron beam acts in particular on the already solidified metallic material in layers produced directly before the new layer.
[0099] The linear region 2 is moved with a lateral speed v.sub.lat perpendicular to its extension direction. The lateral speed v.sub.lat is for example 5 mm/s.
[0100] A plastic deformation of the metallic material in the course of thermally induced mechanical stresses is caused by the melting and the subsequent solidification of the metallic material. The mechanical stresses are generated in a targeted manner by adjustment of the extension direction, speed and temperature of the linear region. The mechanical stresses exceed the yield point of the metallic material in particular in the linear region 2 and/or in the heat-affected zone 3. The mechanical stresses have a preferred direction because of the linear design of the linear region. The mechanical stress field is thus anisotropic. This anisotropy leads to the generation of a single crystal. The crystal orientation, in particular the primary and secondary crystal orientation, can be precisely adjusted by the mechanical stress field generated in a targeted manner by adjustment of extension direction, speed and temperature of the linear region.
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[0105] Even if the portions in which the component 1 still does not have a monocrystalline state in an initial phase of the production method are nevertheless already called component 1 here, it is self-evident that preferably only the portions after single crystal selection has been effected finally form the component 1. For this, the portions from the initial phase of the production method can be detached from the component 1.
LIST OF REFERENCE NUMBERS
[0106] 1 component [0107] 2 linear region [0108] 3 heat-affected zone [0109] 4 construction direction [0110] L length [0111] B width [0112] D depth [0113] ?.sub.yy mechanical stress in the y direction [0114] ?.sub.yy plastic expansion in the y direction [0115] T temperature [0116] T.sub.B construction temperature