METHOD FOR ADDITIVE MANUFACTURING OF THREE-DIMENSIONAL OBJECTS FROM METALLIC GLASSES

Abstract

A method for additive manufacturing of three-dimensional objects from metallic glasses utilizing a process of melting of successive layers of the starting material by a laser beam or an electron beam. The method includes steps such that every material layer is melted twice, using parameters which yield a crystalline melt trace in the first melting, and the successively melted beam paths contact with one another, while in the second melting, parameters yielding an amorphous melt trace are used, and the successively remelted paths or spots do not come in contact with one another, and/or between the scanning of successive paths or spots, an interval not shorter than 10 ms is maintained, the surface power density in the first remelting being lower than in the second remelting.

Claims

1. A method for additive manufacturing of three-dimensional objects from metallic glasses, the method comprising: melting of successive layers of an alloying starting material by a laser beam or an electron beam, wherein every material layer is melted twice, using parameters which yield a crystalline melt trace in the first melting, and the successively melted beam paths come in contact with one another, while in the remelting, parameters yielding an amorphous melt trace are used, and the successively remelted paths or spots do not come in contact with one another, and/or between the scanning of successive paths or spots, an interval not shorter than 10 ms is maintained, the surface power density in the first remelting being lower than in the second remelting.

2. The method according to claim 1, wherein in the amorphous remelting, paths or spots remelted successively are separated by a distance not shorter than 300 m.

3. The method according to claim 1, wherein the first melting is realized with a beam speed of 10-2000 mm/s and a surface power density of 10.sup.4-5.Math.10.sup.5 W/cm.sup.2.

4. The method according to claim 1, wherein the remelting is realized with a beam speed of 200-5000 mm/s and a surface power density above 5.Math.10.sup.5 W/cm.sup.2.

5. The method according to claim 1, wherein the remelting is realized in pulses with a surface power density above 5.Math.10.sup.5 W/cm.sup.2.

6. The method according to claim 1, wherein a layer of the material constituting a cross-section of the manufactured object and a layer of the material surrounding it are melted in the first melting, while in the remelting, parameters yielding an amorphous melt trace are used for the object's cross-section, and for the remaining part of the layer, parameters yielding a crystalline melt trace are used, or this part of the layer is omitted.

7. The method according to claim 6, wherein different melting parameters for the cross-section of the manufactured object and for the remaining part of the layer are used in the first melting.

8. The method according to claim 6, wherein for the part of the material which is not a cross-section of the manufactured object, multiple crystalline melting of each layer is used.

9. The method according to claim 1, wherein the initial material is in a form of a powder, sheet, strip or wire.

10. The method according to claim 1, wherein binary or ternary alloys containing at least one metal and at least one metalloid and/or non-metal are used as the starting material.

11. The method according to claim 10, wherein the at least one metal is iron, tungsten, zinc, nickel, titanium, magnesium, aluminum, yttrium, or calcium.

12. The method according to claim 10, wherein the metalloid and/or non-metal are selected from: silicon, boron, carbon, or phosphorus.

13. A method for additive manufacturing of three-dimensional objects from metallic glasses, the method comprising: providing an alloying starting material in a form of a powder, sheet, strip or wire including binary or ternary alloys containing at least one metal and at least one metalloid and/or non-metal; and melting successive layers of the alloying starting material by a laser beam or an electron beam, wherein every material layer is melted twice, using parameters including a beam speed of 10-2000 mm/s and a surface power density of 10.sup.4-5.Math.10.sup.5 W/cm.sup.2 which yield a crystalline melt trace in the first melting, and the successively melted beam paths come in contact with one another, while in the remelting, parameters yielding an amorphous melt trace are used, and the successively remelted paths or spots are separated by a distance not shorter than 300 m, and/or between the scanning of successive paths or spots, an interval not shorter than 10 ms is maintained, the surface power density in the first remelting being lower than in the second remelting.

14. The method according to claim 13, wherein the remelting is realized with a beam speed of 200-5000 mm/s and a surface power density above 5.Math.10.sup.5 W/cm.sup.2.

15. The method according to claim 13, wherein the remelting is realized in pulses with a surface power density above 5.Math.10.sup.5 W/cm.sup.2.

16. The method according to claim 13, wherein a layer of the material constituting a cross-section of the manufactured object and a layer of the material surrounding it are melted in the first melting, while in the remelting, parameters yielding an amorphous melt trace are used for the object's cross-section, and for the remaining part of the layer, parameters yielding a crystalline melt trace are used, or this part of the layer is omitted.

17. The method according to claim 16, wherein different melting parameters for the cross-section of the manufactured object and for the remaining part of the layer are used in the first melting.

18. The method according to claim 16, wherein for the part of the material which is not a cross-section of the manufactured object, multiple crystalline melting of each layer is used.

19. The method according to claim 13, wherein the at least one metal is iron, tungsten, zinc, nickel, titanium, magnesium, aluminum, yttrium, or calcium and the metalloid and/or non-metal are selected from silicon, boron, carbon, or phosphorus.

20. A method for additive manufacturing of three-dimensional objects from metallic glasses, the method comprising: providing an alloying starting material in a form of a powder, sheet, strip or wire including binary or ternary alloys containing at least one metal and at least one metalloid and/or non-metal, wherein the at least one metal is iron, tungsten, zinc, nickel, titanium, magnesium, aluminum, yttrium, or calcium and the metalloid and/or non-metal are selected from silicon, boron, carbon, or phosphorus; and melting successive layers of the alloying starting material by a laser beam or an electron beam, wherein every material layer is melted twice, using parameters including a beam speed of 10-2000 mm/s and a surface power density of 104-5.Math.105 W/cm2 which yield a crystalline melt trace in the first melting, and the successively melted beam paths come in contact with one another, while in the remelting, parameters yielding an amorphous melt trace are used, and the successively remelted paths or spots are separated by a distance not shorter than 300 m, and/or between the scanning of successive paths or spots, an interval not shorter than 10 ms is maintained, the surface power density in the first remelting being lower than in the second remelting, wherein a layer of the material constituting a cross-section of the manufactured object and a layer of the material surrounding it are melted in the first melting, while in the remelting, parameters yielding an amorphous melt trace are used for the object's cross-section, and for the remaining part of the layer, parameters yielding a crystalline melt trace are used, or this part of the layer is omitted.

Description

DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION

[0023] The method according to the invention envisions two remeltings for each layer. The aim of the first remelting is the densification of the material and a reduction in its porosity, and the aim of the second remelting consists in amorphization of the previously melted material on the cross-section of the manufactured object. Formation of a crystalline structure of the layer as a result of the first melting allows for the elimination of problems connected with obtaining an amorphous structure for numerous starting materials. In order to obtain an amorphous structure, a high beam speed is usually necessary, though increasing the speed leads to defect formation, resulting from incomplete powder melting. The beam power cannot be significantly increased either, as during the key-hole mode melting there occurs an explosive removal of the powder from the processing area. According to the invention, the first crystalline melting eliminates the above limitations, as the entire layer has been previously bonded. As a result, it is possible to execute a deep amorphous remelting of the same layer in the second stage. With a heating rate higher than the critical value, crystallization in the heat-affected zone of the remelting does not occur. This allows for maintaining the continuity of the glassy phase between the layers. Maintaining the distance between the beam paths or spots, or maintaining the time interval during the amorphous remelting limits the influence of the subsequently remelted path on the solidification of the previous one, and as a result, the heat accumulation is limited, which allows for maintaining a high glassy phase content.

[0024] As a result of the method according to the invention, an object in the amorphous form is obtained, possibly surrounded by a crystalline allowance. In the case of manufacturing objects with a complex geometry by additive methods, stress induced in an amorphous object during its production causes the propagation of microcracks and delamination of an object during the manufacturing process, A crystalline allowance around an amorphous object prevents macroscopic cracking, due to the fact that the crystalline phase typically has a higher resistance to cracking than the amorphous phase. The crystalline allowance is removed mechanically or etched chemically, and its porous or scaffold-like form allows for easier removal by penetration with an etching agent. Moreover, in the case of an object with a complex geometry, it is important that the allowance may be removed from all runner extensions or cavities, which would be difficult with a completely solid allowance.

[0025] Application of advanced scanning strategies in known in the art, for example from EP1583625, where a double scanning strategy is used for preliminary heating of a powder, and from EP1419836, where a double scanning strategy is used for reduction of residual stress. Both of these strategies are not suitable for metallic glasses with a low glass-forming ability due to intense crystallization. The strategy applied in EP1583625, used in electron beam melting, causes an increase in the sample temperature, which limits the cooling and heating rates, while the strategy applied in EP1419836 uses parallel paths with double melting, which precludes the vitrification of alloys with a low glass-forming ability. The solution according to the invention also differs from EP2326443 by the scanning order and the applied strategy. In EP2326443 a solution of double scanning for alloys with a high glass-forming ability for subsequent nanocrystalliiation is proposed. However, this solution is unsuitable for an alloy which crystallizes during the first scanning. In the solution according to the invention, the material is first bonded and crystallizes, and only in the second step do densification and amorphization occur due to the separation of the paths and/or spots and remelting with a higher energy density. A change in surface power density in the second scanning ensures a deeper remelting and fusion of the layers.

[0026] Using the method according to the invention, a metallic object containing more than 50% of the amorphous phase and having a relative density higher than 80% is obtained, which may be then subjected to densification by isostatic pressing.

Examples

[0027] The method according to the invention is presented in more detail in the examples. The following examples are included to more clearly demonstrate the overall nature of the invention. These examples are exemplary, not restrictive, of the invention.

Example 1

[0028] An amorphous powder having the following nominal composition: Cu: 40%, Zr: 58%, and Al: 2% by weight was melted selectively on a Realizer SLM-50 apparatus equipped with a 100 W Nd:YAG laser. The layer thickness was 50 m. Every layer was melted twice, at first with a beam speed of 200 mm/s and a surface power density of 8.Math.10.sup.4 W/cm.sup.2, where the laser paths were 50 m wide and realized successively, then the layer was remelted with a surface power density of 10.sup.6 W/cm.sup.2 and a beam speed of 2000 mm/s; the laser paths were 50 m wide, and the successive paths were separated by a distance of 1 mm.

Example 2

[0029] An amorphous powder having the following nominal composition: Mg: 43%, Zn: 53%, and Ca: 4% by weight was remelted selectively on an SLM 280HL apparatus (SLM Solutions) equipped with a 400 W Nd:YAG laser. The layer thickness was 100 m. Every layer of the amorphous core was melted twice, at first with a beam speed of 100 mm/s and a surface power density of 10.sup.4 W/cm.sup.2, where the laser paths were 200 m wide and realized successively, then the layer was melted with a surface power density of 5.Math.10.sup.5 W/cm.sup.2 and a beam speed of 5000 mm/s, the laser paths were 100 m wide, and the successive paths were separated by a distance of 1 mm.

Example 3

[0030] An amorphous powder having the following nominal composition: Fe: 87.160%, Cr: 2.4%, Si: 6.41%, B: 2.51%, and C: 1.60% by weight and a particle size below 53 m was melted selectively on a Realizer SLM-50 apparatus equipped with a 100 W Nd:YAG laser. The layer thickness was 50 m. Every layer of the crystalline allowance was melted once with a beam speed of 100 mm/s and a surface power density of 1.8.Math.10.sup.5 W/cm.sup.2, where the laser paths were 100 m wide and realized successively. The thickness of the crystalline allowance was 2 mm. Every layer of the amorphous core was remelted twice, at first with a beam speed of 100 mm/s and a surface power density of 1.8.Math.10.sup.5 W/cm.sup.2, where the laser paths were 100 m wide and realized successively, then the layer was remelted with a surface power density of 10.sup.6 W/cm.sup.2, where the laser operated in a pulse mode with a pulse duration of 20 s. The amorphous core was covered with a square grid having a periodicity of 40 m, with nodes containing spots irradiated in such a way that two successive remelted spots were separated by a distance not lower than 1 mm. Next, the samples cut off from the build plate were densified by the isostatic pressing method. The crystalline allowance was then removed mechanically, and the object was cleaned in an acid.

Example 4

[0031] A powder having the following nominal composition: Al: 70%, Si: 12%, and Ni: 18% by weight and a particle size below 53 m was obtained by the milling of tapes. It was then melted selectively on an SLM-50 apparatus (Realizer) equipped with a 100 W Nd:YAG laser. The layer thickness was 40 m. The objects had a form of a torus supported on a scaffold-like crystalline allowance. Every layer of the crystalline allowance was melted one time with a beam speed of 250 mm/s and a surface power density of 2.Math.10.sup.5 W/cm.sup.2, where the laser paths were 65 m wide and realized successively. Every layer of the amorphous core was remelted at first with a beam speed of 250 mm/s and a surface power density of 2.Math.10.sup.5 W/cm.sup.2, where the laser paths were 65 m wide and realized successively with a speed of 2000 mm/s, then with a surface power density of 6.Math.10.sup.5 W/cm.sup.2, where the laser paths were 100 m wide, and the two paths being remelted successively were separated by a distance of 300 m. The allowance was removed mechanically.

Example 5

[0032] A mixture of tungsten, silicon and boron pure powders with a mass ratio of 8:1:1 was melted selectively on an SLM 280HL apparatus (SLM Solutions) equipped with a 400 W Nd:YAG laser. The layer thickness was 80 m. The objects had a form of a cylinder prepared directly on a base plate, surrounded with an allowance having a thickness of 500 m. Every layer of the crystalline allowance was remelted one time with a beam speed of 500 mm/s and a surface power density of 8.Math.10.sup.5 W/cm.sup.2, where the laser paths were 50 m wide and realized successively. Every layer of the amorphous core was melted at first with a beam speed of 500 mm/s and a surface power density of 8.Math.10.sup.5 W/cm.sup.2; the laser paths were 70 m wide and realized successively. The layer of the amorphous core was then remelted with a beam speed of 2000 mm/s and a surface power density of 2.Math.10.sup.6 W/cm.sup.2, where the laser paths were 100 m wide, and an interval of 50 ms was used between the successive remelted paths. The allowance was removed by etching.

[0033] Although illustrated and described above with reference to certain specific embodiments and examples, the present invention is nevertheless not intended to be limited to the details shown. Rather, various modifications may be made in the details within the scope and range of equivalents of the claims and without departing from the spirit of the invention. It is expressly intended, for example, that all ranges broadly recited in this document include within their scope all narrower ranges which fall within the broader ranges. It is also expressly intended that the steps of the methods disclosed above are not restricted to any particular order.