POWDERED MATERIAL PREFORM AND PROCESS OF FORMING SAME
20190291185 ยท 2019-09-26
Inventors
Cpc classification
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B22F3/115
PERFORMING OPERATIONS; TRANSPORTING
B33Y70/00
PERFORMING OPERATIONS; TRANSPORTING
F16C7/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B22F1/12
PERFORMING OPERATIONS; TRANSPORTING
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
F16C2208/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B22F3/04
PERFORMING OPERATIONS; TRANSPORTING
B22F2998/10
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B22F3/105
PERFORMING OPERATIONS; TRANSPORTING
F16C2220/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B22F7/062
PERFORMING OPERATIONS; TRANSPORTING
B22F2007/042
PERFORMING OPERATIONS; TRANSPORTING
B22F3/115
PERFORMING OPERATIONS; TRANSPORTING
C22C1/0458
CHEMISTRY; METALLURGY
B22F2301/205
PERFORMING OPERATIONS; TRANSPORTING
C22C1/05
CHEMISTRY; METALLURGY
B22F3/105
PERFORMING OPERATIONS; TRANSPORTING
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
Y02P10/25
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
C22C1/05
CHEMISTRY; METALLURGY
B22F2207/17
PERFORMING OPERATIONS; TRANSPORTING
B22F2302/45
PERFORMING OPERATIONS; TRANSPORTING
B22F3/16
PERFORMING OPERATIONS; TRANSPORTING
B22F1/10
PERFORMING OPERATIONS; TRANSPORTING
B22F5/008
PERFORMING OPERATIONS; TRANSPORTING
B22F7/06
PERFORMING OPERATIONS; TRANSPORTING
B22F7/06
PERFORMING OPERATIONS; TRANSPORTING
B22F3/04
PERFORMING OPERATIONS; TRANSPORTING
B22F1/10
PERFORMING OPERATIONS; TRANSPORTING
B22F7/062
PERFORMING OPERATIONS; TRANSPORTING
F16C2204/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B22F5/008
PERFORMING OPERATIONS; TRANSPORTING
B22F2207/17
PERFORMING OPERATIONS; TRANSPORTING
B22F3/16
PERFORMING OPERATIONS; TRANSPORTING
C22C1/0458
CHEMISTRY; METALLURGY
C22C32/0089
CHEMISTRY; METALLURGY
B22F2998/10
PERFORMING OPERATIONS; TRANSPORTING
B22F5/00
PERFORMING OPERATIONS; TRANSPORTING
B22F2007/042
PERFORMING OPERATIONS; TRANSPORTING
International classification
B22F5/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B22F3/105
PERFORMING OPERATIONS; TRANSPORTING
B22F3/115
PERFORMING OPERATIONS; TRANSPORTING
B33Y70/00
PERFORMING OPERATIONS; TRANSPORTING
B22F1/00
PERFORMING OPERATIONS; TRANSPORTING
B22F3/16
PERFORMING OPERATIONS; TRANSPORTING
B22F3/04
PERFORMING OPERATIONS; TRANSPORTING
F16C7/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A powdered material preform includes a pressed powdered metal or other powdered material, where the preform is processed and sealed so that a skin or shell is formed at the outer surface of the preform (such as via melting an outer layer or surface of the preform or via adding an outer layer around the preform or via a combination thereof), with an inner portion of the preform comprising pressed powdered material. The skinned preform may comprise a shape that is generally similar to that of a final product or part to be formed, or may simply comprise a puck or shape of approximately the same mass of the shape being formed, and the skinned preform is suitable for use in subsequent densification and/or consolidation processes or combinations thereof to form the final, fully processed part.
Claims
1. A preform blank comprising: powdered material that is at least partially compacted to form a shape; an outer surface that encases and seals the powdered material therein; wherein the powdered material comprises one selected from the group consisting of (i) metal, (ii) plastic, and (iii) ceramic; and wherein the outer surface comprises an outer surface established by encasing an outer portion of the powdered material.
2. The preform blank of claim 1, wherein the powdered material comprises metal powder.
3. The preform blank of claim 2, wherein the metal powder comprises at least one selected from the group consisting of titanium, magnesium, aluminum, nickel, and iron.
4. The preform blank of claim 1, wherein the preform blank is suitable for use in one selected from the group consisting of powder metallurgy processes, consolidation processes, and densification processes.
5. The preform blank of claim 1, wherein the powdered material is formed into a blank using one selected from the group consisting of cold compaction, die pressing, and isostatic pressing.
6. The preform blank of claim 1, wherein the powdered material comprises metal powder, and wherein the metal powder comprises at least one metal alloy comprising at least one selected from the group consisting of titanium, magnesium, aluminum, nickel, iron, and graphite.
7. The preform blank of claim 1, wherein the powdered material comprises at least one strengthening material.
8. The preform blank of claim 7, wherein the at least one strengthening material comprises at least one selected from the group consisting of carbon fiber, carbon nanotubes, Kevlar, ceramic, and glass.
9. The preform blank of claim 1, wherein the powdered material comprises at least one strengthening material comprising at least one selected from the group consisting of carbon fiber, carbon nanotubes, Kevlar, ceramic, and glass.
10. The preform blank of claim 1, wherein the preform blank is formed and sealed in a controlled environment.
11. The preform blank of claim 10, wherein the controlled environment comprises a near vacuum.
12. The preform blank of claim 10, wherein the controlled environment comprises an atmosphere composed of one or more gases comprising at least one selected from the group consisting of argon, hydrogen, and nitrogen.
13. The preform blank of claim 1, wherein the outer surface is generated by fusing additional powder around the preform blank using at least one selected from the group consisting of a laser, an electron beam, induction heating, ultrasonic heating, plasma flame, and electric arc.
14. The preform blank of claim 1, wherein the outer surface is generated by fusing the outer layers of powder that make up the preform blank using at least one selected from the group consisting of a laser, an electron beam, induction heating ultrasonic heating, plasma flame, and electric arc.
15. The preform blank of claim 1, wherein the outer surface is generated by a coating or deposition process comprising one selected from the group consisting of a thermal spray, welding, additive manufacturing, 3-D printing, and plating.
16. The preform blank of claim 1, wherein a material of the outer surface comprises at least one selected from the group consisting of a plastic, wax, paint, and metal.
17. The preform blank of claim 1, wherein the outer surface is generated before the preform blank is removed from a preforming die comprising one selected from the group consisting of a cold compaction die, a die pressing die, and an isostatic pressing apparatus.
18. The preform blank of claim 1, wherein the preform blank is further processed using pressure and at least one selected from the group consisting of thermal cycling and magnetic cycling.
19. The preform blank of claim 1, wherein the preform blank is purged of contaminants via a tube that establishes a passageway through the outer surface to the powdered material.
20. The preform blank of claim 1, wherein the outer surface is generated by coalescence of a surface or surfaces just below the outer surface of the powdered material.
21. The preform blank of claim 20, wherein the coalescence is due to an induction field generated at the preform blank.
22. A method of forming a preform blank comprising: providing a powdered material that comprises one selected from the group consisting of (i) metal, (ii) plastic, and (iii) ceramic; pressing the powdered material into a powdered preform shape; and after the powdered material is pressed into the powdered preform shape, establishing an outer skin around the powdered preform shape to encase and seal the powdered preform shape to form a preform blank.
23. The method of claim 22, wherein the powdered material comprises metal powder.
24. The method of claim 23, wherein the metal powder comprises at least one selected from the group consisting of titanium, magnesium, aluminum, nickel, and iron.
25. The method of claim 22, wherein the preform blank is suitable for use in one selected from the group consisting of powder metallurgy processes, consolidation processes, and densification processes.
26. The method of claim 22, wherein pressing the powdered material into a powdered preform shape comprises using one selected from the group consisting of cold compaction, die pressing, and isostatic pressing.
27. The method of claim 22, wherein the powdered material comprises metal powder, and wherein the metal powder comprises at least one selected from the group consisting of metal alloy comprising at least one of titanium, magnesium, aluminum, nickel, iron, and graphite.
28. The method of claim 22, wherein the powdered material comprises at least one strengthening material.
29. The method of claim 28, wherein the at least one strengthening material comprises at least one of carbon fiber, carbon nanotubes, Kevlar, ceramic, and glass.
30. The method of claim 22, wherein the powdered material comprises at least one strengthening material comprising at least one selected from the group consisting of carbon fiber, carbon nanotubes, Kevlar, ceramic, and glass.
31. The method of claim 22, wherein establishing the outer skin around the powdered preform shape comprises establishing the outer skin in a controlled environment.
32. The method of claim 31, wherein the controlled environment comprises a near vacuum.
33. The method of claim 31, wherein the controlled environment comprises an atmosphere composed of one or more gases comprising selected from the group consisting of argon, hydrogen, and nitrogen.
34. The method of claim 22, wherein establishing the outer skin around the powdered preform shape comprises fusing additional powder around the powdered preform shape using at least one selected from the group consisting of a laser, an electron beam, induction heating, ultrasonic heating, plasma flame, and electric arc.
35. The method of claim 22, wherein establishing the outer skin around the powdered preform shape comprises fusing outer layers of powder that make up the powdered preform shape using at least one selected from the group consisting of a laser, an electron beam, induction heating, ultrasonic heating, plasma flame, and electric arc.
36. The method of claim 22, wherein establishing the outer skin around the powdered preform shape comprises coating or depositing the outer skin with one selected from the group consisting of a thermal spray, welding, additive manufacturing, 3-D printing, and plating.
37. The method of claim 22, wherein a material of the outer skin comprises at least one selected from the group consisting of a plastic, wax, paint, and metal.
38. The method of claim 22, wherein the outer skin is established around the powdered preform shape before the powdered preform shape is removed from a preforming die comprising one selected from the group consisting of a cold compaction die, a die pressing die, and an isostatic pressing apparatus.
39. The method of claim 22, further comprising processing the preform blank using pressure and at least one selected from the group consisting of thermal cycling and magnetic cycling.
40. The method of claim 22, further comprising purging the preform blank of contaminants via a tube that establishes a passageway through the outer skin to the powdered material.
41. The method of claim 22, wherein establishing the outer skin comprises coalescing a surface or surfaces just below the outer skin of the powdered material.
42. The method of claim 41, wherein coalescing the surface or surfaces comprises generating an induction field at the preform blank.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0036] Referring now to the drawings and the illustrative embodiments depicted therein, the present invention provides a process of forming a sealed or skinned preform 12 of a powdered material 14, such as a powdered metallic or nonmetallic material, such as titanium, magnesium, steel alloys, aluminum, graphene, ceramics, plastics, or the like (
[0037] The skinned powdered material preform 12 or blank or puck is a sealed, contaminant free, preform used in powdered material consolidation and/or densification processes such as hot isostatic pressing, sintering, thermal cycling, magnetic phase change cycling, a combination of thermal cycling and magnetic phase change cycling or the like. The puck permits commercialization and mass production of powdered metallic or non-metallic components to a scale that is not otherwise achievable. This feat is possible because the sealed or skinned preform or puck is free of gaseous contaminants on the inside and sealed via an outer layer to prevent recontamination. This allows for easy handling as well as enhanced processing for batch or assembly line production styles. In addition, the skinned powdered metallic preform 12 may have a selected material placed inside of the puck, such as a gas (such as nitrogen, argon or the like), a solid (such as graphene or the like), or liquid (such as liquid nitrogen, water or the like). For example, grain growth in the finished product may be a concern, and therefore, nitrogen at a density level between 0 and 5 atmospheres of pressure may be placed inside the sealed puck to alter the grain growth.
[0038] The powder material 14 is premeasured and compacted into a semi-solid using cold compaction, die pressing, or similar operation to produce a powdered blank 10 (see
[0039] After being pressed into the preform shape (such as in a die 11, as shown in
Powder Compaction Step
[0040] The powder compaction step, as shown in
[0041] This is important because, for materials such as titanium, contaminants, such as oxygen, hydrogen, nitrogen, or other contaminants, may react with the powder during the skinning processing step or the densification processing step, which could negatively alter the final chemistry and material properties. On the other hand, certain elements, such as carbon, argon, helium, nitrogen, or the like, may react with the powder during the skinning processing step or the densification processing step and could positively alter the chemistry and material properties. Similarly, the atmosphere in which the puck is produced may have no effect on subsequent processing or part performance, depending on material type.
Puck Sealing Step
[0042] Before leaving the controlled atmosphere, the puck is preferably sealed, as shown in
[0043] Another purpose of the skin 16 is to prevent gaseous or other contaminants from entering the puck. The sealing operation may be performed before the semi-solid puck leaves a controlled atmospheric environment. This ensures that any gas present or absent in the controlled environment cannot penetrate or escape the seal of the puck. The implication is that once the skin 16 is formed around the puck and the puck is fully sealed, the puck can be removed from the controlled atmosphere and put into an uncontrolled atmosphere without the risk of introducing unwanted contaminants to the preformed powder 14. This means the preformed and contaminant free puck can be easily handled in any environment without compromising the integrity of the powder 14 or the final product 18.
[0044] Alternatively, the loose material can be formed or compacted into the preformed blank 10 in a gaseous environment (such as air, nitrogen, argon and/or the like depending on what material is being processed) and then kept in the same gaseous environment or changed to a new gaseous environment, sealed with a skin 16 as described above, and then purged of a process gas or contaminants and then a new process gas can be introduced into the sealed puck for the consolidation and/or densification process step and resealed. This would achieve the same goal as described above but allow for the preform blank to be made in and/or enter into an uncontrolled and/or ambient/atmospheric environment before being sealed.
[0045] Thus, due to the difficulty of the preparation work to prepare powdered titanium (or other metals, non-metals or multi-materials) for a consolidation process, the present invention provides enhanced processing by creating a skinned preform of the powdered material. For example, one of the difficulties of powdered titanium parts is that the powdered titanium has to be consolidated in special environments. By providing a prepackaged, sealed preform or blank or puck, the puck or preform of the present invention can be inserted into any consolidation process, thus saving processing steps and saving time and money, while providing a quality end product.
[0046] The present invention thus provides a process step between making a compressed or formed powdered blank 10 or preform, and the densification of the powdered blank into a near net shaped part. The preformed puck consists of powdered material that is compacted into a shape (a compacted block that can be handled but that may be fragile) that is then sealed (such as by melting its outer surface), which then makes it very durable. The sealed preform 12 thus can be readily used in various processes. For example, the sealed or skinned preforms can be placed into a hopper of an automated system for further processing, be preheated prior to a subsequent densification process, or be pre-densified.
[0047] The compacting and melting of the outer preform surface can be done in a vacuum, in a controlled environment, or in an uncontrolled environment, depending on the compacting and melting (skinning) processes selected, the material to be processed, and quality level needed of the finished component. In addition, it may be desirable to have a controlled environment for the skinning operation, and/or a controlled environment (or a vacuum) for the inside of the skinned puck. For example, for titanium the preferred environment inside the puck would be a near perfect vacuum with almost zero percent oxygen. Different titanium alloys, metals or multi-materials may require different environments.
[0048] The present invention provides a process of forming a powdered material preform 10 (such as powdered titanium, magnesium, steel, aluminum, ceramic, or multi-material powders with or without carbon fiber or carbon nanotubes or other strengthening agents or the like) where the preform is processed and sealed so that a skin 16 or shell is formed at the outer surface of the preform 10. The present invention may also expand the processing and sealing of the preform to include induction as a method of creating the skin or shell, such as shown in
[0049] The proposed induction field would couple into the compacted titanium powder 14 at the surface of the preform 10. By selecting the appropriate induction heating frequency and power level, the outer grains of the preform can be targeted for heating. The heating would be limited to the surface or surfaces just below the exterior of the preform 10.
[0050] The heating is due to an induction field that is generated by an induction coil. The skin 16 can be produced by moving the preform through the induction field, wherein the induction coil remains stationary (see
[0051] Alternatively, the induction process for applying the skin or shell can be accomplished while the preform is in the compaction die, as shown in
[0052] Changes and modifications to the specifically described embodiments may be carried out without departing from the principles of the present invention, which is intended to be limited only by the scope of the appended claims as interpreted according to the principles of patent law including the doctrine of equivalents.