US20160158843A1 - Method of achieving full density binder jet printed metallic articles - Google Patents
Method of achieving full density binder jet printed metallic articles Download PDFInfo
- Publication number
- US20160158843A1 US20160158843A1 US14/960,761 US201514960761A US2016158843A1 US 20160158843 A1 US20160158843 A1 US 20160158843A1 US 201514960761 A US201514960761 A US 201514960761A US 2016158843 A1 US2016158843 A1 US 2016158843A1
- Authority
- US
- United States
- Prior art keywords
- hip
- container
- printed article
- binder
- vacuum
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000000034 method Methods 0.000 title claims abstract description 43
- 239000011230 binding agent Substances 0.000 title claims abstract description 27
- 239000000843 powder Substances 0.000 claims abstract description 56
- 238000007639 printing Methods 0.000 claims abstract description 11
- 230000006641 stabilisation Effects 0.000 claims abstract description 11
- 238000011105 stabilization Methods 0.000 claims abstract description 11
- 238000000354 decomposition reaction Methods 0.000 claims abstract description 5
- 238000010438 heat treatment Methods 0.000 claims abstract description 4
- 239000007789 gas Substances 0.000 claims description 24
- 238000005056 compaction Methods 0.000 claims description 14
- 230000000087 stabilizing effect Effects 0.000 claims description 13
- 238000005245 sintering Methods 0.000 claims description 11
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 239000002184 metal Substances 0.000 claims description 8
- 230000009467 reduction Effects 0.000 claims description 5
- 239000007787 solid Substances 0.000 claims description 4
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 2
- 230000005540 biological transmission Effects 0.000 claims description 2
- 238000009694 cold isostatic pressing Methods 0.000 claims description 2
- 230000002411 adverse Effects 0.000 claims 3
- 238000007789 sealing Methods 0.000 claims 3
- 239000001257 hydrogen Substances 0.000 claims 1
- 229910052739 hydrogen Inorganic materials 0.000 claims 1
- 230000008569 process Effects 0.000 description 15
- 238000004519 manufacturing process Methods 0.000 description 8
- 239000000463 material Substances 0.000 description 8
- 238000012545 processing Methods 0.000 description 6
- 229910000601 superalloy Inorganic materials 0.000 description 6
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 5
- 239000000654 additive Substances 0.000 description 5
- 230000000996 additive effect Effects 0.000 description 5
- 230000004927 fusion Effects 0.000 description 5
- 239000011521 glass Substances 0.000 description 5
- 239000010936 titanium Substances 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 229910001069 Ti alloy Inorganic materials 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 239000000155 melt Substances 0.000 description 4
- 230000004048 modification Effects 0.000 description 4
- 238000012986 modification Methods 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 239000004576 sand Substances 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 3
- 238000012856 packing Methods 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 238000003466 welding Methods 0.000 description 3
- 229910052845 zircon Inorganic materials 0.000 description 3
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- 239000006227 byproduct Substances 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000007596 consolidation process Methods 0.000 description 2
- 239000012611 container material Substances 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 230000033001 locomotion Effects 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000007500 overflow downdraw method Methods 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 239000002002 slurry Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000000280 densification Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000010419 fine particle Substances 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 238000007641 inkjet printing Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 239000012778 molding material Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 229920002379 silicone rubber Polymers 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 238000006557 surface reaction Methods 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- RUDFQVOCFDJEEF-UHFFFAOYSA-N yttrium(III) oxide Inorganic materials [O-2].[O-2].[O-2].[Y+3].[Y+3] RUDFQVOCFDJEEF-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/12—Both compacting and sintering
- B22F3/14—Both compacting and sintering simultaneously
- B22F3/15—Hot isostatic pressing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/10—Formation of a green body
- B22F10/14—Formation of a green body by jetting of binder onto a bed of metal powder
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/60—Treatment of workpieces or articles after build-up
- B22F10/66—Treatment of workpieces or articles after build-up by mechanical means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/12—Both compacting and sintering
- B22F3/16—Both compacting and sintering in successive or repeated steps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2201/00—Treatment under specific atmosphere
- B22F2201/01—Reducing atmosphere
- B22F2201/013—Hydrogen
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2201/00—Treatment under specific atmosphere
- B22F2201/20—Use of vacuum
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
- B22F2998/10—Processes characterised by the sequence of their steps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2999/00—Aspects linked to processes or compositions used in powder metallurgy
-
- Y—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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
Definitions
- thermal operations may include: binder removal, oxide reduction for iron, nickel, and cobalt base superalloys, light sintering for shape stability during transport to the HIP location and the HIP processing conditions.
- a vacuum is maintained in the HIP container from before binder removal to HIP thus maintaining a compressive force on the powder assembly to assure shape retention of the printed article(s).
- This improved process is also effective independent of powder size, thus significantly reducing product cost by enabling the use of lower cost powder.
- the container can be cylindrical, rectangular, or other convenient shape, sized and shaped to hold one or more articles.
- the container material is selected so that it is elastic at HIP conditions, tough enough to withstand HIP compaction and exhibits minimal reaction with the stabilizing fill powder at HIP conditions.
- HIP container materials include mild steel, stainless steel, and titanium.
- the HIP container is compacted under heat and pressure to remove all porosity in the articles.
- the HIP conditions are selected based on the alloy of the article(s), and are limited to those conditions that would not modify the microstructure in an undesirable way.
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Powder Metallurgy (AREA)
Abstract
Description
- This application claims the priority of Provisional Patent Application No. 62/088,009 filed on Dec. 5, 2014 and entitled ACHIEVING FULL DENSITY BINDER JET PRINTED METALLIC ARTICLES.
- 1. Field of the Invention
- The present invention relates to binder-jet printing and, more particularly, to the use of binder-jet printing and hot isostatic press (HIP) processing in the preparation of printed metallic articles.
- 2. Description of the Background Art
- Additive manufacturing has been demonstrated to be highly effective for rapid prototyping and small lot production for plastic articles. More recently, the application of additive manufacturing to metallic materials has been growing, first in medical, dental and specialty consumer products, and now developing in aerospace applications.
- The benefits of direct metal additive manufacturing are best realized in applications involving: high material loss during processing involving high value materials, complex geometries requiring high cost material removal processes or assembly from many fabricated sub-parts, or high tooling expense amortized over short production runs. In these situations, the reduction in expensive material buy-to-fly ratio, specialty machining costs, part number reduction, or tooling overhead cost make direct metal additive manufacturing an attractive alternative.
- Direct metal additive approaches for digital metallic part formation include a variety of methods based either on wire form or powder form feed stock. Wire form is generally applied to larger articles by direct fusion of the wire to build up material much like welding. Powder may be used for smaller articles bye-beam or laser direct fusion or binder-jet printed articles that are subsequently sintered to full density in a secondary high temperature operation. For many alloys and applications these processes are effective.
- Some specialty alloys such as titanium or superalloys experience undesirable microstructural changes when processed using e-beam or laser direct melt fusion or the high temperature sintering near the melt temperature used to densify binder-jet printed articles. High temperatures close to the melt temperature are needed for sintering most metals including titanium and superalloys to near (>90%) full density.
- The above methods have restrictions on powder size that significantly impact cost. The direct melt fusion methods perform better with smaller particle sizes to achieve optimal densification, but the Binder-jet print/high temperature sintering method requires very fine powder size to achieve full density. Since spherical powder is the most desirable for these processes and spherical powder cost is greatest for fine particle sizes, the need for fine powder size in the binder-jet process adds significantly to cost.
- Direct melt fusion methods, whether based on wire or powder, create a high temperature differential in the part as it is being built. That temperature difference causes thermal expansion residual stresses to accumulate in the article. This limits the amount of material that can be deposited and the size of the article that can be built without experiencing residual stress cracking. Depending on the article size and thickness, intermediate stress relief operations have to be performed to relieve the stresses before more material can be deposited. This adds cost and time to the process.
- Binder-jet printing is an ambient temperature process that mimics ink jet printing. A powder bed of the desired alloy powder is ‘printed’ with a binder pattern layer-by-layer to form a powder assembly held together by binder. After printing, the powder bed is baked at moderate temperatures to cure the binder and give the articles sufficient strength to be handled. After curing, the article(s) can be removed from the powder bed for further processing. Binder-jet printing resolves the residual stress buildup encountered with fusion melt processes since it is an ambient temperature process. This enables complete builds of large article(s) without distortion or cracking.
- After creation of the green binder-jet printed form, further processing is performed to remove the binder and sinter the article(s) to near full density at high temperature. This process can create a sintered article, however, the sintering temperatures are typically close to the melt temperature, above the solids but below the liquids, to achieve near full density creating undesirable microstructural modifications and in some cases requiring extremely long sintering times.
- Combining binder-jet printed and cured article(s) with near net shape hot isostatic press (HIP) processing solves both problems encountered with fusion melt processes as well as the baseline binderjet process of high temperature sintering. In this improved process, a binder-jet printed and cured article is packed in a HIP container with shape stabilizing powder media. This media can be non deforming such as Zircon sand or deforming media such as steel or glass powder depending on the desired compaction dynamics. All thermal operations are conducted at temperatures below which detrimental microstructural modification will occur. Typically this is below the beta transus for titanium and titanium alloys, which is significantly below the melt point. These thermal operations may include: binder removal, oxide reduction for iron, nickel, and cobalt base superalloys, light sintering for shape stability during transport to the HIP location and the HIP processing conditions. In the preferred example, a vacuum is maintained in the HIP container from before binder removal to HIP thus maintaining a compressive force on the powder assembly to assure shape retention of the printed article(s). In this way, full density titanium and superalloy articles can be processed while avoiding the two primary production problems. This improved process is also effective independent of powder size, thus significantly reducing product cost by enabling the use of lower cost powder.
-
FIG. 1 is a chart showing the sequence of steps in the method of a first embodiment of the present invention; -
FIG. 2 is a chart showing the sequence of steps in the method of a second embodiment of the present invention; and -
FIG. 3 is a chart showing the sequence of steps in the method of a third embodiment of the present invention. - Referring to
FIG. 1 , the description of the method steps is as follows: - The first operation is to produce a metallic 3-D printed article using a binder-jet printing method. The result is a near net shaped article with a solid metal fraction between 40 and 80 percent held together with a removable polymeric binder. Printing machines of this type are primarily produced by ExOne and Voxeljet.
- This operation establishes a hot isostatic press (HIP) container with the green as-printed article(s) and surrounding stabilizing powder fill.
- Container—The container can be cylindrical, rectangular, or other convenient shape, sized and shaped to hold one or more articles. The container material is selected so that it is elastic at HIP conditions, tough enough to withstand HIP compaction and exhibits minimal reaction with the stabilizing fill powder at HIP conditions. Examples of HIP container materials include mild steel, stainless steel, and titanium.
- Any joints included in the container during fabrication should be leak proof under HIP conditions by a joining method such as tungsten inert gas (TIG) welding. The HIP container is first fabricated with an open top to enable placement of the article(s) and stabilizing powder packing around the article(s).
- Stabilizing Powder—The stabilizing powder fill acts to hold the powder that makes up the article(s) in position after the binder is removed until the compaction operation has been completed. It also acts as the force transmission medium during compaction to translate the HIP forces to achieve compaction of the article(s). The powder might be non-deforming at HIP conditions such as Zircon sand, or deforming at HIP conditions such as steel or glass powder. Non-deforming stabilization powder might be used when the article(s) are simple shapes in which the non-deforming stabilization powder would not inhibit the desired compaction motion of the article(s). Deforming stabilization powder might be used when the geometry of the article(s) is more complex with pockets or shapes that require the stabilization powder to compact along with the article(s) to achieve the desired final shape. It is necessary that the stabilizing powder be removable by some mechanism after compaction without damaging the article(s) themselves. It is desirable that the stabilizing powder have minimal reaction with the article(s) so as to not create an unwanted surface reaction layer that can't be removed.
- Packing Article(s)—The article(s) are placed in the container and packed in stabilizing powder such that the entire container is filled with no gaps. A vibrating action may be applied to enhance the packing of the stabilizing powder around the article(s). In some cases the article(s) may first be coated with a high temperature fine ceramic slurry such as alumina, zirconia or yttria. This slurry would have the effect of improving the surface quality of the printed part after HIP consolidation and, if a deforming glass powder is used it would prevent infiltration of the glass into the article surface.
- A top or closure is placed on the container and sealed to it by means that would create a leak proof joint, for example TIG welding. The closed container includes one or more gas flow tubes that enable the application of vacuum to the inside of the container and the introduction of beneficial gases. In some cases it may be desirable to initially process the packed container without a lid in a vacuum furnace.
- A vacuum is applied to the container either as an enclosed container with gas tubes or in a vacuum furnace with an open top. The application of vacuum removes atmospheric gases that could interfere with subsequent operations such as binder removal or sintering. The introduction of an inert sweep gas such as argon may be useful to enhance the kinetics of atmospheric gas removal and subsequent binder by product removal. The binder used to bond powder particles together in the green as-printed article(s) is removed by heating the container to decompose the binder and drawing off the decomposition by-products with the vacuum system.
- After binder removal, in the case of iron, nickel and cobalt alloys, the sweep gas may be mixed with or replaced by hydrogen gas to reduce any oxide on the surface to the powder making up the article(s). This can be achieved by further increasing the container temperature above that of binder removal. This operation is useful for reducing oxides in superalloy articles based on water atomized powder. Water atomized superalloy powder typically has an oxide rich surface on the powder particles.
- Further stabilization of the powder making up the article(s) is achieved by partially sintering the article(s) to reduce the risk of movement during handling and shipping the HIP containers to the HIP unit. This is achieved by further raising the temperature above that of binder removal and oxide reduction and holding at that temperature for a sufficient time. The goal is to limit the sintering temperature such that the microstructure of the powder metal making up the article(s) is not be modified in an undesirable way.
- If the container has been processed without a lid, a lid would be applied at this time as described in
Operation 4. One or more gas tubes are part of the assembly either on the lid or the container body to enable application of vacuum to the interior of the container. - A vacuum is applied to the container by means of the gas tube(s) to remove all process gases and establish a clean vacuum inside the container. This can be performed while the container is hot and the container is allowed to cool under vacuum. Once cooled, the gas tube(s) are crimp sealed and cut to establish a hermetically sealed container with vacuum pressure inside. The cut tube(s) may be further TIG sealed to assure stability during the HIP compaction.
- The HIP container is compacted under heat and pressure to remove all porosity in the articles. The HIP conditions are selected based on the alloy of the article(s), and are limited to those conditions that would not modify the microstructure in an undesirable way.
- After the HIP compaction, the article(s) is removed from the container by first cutting the container open and subsequent removal of the stabilizing medium. In the case of a non-compacting material such as Zircon sand, the sand can be removed by light mechanical work. In the case of compaction media such as glass powder, the media can be removed by grit blasting. In the case of compaction media such as steel powder, the media can be removed by acid milling.
- After removal of the stabilizing media, the article(s) is finished to final form. This could include minor machining, polishing or other surface finishing operations.
- The method of
FIG. 2 is similar to the method ofFIG. 1 and includesOperation 2 as follows: - This operation may be useful if the as-printed article is particularly low in solid metal fraction, or if a higher precision is required on consolidation. The cold isostatic pressing operation consists of encapsulating the as-printed articles(s) in a flexible molding material such as silicon rubber and subjecting them to a non-heated compression cycle in a high pressure gas chamber. Pressures up to 30,000 psi may be used. This operation will debulk the as-printed green form to assure particle-to particle contact throughout the article(s) that may not have been achieved in the printing operation.
- In the method of
FIG. 3 , instead of applying a lid to the HIP container with one or more gas tubes attached in accordance withOperation 4 of the method ofFIG. 1 , the packed HIP container is processed without a lid in accordance withOperation 5. Thereafter, a lid is applied to the HIP container with one or more gas tubes attached in accordance withOperation 9 of the method ofFIG. 3 and as described inOperation 4 of the method ofFIG. 1 to enable application of vacuum to the interior of the container. The remaining Operations 10-13 are the same as the methods ofFIGS. 1 and 2 . - While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiments, it is to be understood that the invention is not to be limited to the disclosed embodiments, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/960,761 US20160158843A1 (en) | 2014-12-05 | 2015-12-07 | Method of achieving full density binder jet printed metallic articles |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201462088009P | 2014-12-05 | 2014-12-05 | |
US14/960,761 US20160158843A1 (en) | 2014-12-05 | 2015-12-07 | Method of achieving full density binder jet printed metallic articles |
Publications (1)
Publication Number | Publication Date |
---|---|
US20160158843A1 true US20160158843A1 (en) | 2016-06-09 |
Family
ID=56093424
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US14/960,761 Abandoned US20160158843A1 (en) | 2014-12-05 | 2015-12-07 | Method of achieving full density binder jet printed metallic articles |
Country Status (1)
Country | Link |
---|---|
US (1) | US20160158843A1 (en) |
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT201600116950A1 (en) * | 2016-11-18 | 2018-05-18 | Nuovo Pignone Tecnologie Srl | Method for repairing parts of turbomachines by hybrid isostatic hot pressing procedure |
CN108220643A (en) * | 2018-01-29 | 2018-06-29 | 华中科技大学 | A kind of preparation method of tungsten particle enhancing metallic glass composite |
US20180311728A1 (en) * | 2017-04-28 | 2018-11-01 | General Electric Company | Method of making a pre-sintered preform |
CN110494236A (en) * | 2017-03-20 | 2019-11-22 | 斯特拉塔西斯公司 | Use the method and system of the material increasing material manufacturing of powder |
US20200055117A1 (en) * | 2018-08-20 | 2020-02-20 | Honeywell International Inc. | System and method for forming part from rapidly manufactured article |
EP3551363A4 (en) * | 2016-12-09 | 2020-04-22 | H.C. Starck Inc. | Fabrication of metallic parts by additive manufacturing and tungsten heavy metal alloy powders therefor |
DE102018219191A1 (en) * | 2018-11-09 | 2020-05-28 | Volkswagen Aktiengesellschaft | Method for producing a composite material component from at least two component components and composite material component from at least two component components |
WO2020122992A1 (en) * | 2018-12-12 | 2020-06-18 | Arconic Inc. | Methods for producing metallic parts |
CN112670879A (en) * | 2020-12-28 | 2021-04-16 | 国网河南省电力公司检修公司 | SF6 gas leakage stoppage process for high-voltage combined electrical apparatus |
US11167375B2 (en) | 2018-08-10 | 2021-11-09 | The Research Foundation For The State University Of New York | Additive manufacturing processes and additively manufactured products |
CN113909490A (en) * | 2021-09-10 | 2022-01-11 | 华中科技大学 | Metal part and near-net forming method thereof |
US20220055103A1 (en) * | 2020-08-24 | 2022-02-24 | Kennametal Inc. | Method for fabricating a three-dimensional metal part using a conformable fugitive material |
WO2022088707A1 (en) * | 2020-10-30 | 2022-05-05 | 嘉思特华剑医疗器材(天津)有限公司 | Oxide layer-containing zirconium-niobium alloy partitioned bone trabecula femoral condyle prosthesis and preparation method |
US11389867B2 (en) | 2017-02-24 | 2022-07-19 | Hewlett-Packard Development Company, L.P. | Three-dimensional (3D) printing |
CN114833340A (en) * | 2022-05-10 | 2022-08-02 | 安泰科技股份有限公司 | Preparation method of Damascus steel |
US11577316B2 (en) | 2017-02-24 | 2023-02-14 | Hewlett-Packard Development Company, L.P. | Three-dimensional printing |
US11673330B2 (en) | 2017-04-28 | 2023-06-13 | Hewlett-Packard Development Company, L.P. | Metallic build material granules |
US11691196B2 (en) | 2016-04-11 | 2023-07-04 | Stratasys Ltd. | Method and apparatus for additive manufacturing with powder material |
JP7316434B1 (en) | 2022-12-12 | 2023-07-27 | 株式会社パシフィックソーワ | Manufacturing method of sintered body |
US11931806B2 (en) | 2019-01-29 | 2024-03-19 | Hewlett-Packard Development Company, L.P. | Powder based 3D printing |
EP4081388A4 (en) * | 2019-12-17 | 2024-03-27 | Kennametal Inc. | Additive manufacturing techniques and applications thereof |
WO2024092114A1 (en) * | 2022-10-28 | 2024-05-02 | Grid Logic Incorporated | Additive manufacturing hot-isostatic press process for manufacturing a part |
-
2015
- 2015-12-07 US US14/960,761 patent/US20160158843A1/en not_active Abandoned
Cited By (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11980941B2 (en) | 2016-04-11 | 2024-05-14 | Stratasys Ltd. | Method and apparatus for additive manufacturing with powder material |
US11691196B2 (en) | 2016-04-11 | 2023-07-04 | Stratasys Ltd. | Method and apparatus for additive manufacturing with powder material |
IT201600116950A1 (en) * | 2016-11-18 | 2018-05-18 | Nuovo Pignone Tecnologie Srl | Method for repairing parts of turbomachines by hybrid isostatic hot pressing procedure |
EP3323535A1 (en) * | 2016-11-18 | 2018-05-23 | Nuovo Pignone Tecnologie SrL | Method for repairing defects on hot parts of turbomachines through hybrid hot isostatic pressing (hip) process |
CN108070709A (en) * | 2016-11-18 | 2018-05-25 | 诺沃皮尼奥内技术股份有限公司 | Method by mixing the defects of hot isostatic pressing (HIP) process is come on the thermal part of restoring portion of turbine |
KR20180056387A (en) * | 2016-11-18 | 2018-05-28 | 누보 피그노네 테크놀로지 에스알엘 | Method for repairing defects on hot parts of turbomachines through hybrid hot isostatic pressing (hip) process |
KR102371872B1 (en) * | 2016-11-18 | 2022-03-08 | 누보 피그노네 테크놀로지 에스알엘 | Method for repairing defects on hot parts of turbomachines through hybrid hot isostatic pressing (hip) process |
US10760139B2 (en) | 2016-11-18 | 2020-09-01 | Nuovo Pignone Tecnologie S.r.l. | Method for repairing defects on hot parts of turbomachines through hybrid hot isostatic pressing (HIP) process |
EP3551363A4 (en) * | 2016-12-09 | 2020-04-22 | H.C. Starck Inc. | Fabrication of metallic parts by additive manufacturing and tungsten heavy metal alloy powders therefor |
IL266951B2 (en) * | 2016-12-09 | 2024-05-01 | Starck H C Inc | Fabrication of metallic parts by additive manufacturing and tungsten heavy metal alloy powders therefor |
IL266951B1 (en) * | 2016-12-09 | 2024-01-01 | Starck H C Inc | Fabrication of metallic parts by additive manufacturing and tungsten heavy metal alloy powders therefor |
US11511338B2 (en) | 2017-02-24 | 2022-11-29 | Hewlett-Packard Development Company, L.P. | Three-dimensional printing |
US11577316B2 (en) | 2017-02-24 | 2023-02-14 | Hewlett-Packard Development Company, L.P. | Three-dimensional printing |
US11389867B2 (en) | 2017-02-24 | 2022-07-19 | Hewlett-Packard Development Company, L.P. | Three-dimensional (3D) printing |
US11583920B2 (en) | 2017-02-24 | 2023-02-21 | Hewlett-Packard Development Company, L.P. | Three-dimensional printing |
CN110494236A (en) * | 2017-03-20 | 2019-11-22 | 斯特拉塔西斯公司 | Use the method and system of the material increasing material manufacturing of powder |
US11400516B2 (en) | 2017-03-20 | 2022-08-02 | Stratasys Ltd. | Method and system for additive manufacturing with powder material |
EP3600723B1 (en) * | 2017-03-20 | 2023-03-15 | Stratasys Ltd. | Method for additive manufacturing with powder material |
US11123796B2 (en) * | 2017-04-28 | 2021-09-21 | General Electric Company | Method of making a pre-sintered preform |
US11673330B2 (en) | 2017-04-28 | 2023-06-13 | Hewlett-Packard Development Company, L.P. | Metallic build material granules |
US20180311728A1 (en) * | 2017-04-28 | 2018-11-01 | General Electric Company | Method of making a pre-sintered preform |
US11000896B2 (en) * | 2018-01-29 | 2021-05-11 | Huazhong University Of Science And Technology | Preparation method of tungsten particle reinforced amorphous matrix composites |
CN108220643A (en) * | 2018-01-29 | 2018-06-29 | 华中科技大学 | A kind of preparation method of tungsten particle enhancing metallic glass composite |
US11167375B2 (en) | 2018-08-10 | 2021-11-09 | The Research Foundation For The State University Of New York | Additive manufacturing processes and additively manufactured products |
US12122120B2 (en) | 2018-08-10 | 2024-10-22 | The Research Foundation For The State University Of New York | Additive manufacturing processes and additively manufactured products |
US11426818B2 (en) | 2018-08-10 | 2022-08-30 | The Research Foundation for the State University | Additive manufacturing processes and additively manufactured products |
US11229952B2 (en) * | 2018-08-20 | 2022-01-25 | Honeywell International Inc. | System and method for forming part from rapidly manufactured article |
US20200055117A1 (en) * | 2018-08-20 | 2020-02-20 | Honeywell International Inc. | System and method for forming part from rapidly manufactured article |
DE102018219191A1 (en) * | 2018-11-09 | 2020-05-28 | Volkswagen Aktiengesellschaft | Method for producing a composite material component from at least two component components and composite material component from at least two component components |
WO2020122992A1 (en) * | 2018-12-12 | 2020-06-18 | Arconic Inc. | Methods for producing metallic parts |
US11931806B2 (en) | 2019-01-29 | 2024-03-19 | Hewlett-Packard Development Company, L.P. | Powder based 3D printing |
EP4081388A4 (en) * | 2019-12-17 | 2024-03-27 | Kennametal Inc. | Additive manufacturing techniques and applications thereof |
US20220055103A1 (en) * | 2020-08-24 | 2022-02-24 | Kennametal Inc. | Method for fabricating a three-dimensional metal part using a conformable fugitive material |
US12005504B2 (en) * | 2020-08-24 | 2024-06-11 | Kennametal Inc. | Method for fabricating a three-dimensional metal part using a conformable fugitive material |
WO2022088707A1 (en) * | 2020-10-30 | 2022-05-05 | 嘉思特华剑医疗器材(天津)有限公司 | Oxide layer-containing zirconium-niobium alloy partitioned bone trabecula femoral condyle prosthesis and preparation method |
CN112670879A (en) * | 2020-12-28 | 2021-04-16 | 国网河南省电力公司检修公司 | SF6 gas leakage stoppage process for high-voltage combined electrical apparatus |
CN113909490A (en) * | 2021-09-10 | 2022-01-11 | 华中科技大学 | Metal part and near-net forming method thereof |
CN114833340A (en) * | 2022-05-10 | 2022-08-02 | 安泰科技股份有限公司 | Preparation method of Damascus steel |
WO2024092114A1 (en) * | 2022-10-28 | 2024-05-02 | Grid Logic Incorporated | Additive manufacturing hot-isostatic press process for manufacturing a part |
JP7316434B1 (en) | 2022-12-12 | 2023-07-27 | 株式会社パシフィックソーワ | Manufacturing method of sintered body |
JP2024083853A (en) * | 2022-12-12 | 2024-06-24 | 株式会社パシフィックソーワ | Sintered body production method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US20160158843A1 (en) | Method of achieving full density binder jet printed metallic articles | |
US11426792B2 (en) | Method for manufacturing objects using powder products | |
KR102297842B1 (en) | A method of making cermet or cemented carbide powder | |
US6042780A (en) | Method for manufacturing high performance components | |
AU2003245820B2 (en) | Method for producing highly porous metallic moulded bodies close to the desired final contours | |
US20130039799A1 (en) | Method of Making Near-Net Shapes From Powdered Metals | |
GB2062685A (en) | Hot pressing powder | |
CN105555435B (en) | The manufacturing process of HIP containers | |
US11926091B2 (en) | In situ partially degradable separation interface for fabrication of complex near net shape objects by pressure assisted sintering | |
JP5777306B2 (en) | Apparatus and method for hot isostatic pressure container | |
US20220032370A1 (en) | Method for manufacturing a part of complex shape by pressure sintering starting from a preform | |
CN104628393A (en) | Preparation method of high-performance ceramic | |
WO2016030654A1 (en) | A mould for use in a hot isostatic press | |
EP2340905B1 (en) | A method of manufacturing a component | |
US20040146424A1 (en) | Production of component parts by metal injection moulding (mim) | |
CN107671294A (en) | Make high temperature insostatic pressing (HIP) jacket and the heat and other static pressuring processes of preformed member are produced using the jacket | |
CN114245761A (en) | Method for producing green compact and method for producing sintered body | |
KR102605561B1 (en) | Canning free hot isostatic pressure powder metallurgy method | |
EP3646970B1 (en) | Method for fabricating components using hybrid additive manufacturing and consolidation process | |
KR102609282B1 (en) | Hot isostatic pressure powder metallurgy canning container for preventing can pollution by diffusion and the hot isostatic pressure metallurgy method using the same | |
KR102623463B1 (en) | Part manufacturing method using Near-Net Shape powder metallurgy and parts manufactured by this manufacturing method | |
US8392016B2 (en) | Adaptive method for manufacturing of complicated shape parts by hot isostatic pressing of powder materials with using irreversibly deformable capsules and inserts | |
JPS63210201A (en) | Powder sintering method | |
JPH0277501A (en) | Hot isostatic pressing method |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: PURIS, LLC, WEST VIRGINIA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:YOLTON, CHARLES F.;BONO, ERIC SCOTT;HANUSIAK, WILLIAM MICHAEL;SIGNING DATES FROM 20161221 TO 20161222;REEL/FRAME:040742/0215 |
|
AS | Assignment |
Owner name: PURIS, LLC, WEST VIRGINIA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:KIRSCH, CRAIG FREDERICK;REEL/FRAME:041016/0242 Effective date: 20170119 |
|
AS | Assignment |
Owner name: CARPENTER TECHNOLOGY CORPORATION, PENNSYLVANIA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:PURIS, LLC;REEL/FRAME:041927/0498 Effective date: 20170228 |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |