Apparatus and Process for Producing Additive Manufactured Metal Matrix Composites and Articles of Manufacture Thereof
20190084046 ยท 2019-03-21
Inventors
- Robert Swartz (Highland Park, IL)
- John Bayldon (Northbrook, IL, US)
- Buckley Crist (Wilmette, IL, US)
- Eugene Gore (Des Plaines, IL, US)
Cpc classification
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B22F7/08
PERFORMING OPERATIONS; TRANSPORTING
B22F7/04
PERFORMING OPERATIONS; TRANSPORTING
B22F2007/045
PERFORMING OPERATIONS; TRANSPORTING
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
B22F7/08
PERFORMING OPERATIONS; TRANSPORTING
B29C64/112
PERFORMING OPERATIONS; TRANSPORTING
B22F2998/10
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B22F7/062
PERFORMING OPERATIONS; TRANSPORTING
B22F7/062
PERFORMING OPERATIONS; TRANSPORTING
B33Y30/00
PERFORMING OPERATIONS; TRANSPORTING
C22C47/20
CHEMISTRY; METALLURGY
B22F12/00
PERFORMING OPERATIONS; TRANSPORTING
B29C67/00
PERFORMING OPERATIONS; TRANSPORTING
B22F2998/10
PERFORMING OPERATIONS; TRANSPORTING
B33Y40/00
PERFORMING OPERATIONS; TRANSPORTING
C22C47/20
CHEMISTRY; METALLURGY
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
International classification
B22F7/04
PERFORMING OPERATIONS; TRANSPORTING
B29C67/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y30/00
PERFORMING OPERATIONS; TRANSPORTING
C22C47/20
CHEMISTRY; METALLURGY
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B22F3/00
PERFORMING OPERATIONS; TRANSPORTING
C22C47/06
CHEMISTRY; METALLURGY
Abstract
A method, product, apparatus, and article of manufacture for the application of the Composite Based Additive Manufacturing (CBAM) method to produce objects in metal, and in metal fiber hybrids or composites. The approach has many advantages, including the ability to produce more complex geometries than conventional methods such as milling and casting, improved material properties, higher production rates and the elimination of complex fixturing, complex tool paths and tool changes and, for casting, the need for patterns and tools. The approach works by slicing a 3D model, selectively printing a fluid onto a sheet of substrate material for each layer based on the model, flooding onto the substrate a powdered metal to which the fluid adheres in printed areas, clamping and aligning a stack of coated sheets, heating the stacked sheets to melt the powdered metal and fuse the layers of substrate, and removing excess powder and unfused substrate.
Claims
1. An apparatus for producing a 3-D metal object, comprising: an inkjet printer configured to read a file of layers of the 3D object and, for each particular layer, configured to print with a fluid the shape of the particular layer selectively onto a sheet of substrate material; a vibrating trough constructed to dispense a powdered metal mixture onto the sheet of substrate material to produce a powdered sheet, the powdered metal mixture adhering selectively to the printed fluid on the sheet of substrate material; the vibrating trough causing the powdered metal mixture to flow uniformly from a powder reservoir onto the sheet; wherein, the powdered metal mixture comprises powdered metal and a flux material; a removal device to remove excess powder from the powdered sheet; a stacker constructed to stack the powdered sheet, after excess powder removal, onto a stack of powdered sheets, wherein each sheet in the stack of powdered sheets corresponds to a layer in the file of layers; a heating and compressing apparatus constructed to heat and compress the stack of powdered sheets to melt the powdered metal mixture and fuse the layers producing the 3-D metal object.
2. The apparatus of claim 1, further comprising a removal device configured to remove unfused material of the substrate sheets.
3. The apparatus of claim 1 wherein the powdered metal is a solder powder.
4. The apparatus of claim 1, wherein the powdered metal is aluminum, iron, steel, copper, brass, titanium, tin or zinc.
5. The apparatus of claim 1, wherein the removal device removes excess powder using a mechanical means.
6. The apparatus of claim 5 wherein the mechanical means is a vibrator, and air jet, or a vacuum.
7. The apparatus of claim 1, wherein the removal device removes excess powder using a stream of air, a vacuum, or a vibrator.
8. The apparatus of claim 1, wherein the flux material is a powder.
9. The apparatus of claim 1, wherein the heating apparatus and compressing apparatus uses a reducing atmosphere, a vacuum, or an inert atmosphere.
10. The apparatus of claim 9, wherein the powdered metal is aluminum or titanium and the heating apparatus uses an inert atmosphere.
11. The apparatus of claim 1, wherein the heating apparatus raises temperature to the metal powder mixture's melting point.
12. The apparatus of claim 2, wherein the removal device removes unfused substrate material by air-blasting with an abrasive material or by a chemical means.
13. The apparatus of claim 1, wherein the fluid is a solution comprising de-ionized water, pyrrolidone, and alcohol.
14. The apparatus of claim 1, wherein the fluid includes an anti-evaporant chosen from the group consisting of glycols and pyrrolidones.
15. A method for producing a 3-D object, comprising: reading a file of layers of the 3D object, layer by layer, each layer having a shape; for each layer, printing a fluid selectively onto a sheet of substrate material, the printing representing the shape of that layer; flooding onto the substrate a powdered metal mixture that adheres to the selectively printed fluid; removing excess powder; and heating and compressing a plurality of sheets in stacked registration to melt the powdered metal and fuse the layers into the 3-D object.
16. The method of claim 15, further comprising removing unfused material from the 3-D object.
17. The method of claim 1, wherein registration holes are used to stack the sheets in registration.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION OF INVENTION
Output of the Technique
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Description of the Technique
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[0015] 1. Generate a CAD model (Step 102) which is sliced into layers (Step 104) by using a slicer program like Netfabb as described in (International Publication No. WO 2014/134224 A2, ?0055; see also US Application Nos. U.S. 61/528,537 and U.S. 61/769,724). Each slice also includes registration holes, which will be used to orient each printed layer of substrate within the finished object exactly (International Publication No. WO 2014/134224 A2, ?00121).
[0016] 2. The output of the slicer, which for example may be a bitmap file, is sent to an inkjet printer (Step 106). For each layer, the printer selectively prints a fluid onto a sheet of substrate material (Step 108) (International Publication No. WO 2014/134224 A2, ?00113). The fluid may either be the bonding agent itself in liquid form; or it may be a liquid to which a powdered bonding agent adheres. Substrates can include fiberglass, high temperature glass fibers, boron fibers, or carbon fibers.
[0017] 3. If powdered bonding agent is being used, it is flooded onto the printed substrate (International Publication No. WO 2014/134224 A2, ?0059). The powder adheres to the printed areas. Excess powder is removed, either by a stream of air, vacuum, vibration, or other mechanical means.
[0018] 4. The coated sheets of substrate are stacked in press or clamp (Step 110) (International Publication No. WO 2014/134224 A2, ?00124), using the registration holes of each layer to align the printed portions of each sheet within the stack (International Publication No. WO 2014/134224 A2, ?00106).
[0019] 5. The assembled sheets are then heated and possibly compressed in an oven, to melt the bonding material and fusing the layers of substrate to form the 3D object (Step 112) (International Publication No. WO 2014/134224 A2, ?00149).
[0020] 6. The unfused substrate around the 3D object is then removed (Step 114), usually by abrasive blasting material or chemical means (International Publication No. WO 2014/134224 A2, ?0081).
Issues in Using Metals with the Technique
[0021] It has been discovered that metals can be used with this technique. In one example the substrate used is a non-woven carbon fiber veil such as available from Hollingsworth and Vose. Veils that have been metal coated can also be used. The veil or substrate is printed as described above on an inkjet printer using, for example, a HP45 thermal inkjet head with a solution primarily of de-ionized water, pyrrolidone and alcohol. The solution may have an anti-evaporant including glycols and pyrrolidones. This fluid is printed on the area of the substrate that would be part of the object, i.e., the printed area corresponds to a layer shape for the object. This is done for each layer as described in the previous applications. Each layer is flooded with a metal powder for example a solder powder. The excess powder is removed by mechanical, vacuum, vibration or compressed air or a combination of such methods. This leaves the solder powder selectively deposited. One of the problems with using a metal powder in a process of this kind is that the powder oxidizes so that that when heated to its melting point the particles of the powder will not fuse together well. There are a number of solutions to this problem, one such solution is to mix the metal powder with a powder flux such as rosin which acts as a reducing agent. A typical flux to metal powder ratio is about 50/50. Another method is to melt the powders in a reducing, vacuum and/or inert atmosphere oven. In this way other metals or alloys can be used, such as aluminum, steel, stainless steel, copper, brass, and titanium among others. In addition liquid flux may be used as or in combination with the printing fluid, through selective deposition methods such as inkjet printing.
[0022] As an example the metal powder can be mixed with a powder flux before it is deposited on the substrate. Then all the layers of the object are printed and stacked in register as described in the earlier applications. They are compressed and heated as described in the earlier applications. The heating temperature is raised to the melting point of the powder. The layers fuse together and produce a build block. After the build block is removed from the compression jig the build block is abrasively blasted and the areas where no powder adhered, that is the portions of the object that were not coated with metal, are abrasive blasted off, the uncoated carbon fiber being very fragile. What is left is a three dimensional carbon fiber metal composite of the part that was represented by the CAD model.
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