US20140283574A1 - System and process for formation of extrusion structures - Google Patents
System and process for formation of extrusion structures Download PDFInfo
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- US20140283574A1 US20140283574A1 US14/222,468 US201414222468A US2014283574A1 US 20140283574 A1 US20140283574 A1 US 20140283574A1 US 201414222468 A US201414222468 A US 201414222468A US 2014283574 A1 US2014283574 A1 US 2014283574A1
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- extrusion
- billet
- shear
- shear tool
- billet material
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/002—Extruding materials of special alloys so far as the composition of the alloy requires or permits special extruding methods of sequences
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/21—Presses specially adapted for extruding metal
- B21C23/212—Details
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/21—Presses specially adapted for extruding metal
- B21C23/218—Indirect extrusion presses
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C27/00—Containers for metal to be extruded
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C29/00—Cooling or heating work or parts of the extrusion press; Gas treatment of work
- B21C29/003—Cooling or heating of work
Definitions
- the extrusion die and a solid ram are positioned on opposite ends of the billet.
- the extrusion die is attached to a hollow ram on the same side of the billet.
- a mandrel may be attached to the hollow ram during extrusion of the billet material to produce hollow extrudates.
- extrusion structures are not limited.
- extrusion structures may be hollow tubular structures with selected uniform or non-uniform inner dimensions and selected uniform or non-uniform wall thicknesses.
- extrusion structures may be solid extrusion structures with selected uniform or non-uniform cross-sections. No limitations are intended.
- the mandrel may be a fixed mandrel or a floating mandrel.
- the extrusion die may be a bridge extrusion die.
- mandrels and extrusion dies are not limited thereto.
- Shearing forces applied by the present invention may be obtained by rotating the billet while keeping the shear tool stationary, by rotating the shear tool while keeping the billet material stationary, or by rotating the shear tool at a rotational speed different than the rotational speed of the billet material or vice versa.
- applying the rotational shear force and extruding the plasticized billet material may be performed simultaneously. In some applications, applying the rotational shear force and extruding the plasticized billet material may be performed independently from the other step.
- axial extrusion pressures required for extrusion may be reduced by at least a factor of about 16 times compared to extrusion operations performed without the rotational shearing force. In some applications, the axial extrusion pressure is at or below about 50 MPa. In some applications, the axial extrusion pressure is at or below about 25 MPa. However, axial pressures are not limited.
- Shear-assisted extrusion processing of the present invention can refine the microstructure of billet materials including cast billet materials and powdered billet materials, or other processed materials.
- billets containing coarse matrix grains and second-phase intermetallic particles with sizes up to a millimeter (1000 microns) may be refined in a single process step to yield smaller grains and particles.
- the process refines the microstructure to yield fine matrix grains and second-phase intermetallic particles with a size less than or equal to about 10 microns.
- the process yields very (ultra) fine matrix grains and second-phase intermetallic particles with a size less than or equal to about 1 micron or finer.
- the process yields grains with a size less than about 100 nanometers or finer.
- the present invention alters the morphology of second-phase particles in the starting billet material from an aspect ratio above about 2 to an aspect ratio below about 2 following the shear-assisted extrusion processing.
- microstructure grains and particles of the original billet material are refined by at least a factor of 2 times to a size that is at least one-half that of the original billet material prior to extrusion processing or finer.
- Shear-assisted extrusion processing can also uniformly distribute grains and particles within the refined microstructure.
- extrusion structures are tubular extrusion structures that may be included as components of a compression device, a stent device, a bending-resistant device.
- Compression devices include, but are not limited to, e.g., compression bumpers or collapsible safety frames deployed in automobiles.
- extrusion structures of the present invention may be incorporated as components of selected structures such as in support pillars or other structures deployed in vehicles to enhance mechanical properties, performance, or to resist bending.
- extrusion structures may be included as components of a stent device.
- FIG. 2 shows exemplary internal and external components of the extrusion assembly.
- FIG. 3B is an expanded view of the embodiment of FIG. 3A .
- FIG. 1 shows an extrusion assembly 100 of an indirect extrusion type for production of high-performance extrusion structures.
- Extrusion assembly 100 may include a shear tool 2 that is configured to apply a rotational shear (shearing) force 26 and an axial extrusion force 24 to the face of a billet material (not shown) positioned within a die chamber 10 that assists plasticization of the billet material.
- Extrusion assembly 100 and shear tool 2 may be constructed of, e.g., steel alloys (e.g., H-13 tool steel), titanium alloys, nickel alloys, and combinations of these materials that resist physical and chemical wear at a wide range of temperatures, are mechanically strong, and effectively distribute heat through the billet during extrusion processing.
- Extrusion assembly 100 may include a container 8 comprised of, e.g., an upper container plate 7 and a lower container plate 9 .
- Container 8 may also be a single component. No limitations are intended.
- outer (top) die ring 14 and a lower die ring couple together to form die chamber 10 .
- Die chamber 10 may also be a single machined component. Again, no limitations are intended.
- the billet (described hereafter in reference to FIG. 3 ) may be positioned within die chamber 10 to provide aligned contact with shear tool 2 when shear tool 2 is introduced into die chamber 10 during operation.
- Shear tool 2 may include an inner bore 4 of a selected inner dimension with orifices 5 positioned at respective ends of shear tool 2 .
- Outer (top) die ring 14 and lower die ring (not shown) secure shear tool 2 in die chamber 10 .
- Outer die ring 14 may be secured with locking keys (not shown) that insert into key slots 20 positioned on respective sides of shear tool 2 .
- Position and number of key slots 20 is not limited.
- plasticized billet materials extrude along the length of inner bore 4 and exit from an orifice 5 of shear tool 2 as extrusion structures (extrudates) 6 .
- Direction of release of extrudates is not limited, as detailed further herein.
- FIG. 2 is a three-dimensional view of die assembly 100 showing selected internal components.
- outer (top) die ring 14 is shown positioned atop bottom (base) die ring 16 .
- Keys (not shown) described previously in reference to FIG. 1 insert into key slots 20 positioned on opposite sides of outer die ring 14 that lock top die ring 14 and bottom die ring 16 together.
- a mandrel 28 is shown positioned at the base of die chamber 10 .
- Mandrels may include, e.g., fixed mandrels and floating mandrels.
- Mandrel 28 may insert into inner bore 4 of shear tool 2 , e.g., from the billet end of shear tool 2 .
- FIG. 3A is a cross-sectional view of extrusion assembly 100 of an indirect extrusion type described previously in reference to FIG. 1 .
- Extrusion assembly 100 is shown in assembled form with the flow of plasticized billet material illustrated during extrusion operation.
- outer die ring 14 and lower die ring 16 couple together to form die chamber 10 .
- die chamber 10 may also be a single machined component.
- Die chamber 10 may be assembled within the container between, e.g., upper container plate 7 and lower container plate 9 .
- the container may also be a single component.
- billet 22 is shown positioned within die chamber 10 to provide aligned contact with shear tool 2 when shear tool 2 is introduced into die chamber 10 .
- FIG. 3B shows an expanded view of the die assembly 100 of FIG. 3A .
- plasticized billet materials may flow from deformation region 34 through a gap 30 formed between the surface of mandrel 28 and the inner wall of extrusion die 11 .
- Other components of extrusion assembly 100 including billet 22 positioned in chamber 10 , optional spacer 32 , upper die ring 14 , and lower die ring 16 have been described previously herein.
- extrusion structures (extrudates) 6 that are hollow extrusion structures (e.g., tubes).
- extrusion structures may include uniform inner dimensions and wall thicknesses.
- extrusion structures may include non-uniform inner dimensions and wall thicknesses.
- extrusion structures are solid structures. Solid extrusion structures may include uniform dimensions or non-uniform dimensions.
- extrusion structures (extrudates) 6 may be released through another orifice 5 positioned at the bottom end of tool 2 .
- Billets may be in the form of solids, cast solids, blocks, semi-solids, non-solids, and/or powders.
- Cast billets may be cast using casting techniques known in the casting arts.
- Billets may be composed of, or include, any material that can be plastically deformed (plasticized) at selected temperatures.
- Billet materials are preferred that deliver desirable mechanical properties such as ductility, compression strength, bendability, or selected microstructural refinement, or other suitable properties to the extrusion structures or products produced.
- billets may include or be constructed of various materials including selected alloys and high-performance alloys.
- billets may employ magnesium alloys.
- Magnesium alloys include, but are not limited to, e.g., magnesium alloys (e.g., AZ31F); magnesium-aluminum (Mg—Al) alloys; magnesium-zinc (Mg—Zn) alloys; magnesium-zirconium (Mg—Zr) alloys; magnesium-silicon (Mg—Si) alloys (e.g., Mg-2Si; Mg-7Si); magnesium alloys that include rare-earth (RE) elements; magnesium alloys that include various non-rare-earth elements; magnesium-zinc-zirconium alloys (e.g., ZK60-T5), and combinations of these various alloys.
- magnesium alloys e.g., AZ31F
- magnesium alloys e.g., AZ31F
- magnesium alloys e.g., AZ31F
- Mg—Al magnesium-aluminum
- Mg—Zn magnesium-zinc
- Mg—Zr magnesium-zirconium
- billets used for extrusion may include a central bore or hollow cavity through which the mandrel may be introduced during extrusion.
- billets may be solid billets that are pierced or predrilled prior to use.
- Complex shapes include, but are not limited to, e.g., spherical, tetrahedral, pyramidal, pentagonal, pentagonal pyramidal, irregular, ortahedral, icosahedral, dedecahedral, stars, cones, boat-shape ovals, parallelograms, rounded rectangles, chevrons, round left, round right, bent arrows, arrows, double arcs, curved, obround, single-D, double-D, long-D, quad-D, letters, numerical, alpha-numerical, symmetrical shapes, non-symmetrical shapes, oblong shapes, rings, pictoral shapes, other non-standard shapes, including, e.g., embedded shapes such as, e.g., ovals within a square, squares within an oval, and like embedded shapes. All shapes as will be selected by those of ordinary skill in the art in view of the disclosure are within the scope of the present invention. No limitations are intended.
- TABLE 1 lists compositions of alloy billets and process parameters employed in selected extrusion tests.
- Rotation rates for the rotatable shear tool or the billet are not limited. In some embodiments, rotation may proceed at a rate up to about 1000 revolutions-per-minute (rpm). In some embodiments, rotation speed may be between about 50 rpm and about 500 rpm. In some embodiments, the process may include rotating the ram at a rate between about 500 rpm and about 1000 rpm.
- Extrusion ratio (R) may be calculated from Equation [1], as follows:
- shear-assisted extrusion of the present invention may be performed continuously to produce extrusion structures of any selected and/or extended lengths. In some embodiments, shear-assisted extrusion may be performed semi-continuously or batch-wise to produce various and/or multiple extrusion structures.
- Shear-assisted extrusion processing of the present invention refines the microstructure of cast billets. For example, billets containing coarse matrix grains and second-phase intermetallic particles with sizes up to a millimeter (1000 microns) may be refined in a single process step.
- the process yields a microstructure containing fine matrix grains and second-phase intermetallic particles with a size less than or equal to about 10 microns.
- the process yields a microstructure containing very (ultra) fine matrix grains and second-phase intermetallic particles with a size less than or equal to about 1 micron or finer.
- no limitations are intended.
- FIG. 7 is a photomicrograph showing refined grains in an exemplary high-performance extrusion structure following shear-assisted extrusion.
- grains include a size below about 10 microns, and more particularly below about 5 microns.
- the resulting microstructure may be amorphous, meaning grain size is approximately zero. Thus, no limitations are intended.
- Extrusion structures of the present invention find application as parts, pieces, or components in various devices.
- tubular extrusion structures of the present invention may find application as crush tubes or compression structures in front and rear bumpers of automobiles or in other compression applications.
- extrusion structures of the present invention may be in the form of lightweight alloy tubes that find application as dissolvable stents.
- tubes may be inexpensively produced and subsequently machined into stents.
- hollow extrusion structures of the present invention may find application as bendable components, e.g., in pillar applications for use in automobiles. All applications as will be envisioned by those of ordinary skill in the art in view of the disclosure are within the scope of the present invention. No limitations are intended.
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Abstract
Description
- This is a Non-Provisional application that claims priority from U.S. Provisional Application No. 61/804,560 filed 22 Mar. 2013, which reference is incorporated herein in its entirety.
- This invention was made with Government support under Contract DE-AC05-76RLO-1830 awarded by the U.S. Department of Energy. The Government has certain rights in the invention.
- The present invention relates generally to extrusion processing and extrusion tools. More particularly, the invention relates to a shear-assisted extrusion system and process for production of extrusion structures including high-performance extrusion structures.
- Extrusion is a process in which a billet or block of material composed of metals, polymers, ceramics, or foodstuffs is forced through an extrusion die with a ram tool that transmits an extrusion force to the billet that plasticizes the material. The plasticized material is then extruded through the orifice of an extrusion die that forms an extrusion product (extrudate). The resulting extrusion product has a cross-sectional area or profile that is typically smaller than that of the original billet. In conventional extrusion, only the linear or axial motion of the ram plasticizes and extrudes the billet material. Extrusion processes fall under two general categories: (i) direct extrusion, and (ii) indirect extrusion. In direct extrusion, the extrusion die and a solid ram are positioned on opposite ends of the billet. In indirect extrusion, the extrusion die is attached to a hollow ram on the same side of the billet. A mandrel may be attached to the hollow ram during extrusion of the billet material to produce hollow extrudates. Problems with extrusion processing are well known in the art. Conventional extrusion requires high extrusion pressures on the order of 400 MPa or higher. In addition, non-uniform deformation of extrudates is common, which yields extrusion products with structural and physical property variations in both the longitudinal and transverse directions. Further, microstructure refinement is often inconsistent and typically insufficient so mechanical properties vary widely. And, while processes like mechanical alloying, rapid solidification, friction stir processing, equal channel angular extrusion, twist extrusion, waffle pattern rolling, non-axis symmetric rolling, and other processes have been used to make high performance materials, such processes are not presently cost-effective for commercial production. Accordingly, new extrusion processing tools and processes are needed that overcome conventional force requirements and other limitations of conventional extrusion processing. The present invention addresses these needs. The purpose of the foregoing abstract is to enable the United States Patent and Trademark Office and the public generally, especially scientists, engineers, and practitioners in the art who are not familiar with patent or legal terms or phraseology, to determine quickly from a cursory inspection the nature and essence of the technical disclosure of the application. The abstract is neither intended to define the invention of the application, which is measured by the claims, nor is it intended to be limiting as to the scope of the invention in any way.
- The present invention includes an extrusion assembly and process for production of high-performance extrusion structures and extrusion products. The extrusion assembly may include a shear tool with an extrusion die of a selected shape. The shear tool is configured to apply a rotational shear (shearing) force and an axial extrusion pressure to the face of a billet material at the shear tool/billet interface positioned within the die chamber of the extrusion assembly that plastically deforms the billet material. The billet may include various selected materials including, but not limited to, e.g., metals, metal alloys, cast solids, powders, and non-solids. The extrusion die may be positioned at the billet end of the shear tool and may include an orifice with a selected shape and selected dimensions. The extrusion die may extrude the plasticized billet material along the length of the inner bore of the shear tool in response to the axial extrusion pressure applied to the face of the billet yielding extrusion structures and products with selected shapes including complex shapes with selected dimensions. The inner bore of the shear tool may include selected dimensions. The shear tool forms extrusion structures and products at an axial extrusion pressure significantly lower than required for extrusion structures without the shearing force applied. The extrusion die may extrude the plasticized billet material along the length of the inner bore of the shear tool in response to the axial extrusion pressure applied to the face of the billet material.
- The present invention also includes a shear-assisted extrusion process that produces extrusion structures including high-performance extrusion structures. The process may include applying a rotational shearing force and an axial extrusion force to the face of the billet material at the shear tool/billet interface to plasticize the billet material. The shearing force may be applied at the shear tool/billet interface by rotation of the shear tool at a selected rotation speed relative to a stationary billet, or by rotation of the billet relative to a stationary shear tool, and/or by rotation of the shear tool at a rotation speed that is different relative to the rotation of the billet, or vice versa. The plasticized material may be extruded the through an orifice of an extrusion die positioned on the billet side of the shear tool. The orifice of the extrusion die may include various selected shape that yield extrusion structures with selected shapes. Rotational shear force values are not limited. Shear forces are selected that reduce the axial extrusion pressures needed to plasticize billet materials. The extrusion assembly extrudes the billet material at an axial extrusion force less than that required for extrusions performed without the rotational shearing force applied by the shear tool and/or the billet at the shear tool/billet interface.
- In some applications, the billet may be a pierced cast billet, a pre-drilled cast billet, a solid cast billet, or loose powder billets.
- Extrusion structures may be hollow or solid. The extrusion assembly may include a mandrel that inserts into the inner bore of the shear tool to a selected depth. In some applications, the mandrel may be introduced through the center of the billet and into the inner bore through an orifice of the extrusion die positioned at the billet end or other end of the shear tool. The mandrel may include a width dimension that is less than the dimension of the orifice of the extrusion die that forms a separation gap between the surface of the mandrel and the inner wall of the extrusion die when the mandrel is inserted. During extrusion, the separation gap allows plasticized materials to flow past the mandrel along the length of the inner wall of the extrusion die and into the inner bore of the shear tool that yields hollow extrusion structures with selected shapes. The extrusion die determines the wall thickness of hollow extrusion structures produced during extrusion.
- Shapes are not limited. In various applications, extrusion structures may be hollow tubular structures with selected uniform or non-uniform inner dimensions and selected uniform or non-uniform wall thicknesses. In various applications, extrusion structures may be solid extrusion structures with selected uniform or non-uniform cross-sections. No limitations are intended.
- In some applications, the mandrel may be a fixed mandrel or a floating mandrel. In some applications, the extrusion die may be a bridge extrusion die. However, mandrels and extrusion dies are not limited thereto.
- The shear tool may include one or more surface features positioned at the billet end of the shear tool that engage the face of the billet material to facilitate shear-assisted extrusion and flow of plasticized materials during operation. Features may include, but are not limited to, e.g., scrolls, flutes, vanes, or other features including combinations of these features.
- In some applications, the extrusion assembly may include a heating device such as an external heating device or an embedded heating device and/or a cooling device positioned to heat or cool the billet material positioned within the die chamber, respectively. Billet materials may also be heated using the frictional heat generated from the plastically deformed billet materials.
- Extrusion temperatures are not limited. In some applications, extrusion of the plasticized billet material may be performed at a temperature selected between about −196° C. and about 0° C. In some applications, extrusion of the plasticized billet material may be performed at a temperature selected between about 0° C. and about 1000° C., or greater.
- Shearing forces applied by the present invention may be obtained by rotating the billet while keeping the shear tool stationary, by rotating the shear tool while keeping the billet material stationary, or by rotating the shear tool at a rotational speed different than the rotational speed of the billet material or vice versa.
- In some applications, applying the rotational shear force and extruding the plasticized billet material may be performed simultaneously. In some applications, applying the rotational shear force and extruding the plasticized billet material may be performed independently from the other step.
- In some applications, axial extrusion pressures required for extrusion may be reduced by at least a factor of about 16 times compared to extrusion operations performed without the rotational shearing force. In some applications, the axial extrusion pressure is at or below about 50 MPa. In some applications, the axial extrusion pressure is at or below about 25 MPa. However, axial pressures are not limited.
- Feed rates for the billet are not limited. In some applications, feed rates may be between about 0.15 inches (0.38 cm) per minute and about 1.18 inches (3.0 cm) per minute.
- Rotational speeds are not limited. In various applications, rotation may be performed at a rotation speed between about 500 revolutions-per-minute (rpm) and about 1000 rpm. In some applications, rotation may be performed at a rotation speed up to about 1000 rpm. In some applications, rotation speed may be between about 10 rpm and about 1000 rpm.
- Shear-assisted extrusion processing of the present invention can refine the microstructure of billet materials including cast billet materials and powdered billet materials, or other processed materials. For example, billets containing coarse matrix grains and second-phase intermetallic particles with sizes up to a millimeter (1000 microns) may be refined in a single process step to yield smaller grains and particles. In some applications, the process refines the microstructure to yield fine matrix grains and second-phase intermetallic particles with a size less than or equal to about 10 microns. In some applications, the process yields very (ultra) fine matrix grains and second-phase intermetallic particles with a size less than or equal to about 1 micron or finer. In some applications, the process yields grains with a size less than about 100 nanometers or finer. However, no limitations are intended. In some applications, the present invention alters the morphology of second-phase particles in the starting billet material from an aspect ratio above about 2 to an aspect ratio below about 2 following the shear-assisted extrusion processing. In some applications, microstructure grains and particles of the original billet material are refined by at least a factor of 2 times to a size that is at least one-half that of the original billet material prior to extrusion processing or finer. Shear-assisted extrusion processing can also uniformly distribute grains and particles within the refined microstructure.
- In some applications, extrusion structures are tubular extrusion structures that may be included as components of a compression device, a stent device, a bending-resistant device. Compression devices include, but are not limited to, e.g., compression bumpers or collapsible safety frames deployed in automobiles. In various applications, extrusion structures of the present invention may be incorporated as components of selected structures such as in support pillars or other structures deployed in vehicles to enhance mechanical properties, performance, or to resist bending. In some applications, extrusion structures may be included as components of a stent device.
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FIG. 1 is an isometric external view of an extrusion assembly of an indirect extrusion type, according to one embodiment of the present invention. -
FIG. 2 shows exemplary internal and external components of the extrusion assembly. -
FIG. 3A is a cross-sectional view of the extrusion assembly ofFIG. 1 . -
FIG. 3B is an expanded view of the embodiment ofFIG. 3A . -
FIG. 3C shows a cross-sectional view of an extrusion assembly of a direct extrusion type, according to another embodiment of the present invention. -
FIG. 4 is a perspective view of a shear tool that includes a scroll feature. -
FIG. 5 compares extrusion pressure data for conventional indirect extrusion and shear-assisted extrusion of the present invention. -
FIG. 6 shows exemplary tubular extrusion structures produced by the process of the present invention. -
FIG. 7 is a photomicrograph showing grains and particles in the extrusion structure following extrusion processing. - A new shear-assisted extrusion apparatus and process are disclosed for producing high-performance extrusion structures including, e.g., hollow and solid extrusion structures. In the following description, embodiments of the present invention are shown and described that include a best mode contemplated for carrying out the invention. It will be clear from the following description that the invention is susceptible of various modifications and alternative constructions. The present invention is intended to cover all modifications, alternative constructions, and equivalents falling within the spirit and scope of the invention as defined in the claims. Therefore the description should be seen as illustrative and not limiting.
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FIG. 1 shows anextrusion assembly 100 of an indirect extrusion type for production of high-performance extrusion structures.Extrusion assembly 100 may include ashear tool 2 that is configured to apply a rotational shear (shearing)force 26 and anaxial extrusion force 24 to the face of a billet material (not shown) positioned within adie chamber 10 that assists plasticization of the billet material.Extrusion assembly 100 andshear tool 2 may be constructed of, e.g., steel alloys (e.g., H-13 tool steel), titanium alloys, nickel alloys, and combinations of these materials that resist physical and chemical wear at a wide range of temperatures, are mechanically strong, and effectively distribute heat through the billet during extrusion processing. -
Extrusion assembly 100 may include acontainer 8 comprised of, e.g., anupper container plate 7 and alower container plate 9.Container 8 may also be a single component. No limitations are intended. In the instant embodiment, outer (top) diering 14 and a lower die ring (described further in reference toFIG. 2 ) couple together to form diechamber 10. Diechamber 10 may also be a single machined component. Again, no limitations are intended. The billet (described hereafter in reference toFIG. 3 ) may be positioned withindie chamber 10 to provide aligned contact withshear tool 2 whenshear tool 2 is introduced intodie chamber 10 during operation. -
Shear tool 2 may include aninner bore 4 of a selected inner dimension withorifices 5 positioned at respective ends ofshear tool 2. Outer (top) diering 14 and lower die ring (not shown)secure shear tool 2 indie chamber 10.Outer die ring 14 may be secured with locking keys (not shown) that insert intokey slots 20 positioned on respective sides ofshear tool 2. Position and number ofkey slots 20 is not limited. During operation, plasticized billet materials extrude along the length ofinner bore 4 and exit from anorifice 5 ofshear tool 2 as extrusion structures (extrudates) 6. Direction of release of extrudates is not limited, as detailed further herein. -
FIG. 2 is a three-dimensional view ofdie assembly 100 showing selected internal components. In the figure, outer (top) diering 14 is shown positioned atop bottom (base) diering 16. Keys (not shown) described previously in reference toFIG. 1 insert intokey slots 20 positioned on opposite sides ofouter die ring 14 that locktop die ring 14 and bottom diering 16 together. Amandrel 28 is shown positioned at the base ofdie chamber 10. Mandrels may include, e.g., fixed mandrels and floating mandrels.Mandrel 28 may insert intoinner bore 4 ofshear tool 2, e.g., from the billet end ofshear tool 2.Mandrel 28 may direct flow of extruded billet materials along the length ofinner bore 2. Extruded materials may release through anorifice 5 positioned, e.g., at a top end ofshear tool 2. However, release is not limited thereto, as detailed further herein. -
FIG. 3A is a cross-sectional view ofextrusion assembly 100 of an indirect extrusion type described previously in reference toFIG. 1 .Extrusion assembly 100 is shown in assembled form with the flow of plasticized billet material illustrated during extrusion operation. In the figure,outer die ring 14 andlower die ring 16 couple together to form diechamber 10. In some embodiments, diechamber 10 may also be a single machined component. Diechamber 10 may be assembled within the container between, e.g.,upper container plate 7 andlower container plate 9. In some embodiments, the container may also be a single component. In the figure,billet 22 is shown positioned withindie chamber 10 to provide aligned contact withshear tool 2 whenshear tool 2 is introduced intodie chamber 10. Amandrel 28 described previously in reference toFIG. 2 may be positioned inchamber 10, which may insert to a selected depth ininner bore 4 ofshear tool 2 during assembly through an optional spacer (e.g., a graphite spacer) 32 throughbillet 22 and through anorifice 5 of anextrusion die 11. Extrusion die 11 may be positioned at the billet end ofshear tool 2. Extrusion dies are not limited. In some embodiments, a bridge die may be employed.Orifice 5 of extrusion die 11 may include selected shapes described further herein. The extrusion die determines at least in part the shape of extrusion structures produced during extrusion operation.Mandrel 28,optional spacer 32, andbillet 22 may be secured inchamber 10 by introducing locking keys (described previously) intokey slots 20 positioned on respective sides ofouter die ring 14 as described previously herein. - In operation,
shear tool 2 when introduced intochamber 10 applies a rotational shear (shearing)force 26 and anaxial extrusion force 24 to the face ofbillet material 22 at the shear tool/billet interface withindie chamber 10. Rotational shear (shearing)force 26 assists or promotes plasticization ofbillet material 22. In some embodiments, rotational shear (shearing)force 26 may be applied by rotating theshear tool 2 at a selected rotation speed while keepingbillet 22 stationary. In some embodiments, rotational shear (shearing)force 26 may be applied by rotating thebillet 22 while keepingshear tool 2 stationary. In some embodiments, rotational shear (shearing)force 26 is applied by rotatingshear tool 2 andbillet 22 at different rotation speeds relative to the other component or material. - Die assembly 100 may further include an optional heater/cooler 36 that couples externally to, or is embedded within,
outer die ring 14 to heat orcool billet material 22 positioned withinchamber 10. Heating and cooling ofbillet material 22 can be used to assist deformation ofbillet material 22, e.g., by softening the billet material in cases where the billet material shows limited initial plasticity. Heating may also be used, e.g., to lower frictional forces that assist extrusion of the plasticized billet material. All heating and cooling devices as will be selected by those of ordinary skill in the art in view of this disclosure are within the scope of the present invention. No limitations are intended. - Application of
axial extrusion force 24,rotational shear force 26, and/or heat or cooling tobillet material 22 plasticizes the billet material, which forms a region of plastic deformation (SPD) 34 positioned at the shear tool/billet interface.SPD region 34 is typically narrow (e.g., <300 microns) to reduceextrusion force 24 needed to extrude the plasticized billet materials. - Plasticized billet materials may enter into
inner bore 4 through an orifice (not shown) positioned, e.g., at the billet end ofshear tool 2. In the instant embodiment, plasticized material extrudespast mandrel 28 and flows upward to yield extrusion structures (extrudates) 6 that are hollow extrusion structures (e.g., tubes). In some embodiments, extrusion structures may include uniform inner dimensions and wall thicknesses. In some embodiments, extrusion structures may include non-uniform inner dimensions and wall thicknesses. When mandrel 28 is not employed, extrusion structures are solid structures. Solid extrusion structures may include uniform dimensions or non-uniform dimensions. In the instant embodiment, extrusion structures (extrudates) 6 may be released through anotherorifice 5 positioned at the top end ofshear tool 2. -
FIG. 3B shows an expanded view of thedie assembly 100 ofFIG. 3A . As shown in the figure, plasticized billet materials may flow fromdeformation region 34 through agap 30 formed between the surface ofmandrel 28 and the inner wall of extrusion die 11. Other components ofextrusion assembly 100 includingbillet 22 positioned inchamber 10,optional spacer 32,upper die ring 14, andlower die ring 16 have been described previously herein. -
FIG. 3C is a cross-sectional view of another embodiment ofextrusion assembly 100 of a direct extrusion type. Dieassembly 100 is shown in assembled form and also shows flow of plasticized billet material during extrusion operation. In the figure, dieassembly 100 includes a billet rotation tool or device, e.g., diering 16, configured to applyrotational shear force 26 to thebillet material 22 positioned withindie chamber 10.Billet material 22 may be in aligned contact withtool 2 or a die support. Amandrel 28 described previously in reference toFIG. 3A may be positioned inchamber 10, which may insert to a selected depth ininner bore 4 ofshear tool 2 during assembly through an optional spacer (e.g., a graphite spacer) 32 throughbillet 22 and through an orifice (not shown) of extrusion die 11 positioned at the billet end ofshear tool 2. Extrusion dies are not limited. In some embodiments, a bridge die may be employed. In operation,billet rotation tool 16 applies a rotational shear (shearing)force 26 and anaxial extrusion force 24 to the face ofbillet material 22 at the shear tool/billet interface withindie chamber 10.Extrusion assembly 100 may further include an optional heater/cooler (not shown) described previously in reference toFIG. 3A . Application ofaxial extrusion force 24,rotational shear force 26, and/or heat or cooling tobillet material 22 plasticizes the billet material, which forms a region of plastic deformation (SPD) 34 positioned at the shear tool/billet interface.SPD region 34 is preferably narrow (e.g., <300 microns) to reduce theextrusion force 24 needed to extrude plasticized billet materials. Plasticized billet materials may flow downward fromdeformation region 34 and extrude through anorifice 5 of extrusion die 11 that is positioned at the billet end oftool 2 intoinner bore 4. Plasticized billet materials may then flow through gap (FIG. 3B ) formed between the external surface ofmandrel 28 and the inner wall (not shown) of extrusion die 11. In the instant embodiment, plasticized material extrudespast mandrel 28 and flows downward to yield extrusion structures (extrudates) 6 that are hollow extrusion structures (e.g., tubes). In some embodiments, extrusion structures may include uniform inner dimensions and wall thicknesses. In some embodiments, extrusion structures may include non-uniform inner dimensions and wall thicknesses. When mandrel 28 is not employed, extrusion structures are solid structures. Solid extrusion structures may include uniform dimensions or non-uniform dimensions. In the instant embodiment, extrusion structures (extrudates) 6 may be released through anotherorifice 5 positioned at the bottom end oftool 2. -
FIG. 4 is a perspective view showing an exemplary configuration forshear tool 2. In the instant embodiment,shear tool 2 includes ascroll feature 38 positioned at an end (face) ofshear tool 2 that engages the face of the billet (FIG. 3 ) to facilitate shear-assisted extrusion and flow of plasticized materials. Features include, but are not limited to, e.g., scrolls, flutes, vanes, and like features. Number of features and types of features are not intended to be limited. - Billets may be in the form of solids, cast solids, blocks, semi-solids, non-solids, and/or powders. Cast billets may be cast using casting techniques known in the casting arts. Billets may be composed of, or include, any material that can be plastically deformed (plasticized) at selected temperatures. Billet materials are preferred that deliver desirable mechanical properties such as ductility, compression strength, bendability, or selected microstructural refinement, or other suitable properties to the extrusion structures or products produced. However, no limitations are intended. In various embodiments, billets may include or be constructed of various materials including selected alloys and high-performance alloys. In some embodiments, billets may employ magnesium alloys. Magnesium alloys include, but are not limited to, e.g., magnesium alloys (e.g., AZ31F); magnesium-aluminum (Mg—Al) alloys; magnesium-zinc (Mg—Zn) alloys; magnesium-zirconium (Mg—Zr) alloys; magnesium-silicon (Mg—Si) alloys (e.g., Mg-2Si; Mg-7Si); magnesium alloys that include rare-earth (RE) elements; magnesium alloys that include various non-rare-earth elements; magnesium-zinc-zirconium alloys (e.g., ZK60-T5), and combinations of these various alloys. While magnesium-based alloys are described herein due to their desirable ductility properties for compression applications, the present invention is not intended to be limited thereto. In some embodiments, billets used for extrusion may include a central bore or hollow cavity through which the mandrel may be introduced during extrusion. In some embodiments, billets may be solid billets that are pierced or predrilled prior to use.
- The shear tool of the present invention may include an extrusion die that includes an inner bore with various selected shapes that delivers extrusion structures with selected shapes including complex shapes. Shapes include, but are not limited to, e.g., round, oval, circular, square, rectangular, triangular, pentagonal, hexagonal, octagonal, ellipsoidal, trapezoidal, rhombal, or combinations of these various shapes. Complex shapes include, but are not limited to, e.g., spherical, tetrahedral, pyramidal, pentagonal, pentagonal pyramidal, irregular, ortahedral, icosahedral, dedecahedral, stars, cones, boat-shape ovals, parallelograms, rounded rectangles, chevrons, round left, round right, bent arrows, arrows, double arcs, curved, obround, single-D, double-D, long-D, quad-D, letters, numerical, alpha-numerical, symmetrical shapes, non-symmetrical shapes, oblong shapes, rings, pictoral shapes, other non-standard shapes, including, e.g., embedded shapes such as, e.g., ovals within a square, squares within an oval, and like embedded shapes. All shapes as will be selected by those of ordinary skill in the art in view of the disclosure are within the scope of the present invention. No limitations are intended.
- TABLE 1 lists compositions of alloy billets and process parameters employed in selected extrusion tests.
-
TABLE 1 Test Matrix for selected extrusion structures of the present invention. Ram Rotation Feed Rate Test No. Alloy (rpm) (inches/min) 1 Mg—2Si 500 0.15 2 Mg—7Si 500 0.15 3 AZ31F 500 0.15 4 ZK60-T5 500 0.15 - Billet feed rates are not limited. Feed rates may be selected that maximize extrusion throughput, plasticity, flow, uniformity of the extrudates, and other physical and mechanical properties. In some embodiments, feed rates for billet deformation may be greater than about 0.01 inches per minute. In some embodiments, feed rates for billet deformation may be between about 0.01 inches per minute and about 0.1 inches per minute. In some embodiments, feed rates for billet deformation may be between about 0.1 inches per minute and about 1.0 inches per minute. In some embodiments, feed rates for billet deformation may be between about 1.0 inches per minute and about 10 inches per minute.
- Rotation rates for the rotatable shear tool or the billet are not limited. In some embodiments, rotation may proceed at a rate up to about 1000 revolutions-per-minute (rpm). In some embodiments, rotation speed may be between about 50 rpm and about 500 rpm. In some embodiments, the process may include rotating the ram at a rate between about 500 rpm and about 1000 rpm.
- Extrusion temperatures are not limited. Temperatures may be selected that maximize shear on the face of the billet, plastic deformation of the selected billet materials, microstructure refinement, and other physical and mechanical properties. In some embodiments, extrusion may be performed at temperatures above about 100° C. In some embodiments, extrusion may be performed at temperatures between about 100° C. and about 500° C. In some embodiments, extrusion may be performed at temperatures between about 500° C. and about 1000° C. In some embodiments, extrusion may be performed at temperatures above about 1000° C. In some embodiments, extrusion may be performed at temperatures below about 100° C. In some embodiments, extrusion may be performed at temperatures between about 0° C. and about −100° C. In some embodiments, extrusion may be performed at temperatures between about −100° C. and about −196° C. (the temperature of liquid nitrogen). No limitations are intended. In other embodiments, temperatures may be selected that are identified from equilibrium phase diagrams of the selected alloys or the billet materials being processed. No limitations are intended.
-
FIG. 5 plots extrusion pressure (axial load/billet cross sectional area) against the displacement (i.e., depth) of the shear tool. Data in the figure compare axial extrusion pressure (force) for shear-assisted extrusion processing of the present invention against conventional extrusion applied to the face of a 1.25″ (3.18 cm) diameter magnesium alloy billet [e.g., a ZK60 grade magnesium-zinc-zirconium (Mg—Zn—Zr) alloy, Luoyang Kunyao Metal Material Co., Ltd., Luoyang, China]. As shown, significantly higher extrusion pressures are required for the extrusion performed absent the shear tool when compared to the shear-assisted extrusion. Maximum process pressure applied by the shear tool during shear-assisted extrusion is less than about 20 MPa at a shear tool displacement of 0.13 inches (0.32 cm). By comparison, conventional extrusion processing requires an extrusion pressure greater than about 400 MPa (e.g., 430 MPa) and a temperature of 350° C. (i.e., when billets are already soft), a factor of 16 times greater than shear-assisted extrusion processing of the present invention. In some embodiments, the present invention employs an extrusion pressure below about 50 MPa. In some embodiments, shear-assisted extrusion processing employs an extrusion pressure below about 25 MPa. Dimensions of hollow extrusion structures including the inner bore dimension and inner wall thickness are not limited. Extrusion structures may also be solid structures. Cross sectional dimensions, shapes, and length dimensions are not limited. TABLE 2 lists dimensions of exemplary hollow extrusion structures of the present invention obtained in selected extrusion tests from selected alloy billets.FIG. 6 shows photos of the tubes obtained. - TABLE 2 lists results obtained from extrusion of selected materials.
-
O.D. I.D. Extrusion Extrusion TEST # ALLOY Inches mm Inches mm Ratio Rate 1 Mg—2Si 0.292 7.42 0.231 5.87 48.977 7.347 2 Mg—7Si 0.291 7.39 0.233 5.92 51.412 7.712 3 AZ31F 0.291 7.39 0.232 5.89 50.637 7.596 4 ZK60-TS 0.293 7.44 0.23 5.84 47.422 7.113 AVERAGE 0.292 7.41 0.232 5.88 49.612 7.442 STD. DEV. 9.5E−4 2.4E−2 1.3E−3 0.033 1.779 0.267 - Extrusion ratio (R) may be calculated from Equation [1], as follows:
-
R=A 0 /A f [1] - Here, (A0) is the initial cross sectional area of the billet, and (Af) is the final cross-sectional area of the extrusion structures following extrusion.
- In some embodiments, shear-assisted extrusion of the present invention may be performed continuously to produce extrusion structures of any selected and/or extended lengths. In some embodiments, shear-assisted extrusion may be performed semi-continuously or batch-wise to produce various and/or multiple extrusion structures.
- Shear-assisted extrusion processing of the present invention refines the microstructure of cast billets. For example, billets containing coarse matrix grains and second-phase intermetallic particles with sizes up to a millimeter (1000 microns) may be refined in a single process step. In some embodiments, the process yields a microstructure containing fine matrix grains and second-phase intermetallic particles with a size less than or equal to about 10 microns. In some embodiments, the process yields a microstructure containing very (ultra) fine matrix grains and second-phase intermetallic particles with a size less than or equal to about 1 micron or finer. However, no limitations are intended. For example, in some embodiments, the present invention alters the morphology of second-phase particles in the starting billet material from an aspect ratio above about 2 to an aspect ratio below about 2 following shear-assisted extrusion processing. In some embodiments, microstructure grains and particles of the original billet material are refined by at least a factor of 2 times or finer. Grains and/or particles are formed that have a size at least one-half that of grains in the original billet material prior to extrusion processing. Shear-assisted extrusion processing can further distribute grains and particles uniformly within the refined microstructure.
-
FIG. 7 is a photomicrograph showing refined grains in an exemplary high-performance extrusion structure following shear-assisted extrusion. In the figure, grains include a size below about 10 microns, and more particularly below about 5 microns. In some embodiments, the resulting microstructure may be amorphous, meaning grain size is approximately zero. Thus, no limitations are intended. - Extrusion structures of the present invention find application as parts, pieces, or components in various devices. In some embodiments, tubular extrusion structures of the present invention may find application as crush tubes or compression structures in front and rear bumpers of automobiles or in other compression applications. In other embodiments, extrusion structures of the present invention may be in the form of lightweight alloy tubes that find application as dissolvable stents. For example, tubes may be inexpensively produced and subsequently machined into stents. In yet other embodiments, hollow extrusion structures of the present invention may find application as bendable components, e.g., in pillar applications for use in automobiles. All applications as will be envisioned by those of ordinary skill in the art in view of the disclosure are within the scope of the present invention. No limitations are intended.
- While preferred embodiments of the present invention have been shown and described, it will be apparent to those of ordinary skill in the art that many changes and modifications may be made without departing from the invention in its true scope and broader aspects. The appended claims are therefore intended to cover all such changes and modifications as fall within the spirit and scope of the invention.
Claims (23)
Priority Applications (20)
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US15/351,201 US10189063B2 (en) | 2013-03-22 | 2016-11-14 | System and process for formation of extrusion products |
US15/898,515 US10695811B2 (en) | 2013-03-22 | 2018-02-17 | Functionally graded coatings and claddings |
US16/028,173 US11045851B2 (en) | 2013-03-22 | 2018-07-05 | Method for Forming Hollow Profile Non-Circular Extrusions Using Shear Assisted Processing and Extrusion (ShAPE) |
US16/562,314 US11383280B2 (en) | 2013-03-22 | 2019-09-05 | Devices and methods for performing shear-assisted extrusion, extrusion feedstocks, extrusion processes, and methods for preparing metal sheets |
US16/916,548 US11517952B2 (en) | 2013-03-22 | 2020-06-30 | Shear assisted extrusion process |
US17/033,854 US20210053100A1 (en) | 2013-03-22 | 2020-09-27 | Devices and Methods for Performing Shear-Assisted Extrusion and Extrusion Processes |
US17/035,597 US20210197241A1 (en) | 2013-03-22 | 2020-09-28 | Shape processes, feedstock materials, conductive materials and/or assemblies |
US17/175,464 US11534811B2 (en) | 2013-03-22 | 2021-02-12 | Method for forming hollow profile non-circular extrusions using shear assisted processing and extrusion (ShAPE) |
US17/242,166 US20210379638A1 (en) | 2013-03-22 | 2021-04-27 | Devices and Methods for Performing Shear-Assisted Extrusion and Extrusion Processes |
US17/473,178 US20210402471A1 (en) | 2013-03-22 | 2021-09-13 | Devices and Methods for Performing Shear-Assisted Extrusion and Extrusion Processes |
US17/665,433 US11684959B2 (en) | 2013-03-22 | 2022-02-04 | Extrusion processes for forming extrusions of a desired composition from a feedstock |
US17/826,054 US20220297174A1 (en) | 2013-03-22 | 2022-05-26 | Devices and Methods for Performing Shear-Assisted Extrusion, Extrusion Feedstocks, Extrusion Processes, and Methods for Preparing Metal Sheets |
US17/874,140 US20220371067A1 (en) | 2013-03-22 | 2022-07-26 | Devices and Methods for Performing Shear-Assisted Extrusion and Extrusion Processes |
US17/957,207 US20230042802A1 (en) | 2013-03-22 | 2022-09-30 | Devices and Methods for Performing Shear-Assisted Extrusion and Extrusion Processes |
US17/984,144 US20230088412A1 (en) | 2013-03-22 | 2022-11-09 | Functionally Graded Coatings and Claddings |
US17/985,611 US20230081786A1 (en) | 2013-03-22 | 2022-11-11 | Method for Forming Hollow Profile Non-Circular Extrusions Using Shear Assisted Processing and Extrusion (ShAPE) |
US18/093,636 US20230150022A1 (en) | 2013-03-22 | 2023-01-05 | Devices and Methods for Performing Shear-Assisted Extrusion and Extrusion Processes |
US18/121,563 US20230234115A1 (en) | 2013-03-22 | 2023-03-14 | Extrusion processes, feedstock materials, conductive materials and/or assemblies |
US18/426,042 US20240216973A1 (en) | 2013-03-22 | 2024-01-29 | Devices and methods for performing shear-assisted extrusion and extrusion processes |
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