US20140283574A1 - System and process for formation of extrusion structures - Google Patents

System and process for formation of extrusion structures Download PDF

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Publication number
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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US
United States
Prior art keywords
extrusion
billet
shear
shear tool
billet material
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
Application number
US14/222,468
Inventor
Curtis A. Lavender
Vineet V. Joshi
Dean M. Paxton
Saumyadeep Jana
Glenn J. Grant
Darrell R. Herling
Richard W. Davies
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Battelle Memorial Institute Inc
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Battelle Memorial Institute Inc
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Priority to US14/222,468 priority Critical patent/US20140283574A1/en
Assigned to BATTELLE MEMORIAL INSTITUTE reassignment BATTELLE MEMORIAL INSTITUTE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GRANT, GLENN J., DAVIES, Richard W., HERLING, DARRELL R., JANA, SAUMYADEEP, JOSHI, VINEET V., LAVENDER, CURTIS A., PAXTON, DEAN M.
Assigned to U.S. DEPARTMENT OF ENERGY reassignment U.S. DEPARTMENT OF ENERGY CONFIRMATORY LICENSE (SEE DOCUMENT FOR DETAILS). Assignors: BATTELLE MEMORIAL INSTITUTE, PACIFIC NORTHWEST DIVISION
Publication of US20140283574A1 publication Critical patent/US20140283574A1/en
Priority to US15/351,201 priority patent/US10189063B2/en
Assigned to BATTELLE MEMORIAL INSTITUTE reassignment BATTELLE MEMORIAL INSTITUTE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: WHALEN, SCOTT A., GRANT, GLENN J., DARSELL, JENS T., JANA, SAUMYADEEP, JOSHI, VINEET V., LAVENDER, CURTIS A., OVERMAN, NICOLE R.
Priority to US15/898,515 priority patent/US10695811B2/en
Assigned to BATTELLE MEMORIAL INSTITUTE reassignment BATTELLE MEMORIAL INSTITUTE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: CATALINI, DAVID, DARSELL, JENS T., GRANT, GLENN J., JANA, SAUMYADEEP, JOSHI, VINEET V., LAVENDER, CURT A., WHALEN, SCOTT A.
Priority to US16/028,173 priority patent/US11045851B2/en
Assigned to BATTELLE MEMORIAL INSTITUTE reassignment BATTELLE MEMORIAL INSTITUTE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: JOSHI, VINEET V., LAVENDER, CURT A., DARSELL, JENS T., ROHATGI, AASHISH, GRANT, GLENN J., REZA-E-RABBY, MD., WHALEN, SCOTT A.
Priority to US16/562,314 priority patent/US11383280B2/en
Priority to US16/916,548 priority patent/US11517952B2/en
Priority to US17/033,854 priority patent/US20210053100A1/en
Priority to US17/035,597 priority patent/US20210197241A1/en
Priority to US17/175,464 priority patent/US11534811B2/en
Priority to US17/242,166 priority patent/US20210379638A1/en
Priority to US17/473,178 priority patent/US20210402471A1/en
Priority to US17/665,433 priority patent/US11684959B2/en
Priority to US17/826,054 priority patent/US20220297174A1/en
Priority to US17/874,140 priority patent/US20220371067A1/en
Priority to US17/957,207 priority patent/US20230042802A1/en
Priority to US17/984,144 priority patent/US20230088412A1/en
Priority to US17/985,611 priority patent/US20230081786A1/en
Priority to US18/093,636 priority patent/US20230150022A1/en
Priority to US18/121,563 priority patent/US20230234115A1/en
Priority to US18/426,042 priority patent/US20240216973A1/en
Abandoned legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C23/00Extruding metal; Impact extrusion
    • B21C23/002Extruding materials of special alloys so far as the composition of the alloy requires or permits special extruding methods of sequences
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C23/00Extruding metal; Impact extrusion
    • B21C23/21Presses specially adapted for extruding metal
    • B21C23/212Details
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C23/00Extruding metal; Impact extrusion
    • B21C23/21Presses specially adapted for extruding metal
    • B21C23/218Indirect extrusion presses
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C27/00Containers for metal to be extruded
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C29/00Cooling or heating work or parts of the extrusion press; Gas treatment of work
    • B21C29/003Cooling 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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  • Mechanical Engineering (AREA)
  • Extrusion Of Metal (AREA)

Abstract

An extrusion apparatus and process are disclosed that produce high-performance extrusion structures. The extrusion apparatus includes a shear tool that applies a rotational shear force and an axial extrusion force to the face of a billet material that plasticizes the billet material. Plasticized material is extruded through an extrusion die along the length of the inner bore of the shear tool which yields hollow and solid extrusion structures. The process refines the microstructures of the extrusion structures and extrusion materials.

Description

    CROSS REFERENCE TO RELATED APPLICATION
  • 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.
  • STATEMENT REGARDING RIGHTS TO INVENTION MADE UNDER FEDERALLY-SPONSORED RESEARCH AND DEVELOPMENT
  • 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.
  • FIELD OF 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.
  • BACKGROUND OF THE INVENTION
  • 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.
  • SUMMARY OF THE INVENTION
  • 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.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • 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 of FIG. 1.
  • FIG. 3B is an expanded view of the embodiment of FIG. 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.
  • DETAILED DESCRIPTION OF THE INVENTION
  • 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.
  • 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. In the instant embodiment, outer (top) die ring 14 and a lower die ring (described further in reference to FIG. 2) 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. During operation, 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. In the figure, 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. Mandrel 28 may direct flow of extruded billet materials along the length of inner bore 2. Extruded materials may release through an orifice 5 positioned, e.g., at a top end of shear tool 2. However, release is not limited thereto, as detailed further herein.
  • 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. In the figure, outer die ring 14 and lower die ring 16 couple together to form die chamber 10. In some embodiments, 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. In some embodiments, the container may also be a single component. In the figure, 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. A mandrel 28 described previously in reference to FIG. 2 may be positioned in chamber 10, which may insert to a selected depth in inner bore 4 of shear tool 2 during assembly through an optional spacer (e.g., a graphite spacer) 32 through billet 22 and through an orifice 5 of an extrusion die 11. Extrusion die 11 may be positioned at the billet end of shear 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, and billet 22 may be secured in chamber 10 by introducing locking keys (described previously) into key slots 20 positioned on respective sides of outer die ring 14 as described previously herein.
  • In operation, shear tool 2 when introduced into chamber 10 applies a rotational shear (shearing) force 26 and an axial extrusion force 24 to the face of billet material 22 at the shear tool/billet interface within die chamber 10. Rotational shear (shearing) force 26 assists or promotes plasticization of billet material 22. In some embodiments, rotational shear (shearing) force 26 may be applied by rotating the shear tool 2 at a selected rotation speed while keeping billet 22 stationary. In some embodiments, rotational shear (shearing) force 26 may be applied by rotating the billet 22 while keeping shear tool 2 stationary. In some embodiments, rotational shear (shearing) force 26 is applied by rotating shear tool 2 and billet 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 or cool billet material 22 positioned within chamber 10. Heating and cooling of billet material 22 can be used to assist deformation of billet 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 to billet 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 reduce extrusion 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 of shear tool 2. In the instant embodiment, plasticized material extrudes past 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 another orifice 5 positioned at the top end of shear tool 2.
  • FIG. 3B shows an expanded view of the die assembly 100 of FIG. 3A. As shown in the figure, 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.
  • FIG. 3C is a cross-sectional view of another embodiment of extrusion assembly 100 of a direct extrusion type. Die assembly 100 is shown in assembled form and also shows flow of plasticized billet material during extrusion operation. In the figure, die assembly 100 includes a billet rotation tool or device, e.g., die ring 16, configured to apply rotational shear force 26 to the billet material 22 positioned within die chamber 10. Billet material 22 may be in aligned contact with tool 2 or a die support. A mandrel 28 described previously in reference to FIG. 3A may be positioned in chamber 10, which may insert to a selected depth in inner bore 4 of shear tool 2 during assembly through an optional spacer (e.g., a graphite spacer) 32 through billet 22 and through an orifice (not shown) of extrusion die 11 positioned at the billet end of shear 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 an axial extrusion force 24 to the face of billet material 22 at the shear tool/billet interface within die chamber 10. Extrusion assembly 100 may further include an optional heater/cooler (not shown) described previously in reference to FIG. 3A. Application of axial extrusion force 24, rotational shear force 26, and/or heat or cooling to billet 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 the extrusion force 24 needed to extrude plasticized billet materials. Plasticized billet materials may flow downward from deformation region 34 and extrude through an orifice 5 of extrusion die 11 that is positioned at the billet end of tool 2 into inner bore 4. Plasticized billet materials may then flow through gap (FIG. 3B) formed between the external surface of mandrel 28 and the inner wall (not shown) of extrusion die 11. In the instant embodiment, plasticized material extrudes past 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 another orifice 5 positioned at the bottom end of tool 2.
  • FIG. 4 is a perspective view showing an exemplary configuration for shear tool 2. In the instant embodiment, shear tool 2 includes a scroll feature 38 positioned at an end (face) of shear 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
  • 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.
  • Extrusion Shapes
  • 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.
  • Process Parameters
  • 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
  • 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
  • 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.
  • Microstructure Refinement
  • 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.
  • Applications
  • 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)

What is claimed is:
1. A shear-assisted extrusion system for production of an extrusion structure, the system comprises:
a shear tool configured to simultaneously apply a rotational shearing force and an axial extrusion force to the face of a billet material at the shear tool/billet interface that plastically deforms the billet material, the shear tool includes an extrusion die with an orifice having a selected shape that extrudes the plasticized billet material that forms the extrusion structure with a selected shape at an axial extrusion force less than that required for extrusions performed absent the rotational shearing force.
2. The system of claim 1, wherein the extrusion die is configured to extrude the plasticized billet material along the length of an inner bore of the shear tool in response to the axial extrusion pressure applied to the face of the billet material.
3. The system of claim 1, further includes a mandrel configured to insert a selected depth into the inner bore of the shear tool during extrusion that allows plasticized material to flow past the mandrel along the length of the inner bore that yields a hollow extrusion structure.
4. The system of claim 3, wherein the mandrel is a fixed mandrel or a floating mandrel, or the extrusion die is a bridge die.
5. The system of claim 1, wherein the shear tool includes at least one surface feature disposed at an end thereof configured to engage the face of the billet during extrusion operation.
6. The system of claim 1, further includes a heating or a cooling device disposed to heat or cool the billet material.
7. The system of claim 1, wherein the system is configured to apply the shearing force at the shear tool/billet interface by rotation of the shear tool relative to a stationary billet, 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.
8. A shear-assisted extrusion process for production of an extrusion structure or product, the process comprising the steps of:
applying a rotational shearing force and an axial extrusion force to the face of the billet material with a shear tool at the shear tool/billet interface at a selected rotation speed to plastically deform the billet material; and
extruding the plasticized material through an orifice of an extrusion die of the shear tool that includes a selected shape to form the extrusion structure or product with a selected shape at an axial extrusion force less than that required for extrusions performed absent the rotational shearing force.
9. The process of claim 8, wherein the plasticized billet material extrudes 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.
10. The process of claim 8, further including introducing a mandrel into the inner bore of the ram tool to a selected depth such that the plasticized material extrudes through the orifice of the extrusion die past the mandrel along the length of the inner bore of the shear tool producing a hollow extrusion structure with a selected shape.
11. The process of claim 10, wherein the extrusion is performed with a fixed mandrel or a floating mandrel, or the extrusion is performed with a stationary bridge die.
12. The process of claim 8, wherein applying the rotational shear force includes engaging the billet material with the shear tool that includes a feature disposed at the end thereof.
13. The process of claim 8, wherein the extrusion structure includes a uniform inner wall thickness, a uniform inner dimension, and a selected shape; or a non-uniform inner wall thickness, a non-uniform inner dimension, and a selected shape.
14. The process of claim 8, wherein the process includes heating or cooling the billet material with a selected heating device and/or cooling device.
15. The process of claim 8, wherein the process includes heating the plasticized billet material with frictional heat generated during deformation of the billet material.
16. The process of claim 8, wherein extrusion of the plasticized billet material is performed at a temperature selected between about −196° C. and about 0° C.; or between about 0° C. and about 1000° C.; or greater.
17. The process of claim 8, wherein the rotational shear force is applied by rotating the billet at a selected rotational speed while keeping the shear tool stationary, by rotating the shear tool at a selected rotational speed while keeping the billet material stationary, or by rotating the shear tool at a selected rotational speed different than the rotational speed of the billet material or vice versa.
18. The process of claim 17, wherein the selected rotational speed is up to about 1000 revolutions-per-minute.
19. The process of claim 8, wherein the axial extrusion pressure is at or below about 50 MPa.
20. The process of claim 8, wherein the process includes altering the morphology of second-phase particles in the billet material from an aspect ratio above about 2 prior to extrusion to an aspect ratio below about 2 following extrusion.
21. The process of claim 8, wherein the process yields microstructure grains in the extrusion structure or product at least about one-half the size of the grains prior to extrusion.
22. The process of claim 8, wherein the process yields microstructure grains with a size less than or equal to about 10 microns, less than or equal to about 5 microns, or finer.
23. The process of claim 8, wherein the extrusion structure is a tubular extrusion structure included as a component of a compression device, a stent device, a bending resistant device, including combinations of these devices.
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US14/222,468 US20140283574A1 (en) 2013-03-22 2014-03-21 System and process for formation of extrusion structures
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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