Classifications

• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B33—ADDITIVE MANUFACTURING TECHNOLOGY
  • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
  • B33Y10/00—Processes of additive manufacturing
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
  • B22F3/10—Sintering only
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
  • B22F3/10—Sintering only
  • B22F3/11—Making porous workpieces or articles
  • B22F3/1146—After-treatment maintaining the porosity
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
  • B22F1/05—Metallic powder characterised by the size or surface area of the particles
  • B22F1/052—Metallic powder characterised by the size or surface area of the particles characterised by a mixture of particles of different sizes or by the particle size distribution
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
  • B22F1/09—Mixtures of metallic powders
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
  • B22F10/10—Formation of a green body
  • B22F10/14—Formation of a green body by jetting of binder onto a bed of metal powder
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
  • B22F3/10—Sintering only
  • B22F3/1035—Liquid phase sintering
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
  • B22F3/10—Sintering only
  • B22F3/11—Making porous workpieces or articles
  • B22F3/1103—Making porous workpieces or articles with particular physical characteristics
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
  • B22F3/24—After-treatment of workpieces or articles
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F9/00—Making metallic powder or suspensions thereof
  • B22F9/02—Making metallic powder or suspensions thereof using physical processes
  • B22F9/06—Making metallic powder or suspensions thereof using physical processes starting from liquid material
  • B22F9/08—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying
  • B22F9/082—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B33—ADDITIVE MANUFACTURING TECHNOLOGY
  • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
  • B33Y70/00—Materials specially adapted for additive manufacturing
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C33/00—Making ferrous alloys
  • C22C33/02—Making ferrous alloys by powder metallurgy
  • C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
  • C22C33/0278—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
  • B22F10/30—Process control
  • B22F10/34—Process control of powder characteristics, e.g. density, oxidation or flowability
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F9/00—Making metallic powder or suspensions thereof
  • B22F9/02—Making metallic powder or suspensions thereof using physical processes
  • B22F9/06—Making metallic powder or suspensions thereof using physical processes starting from liquid material
  • B22F9/08—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying
  • B22F9/082—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid
  • B22F2009/0824—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid with a specific atomising fluid
  • B22F2009/0828—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid with a specific atomising fluid with water
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F2301/00—Metallic composition of the powder or its coating
  • B22F2301/35—Iron
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F2302/00—Metal Compound, non-Metallic compound or non-metal composition of the powder or its coating
  • B22F2302/10—Carbide
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F2304/00—Physical aspects of the powder
  • B22F2304/10—Micron size particles, i.e. above 1 micrometer up to 500 micrometer
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
  • B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
  • B22F2998/10—Processes characterised by the sequence of their steps
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B33—ADDITIVE MANUFACTURING TECHNOLOGY
  • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
  • B33Y80/00—Products made by additive manufacturing
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
  • Y02P10/00—Technologies related to metal processing
  • Y02P10/25—Process efficiency

Definitions

• Various embodiments relate generally to additive manufacturing of metal parts, and more particularly to binder jet additive manufacturing of metal parts.
• Binder Jetting Additive Manufacturing (BJAM) process is also known for prototyping of polymer materials and for the production of sand cores for the casting industry.
• Metallic components are also produced by BJAM, at low sintered densities, requiring infiltration of parts after sintering.
• Slurry pump impellers are an example of application of this technology.
• One or more non-limiting embodiments utilize BJAM and sintering to facilitate the manufacture of complex shapes, with good wear resistant microstructures and high hardness levels. According to various of these embodiments, the design freedom and material properties offer advantages over conventional processing.
• Additive Manufacturing typically requires expensive specialized iron powders (e.g., gas atomized iron powders).
• one or more non-limiting embodiments use readily available low cost water atomized grades.
• One or more non-limiting embodiments provides a method of manufacturing a metallic component by BJAM printing a powder blend of water atomized base iron powder and a at least one master ferroalloy powder to form a printed part, and super solidus sintering the printed part to form the metallic component.
• the method also includes, before said printing, blending the water atomized base iron powder with the at least one master ferroalloy powder to form the powder blend.
• the water atomized base iron powder comprises pure or prealloyed grade iron powder.
• the sintering densifies the metallic component.
• the metallic component comprises a high strength metallic component.
• the ferroalloy comprises a transition element.
• the transition element comprises
• the at least one master ferroalloy powder comprises between 5 and 10 wt% carbon.
• the at least one master ferroalloy powder has a D50 particle size of less than 45 um.
• the water atomized base iron powder has a D50 particle size of less than 40 um.
• the water atomized base iron powder has a D50 particle size of between 70 and l30um.
• the powder blend has a total alloy content of between 15 and 35 wt %.
• the powder blend has a carbon content of between 2 and 5 wt %.
• said printing comprises curing and depowdering to form the printed part.
• the printed part has a porosity of
• the metallic component has a porosity of less than 10%.
• said sintering occurs at temperatures between 1100 and l400°C.
• said sintering causes linearly shrinks the printed part by 15-25%.
• a microstructure of the metallic component contains carbide phase portions embedded in a matrix, wherein the matrix is softer than the carbide phase portions.
• the carbide phase portions have a micro hardness of 1000-1700 HV0.1.
• the matrix has a micro hardness of
• the method upon completion of said sintering, the metallic component has a hardness of 30-50 HRC.
• the method also includes, after said sintering, heat treating the metallic component, wherein said heat treating increases a hardness of the metallic component.
• the metallic component contains carbide phase portions embedded in a martensitic matrix.
• the metallic component after said heat treating, has a hardness of at least 50 HRC.
• the metallic component after said heat treating, has a hardness of 55-65 HRC.
• the carbide phase portions have a micro hardness of 1000-1700 HV0.1.
• the matrix has a micro hardness of
• the metallic component after said heat treating, has a wear resistance so as to have a volume loss of less than or equal to 100 mm 3 according to ASTM G65-10 procedure A.
• One or more embodiments provide a metallic component manufactured by: binder jet additive manufacture printing a powder blend to form a printed part; and super solidus sintering the printed part to form the metallic component.
• the powder blend comprises a blend of water atomized base iron powder and at least one master ferroalloy powder.
• One or more embodiments facilitates the manufacture of complexly shaped ferrous alloy components to high densities, hardnesses, and toughnesses without the need for secondary operations to achieve the net desired component shape and size.
• the BJAM printing process facilitates new low volume markets for complex, tough, hard components.
• All closed-ended (e.g., between A and B) and open-ended (greater than C) ranges of values disclosed herein explicitly include all ranges that fall within or nest within such ranges.
• a disclosed range of 1-10 is understood as also disclosing, among other ranges, 2-10, 1-9, 3-9, etc.
• the embodiments disclosed herein explicitly include combinations of any value within the disclosed range of one parameter (e.g., parameter C) with any value within the disclosed range of any other parameter (e.g., parameter D).
• FIG. 1 is a flowchart illustrating various methods of manufacturing metallic components according to alternative embodiments.
• FIG. 2 is an illustrative Fe-C phase diagram.
• FIG. 3 is a perspective drawing of a metallic component made in accordance with one or more of the manufacturing methods shown in FIG. 1.
• FIG. 1 is a flowchart illustrating various methods of manufacturing metallic components according to alternative embodiments. Steps 1A-5A provide manufacturing steps for a non-heat treated component 160, while steps 1B-6B provide manufacturing steps for a heat-treated component 200.
• step 1A/1B base iron powder and/or a prealloyed base iron powder 100 is blended with a master alloy powder 110 to form a powder blend 120.
• the base iron powder 100 comprises at least 10,
• the iron powder 100 comprises a standard, low-cost, WA iron powder.
• the WA iron powder 100 has a D40, D45, D50, D55, D60, D65, D70, D75, and/or D80 particle size of (a) less than 150, 140, 130, 125, 120, 115, 110, 105, 100, 95, 90, 85, 80, 70, 65, 60, 55, 50, 45, 40, 35, and/or 30 urn, (b) more than 20, 25, 30, 35, 40, 45, 50, 55, 60, 65, 70, 75, 80, 85, 90, 95, and/or 100 um, and/or (c) between any two such values (e.g., a D50 particle size of between 20 and 150 um, 25 and 40 um, and/or 90 and 110 um; a D60 particle size of between 20 and 150 um, 25 and 40 um, and/or 90 and 110 um).
• the master alloy powder 110 comprises at least one ferroalloy powder that includes ferrous powder with a high alloy and high carbon content.
• the alloy material of the master alloy powder 110 comprises one or more transition elements typically used in steel and cast iron metallurgy, including but not limited to, Cr, Mn, Mo, V, W, Ni, and/or Cu.
• the master alloy powder 110 may comprise one or more ferroalloys such as ferromanganese (FeMn), ferrochromium (FeCr), ferrovanadium (FeV), and/or ferromolybdenum (FeMo).
• the master alloy powder 110 comprises a mixture of one or more of these ferroalloys (including any and all combinations of these ferroalloys).
• the master alloy powder 110 comprises a mixture of the FeMn Powder Blend (discussed below) and FeCr Powder Blend
• the master alloy powder 110 has a carbon content of (a) at least 2, 3, 4, 5, 6, 7, 8, 9, and/or 10 wt %, (b) less than 14, 13, 12, 11, 10, 9, 8, 7, 6, 5, 4, 3, 2, and/or 1 wt %, and/or (c) between any two such values (e.g., between 2 and 14 wt %, between 5 and 10 wt%).
• the use of ferroalloys with high carbon content facilitates effective BJAM printing of the alloy powder 110 so as to facilitate BJAM introduction of the included carbon into the printed component 130.
• the ferroalloys thus function as an effective BJAM printable carrier for carbon so as to increase the carbon content of the printed component 130.
• the master alloy powder 110 has a D40, D50,
• the master alloy powder 110 comprises 6.53% C
• this master alloy powder is referred to as FeMn Powder Blend (despite the fact that this powder comprises additional components).
• the master alloy powder 110 comprises
• this master alloy powder is referred to as FeCr Powder Blend (despite the fact that this powder comprises additional components).
• the master alloy powder 110 comprises
• the master alloy powder 110 comprises about 97% FeCr Powder Blend and about 3% FeMn Powder Blend.
• any ratio of such Powder Blends may be used for the master alloy powder 110, e.g., at least 1, 2, 3, 4, 5, 10, 15, 20, 30, 40, 50, 60, 70, 80, 85, 90, 95, 96, 97, 98, and/or 99% FeCr
• Powder Blend and/or at least 1, 2, 3, 4, 5, 10, 15, 20, 30, 40, 50, 60, 70, 80, 85, 90, 95, 96, 97, 98, and/or 99% FeMn Powder Blend.
• the base iron powder 100 may be blended with the master alloy powder 110 in a variety of combinations to tailor the powder blend 120 as appropriate to achieve specific application property requirements. According to various embodiments
• base iron powder 100 content of the powder blend 120 is (a) at least 45, 50, 55, 60, 65, 70, 75, 80, and/or 85%, (b) less than 95, 90, 85, 80, 75, 70, 65, 60, 55, 50, 45, 40, and/or 35%, and/or (c) between any two such values (e.g., between 45 and 95%, between 55 and 65%, between 75 and 85%).
• the master alloy powder 110 content of the powder blend 120 is (a) less than 65, 60, 55, 50, 45, 40, 35, 30, 25, 20, and/or 15%, (b) greater than 5, 10, 15, 20, 25, 30, 35, 40, 45, 50, 55, 60, and/or 65 %, and/or (c) between any two such values (e.g., between 5 and 65%, between 35 and 45%, between 25 and 35%).
• the powder blend 120 has a total non-Fe alloy content (i.e., the cumulative content of the non-iron components of the powder blend 120 (e.g., including Cr, Mn, Mo, C, etc.)) of at least 5, 10, 15, 20, 25 wt %, less than 50, 45, 40, 35, 30 wt %, and/or between any two such values (e.g., between 5 and 50 wt %, between 10 and 45 wt %, between 15 and 35 wt %).
• a total non-Fe alloy content i.e., the cumulative content of the non-iron components of the powder blend 120 (e.g., including Cr, Mn, Mo, C, etc.) of at least 5, 10, 15, 20, 25 wt %, less than 50, 45, 40, 35, 30 wt %, and/or between any two such values (e.g., between 5 and 50 wt %, between 10 and 45 wt %, between 15 and 35 wt %).
• the total iron content of the powder blend 120 may comprise (a) at least 50, 55, 60, 65, 70, 75, 80, 85, 90, and/or 95% Fe, (b) less than 5, 10, 15, 20, and/or 25% Fe, and/or (c) any value between any two such upper and lower values (e.g., between 50 and 95 % Fe, between 55 and 90 % Fe, between 65 and 85 % Fe).
• the blend powder 120 has a carbon content of (a) at least 1, 2, 2.5, 3, 3.5, and/or 4 wt %, (b) less than 6, 5.5, 5, 4.5, 4, 3.5, 3, 2.5, 2, and/or 1 wt %, and/or (c) between any two such values (e.g., between 2 and 5 wt %, between 2 and 3.5 wt%).
• the blended powder 120 comprises about 20% FeCr alloy Powder (e.g., 28% Fe, 60% Cr, 9% C), 20% FeMn alloy Powder Blend (e.g., 17% Fe, 75% Mn, 6%C), and about 60% base iron powder 100.
• E2132 comprises about 3.05 % C, 15 % Mn, 12 % Cr, 0.84 % Si, and about 70 % Fe.
• blend code According to an alternative embodiment (hereinafter referred to as blend code
• the blend powder 120 comprises about 30% FeCr Powder, 1% FeMn Powder, and about 69% base iron powder 100. According to various embodiments, after sintering, E2138 comprises about 2.7 % C, 0.75 % Mn, 18.1 % Cr, 0.83 % Si, and about 78 % Fe. [0062] According to various embodiments, the powder blend 120 comprises 11-30% Cr, 0-
• Nr 2.5% Nr, 0-18% Mn, 0-3% Mo, 0-1.2% Cu, 2-5% C, 0-3% V, and the balance being Fe and unavoidable impurities.
• the blend powder 120 is BJAM printed into a printed 3D component
• carbon is introduced into the component 130 via the carbon content of the master alloy powder 110, rather than through elemental carbon (e.g., graphite).
• this avoids the difficult process of BJAM printing elemental carbon (e.g., graphite) and/or avoids having to modify the WA iron powder to have a higher carbon content. It would be difficult or impossible to simply blend elemental carbon into the powder to be printed because elemental carbon (graphite) is very fine (e.g., 5-15 um) and dusty and would not blend well or flow and spread.
• adding carbon as a master alloy form allows blending and spreading in the powder bed.
• a density of the green component 140 is (a) at least 30%, 35%, 40%, 45%, 50%, 55%, and/or 60%, (b) less than 65%, 60%, 55%, 50%, 45%, and/or 40%, and/or (c) between any two such values (e.g., between 30 and 65%, between 30 and 60%, between 35 and 55%, between 40 and 60%).
• a density of the green component 140 is a function of the particle size distribution of the powder blend 120, and is relatively close to an apparent density of the powder blend 120 (e.g., ranging from 3 g/cc to 4 g/cc according to various non-limiting embodiments).
• the green component 140 is super solidus sintered to form a sintered component 150.
• Super solidus sintering results in a combination of liquid and solid phases being present at different percentages.
• the liquid phase material helps to shrink and densify the component, while the solid phase material helps to maintain the component’s shape and avoid slumping.
• the super solidus sintering occurs at
• the sintering temperature is selected to correspond to the super solidus temperature of constituents of the component 140 (i.e., the super solidus range based on the phase diagram of the component 140). As the sintering temperature increases, carbon diffuses until locally it forms a liquid phase, which promotes interdiffusion of alloy elements with iron. At the top temperature, there remains a percentage of liquid phase which accelerates further particle consolidation and sintering, pore rounding, densification, and homogenization of carbon and alloys.
• the sintering temperature may be balanced to increase liquid phase material, while maintaining sufficient solid phase material to maintain the component’s shape.
• the sintering occurs in the shaded super solidus temperature zone shown in FIG. 2.
• the phase diagram in FIG. 2 is for Fe-C only, and is provided for illustration purposes only. The addition of alloys (e.g., transition metals) will modify the phase diagram of the actual alloy powder.
• the sintering shrinks and densifies the green component 140 so as to create a sintered component 150 with a density of (a) at least 80, 81, 82, 83, 84, 85, 86, 87, 88, 89, 90, 91, and/or 92%, (b) less than 100, 99, 98, 97, 96, 95, 94, 93, and/or (c) between any two such values (e.g., between 80 and 99%, between 85 and 95%, between 90 and 95%).
• such density is achieved without post-sintering infiltration of material.
• the sintering results in linear shrinkage of the green component 150 of (a) at least 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, and/or 30%, (b) less than 40, 35, 34, 33, 32, 31, 30, 29, 28, 27, 26, 25, 24, 23, 22, 21, 20, 19, and/or 18%, and/or (c) between any two such values (e.g., between 15 and 40%, between 20 and 27 %, between 15 and 25%).
• the sintered metallic component 150 is finished (e.g., via machining, polishing, etc.) to form the non-heat-treated final metallic component 160.
• the finishing step is omitted, and the sintered metallic component 150 is the final metallic component.
• the component 160 has a hardness of (a) at least
• 25, 30, 35, 40, and/or 45 HRC (b) less than 55, 50, 45, 40, and/or 35 HRC, and/or (c) between any two such values (e.g., between 25 and 55 HRC, between 30 and 50 HRC, between 35 and 45 HRC).
• the component 160 has a microstructure that contains relatively hard carbide phase portions embedded in an austenite matrix that is softer than the carbide phase portions. According to various embodiments, the component 160 has a good combination of wear resistance and toughness. According to various embodiments, the carbide phase portions have a micro hardness of 1000-1700 HV0.1, and the matrix has a micro hardness of 250-800 HV0.1 and/or 250-350 HV0.1.
• the powder blend 120 is E2132
• the sintering occurs at around 1 l80°C and results in about 23% linear shrinkage
• the post-sintering (e.g., non- heat treated) hardness of the component 160 is about 37.0 HRC
• a micro hardness of the carbide phase portions is about 1089 HV0.1
• a micro hardness of the matrix e.g., austenite
• TRS Transverse Rupture Strength
• the sintered metallic component 150 may be heat treated (e.g., hardening, quenching).
• the sintered metallic component 150 may be finished/machined prior to the heat treatment step 5B. According to various embodiments, such finishing/machining is easier to do prior to the heat treatment. The finishing/machining may be done to conform the component 150 to the desired shape and tolerances of the final component 200.
• the heat-treated metallic component is finished to form a final, heat- treated metallic component 200.
• the finishing step is omitted, and the heat-treated metallic component is the final metallic component.
• the component 200 has a microstructure that contains hard carbide phase portions embedded in a hard martensitic matrix. According to various embodiments, the component has superior wear resistance and high hardness. According to various embodiments, the carbide phase portions of the component 200 have a micro hardness of 1000-1700 HV0.1. According to various embodiments, the matrix of the component 200 has a micro hardness of 600-800 HV0.1. According to various embodiments, after said heat treating, the metallic component 200 has a wear resistance so as to have a volume loss of less than or equal to 100 mm 3 according to ASTM G65-10 procedure A.
• the component 200 has a hardness of (a) at least
• 40, 45, 50, 55, and/or 60 HRC (b) less than 80, 75, 70, 65, and/or 60 HRC, and/or (c) between any two such values (e.g., between 40 and 80 HRC, between 50 and 60 HRC, between 55 and 65 HRC).
• the powder blend 120 is E2138
• the sintering occurs at around l300°C and results in a density of about 7.50 g/cc
• the sintered component 150 is heat treated via neutral hardening
• the post-heat-treated hardness of the component 200 is about 60 HRC
• a micro hardness of the carbide phase portions is about 1550 HV0.1
• a micro hardness of the martensitic matrix is about 690 HV0.1.
• the E2138 powder blend 120 may alternatively be used in a process that omits a heat treatment step to provide a final metallic component 160 made from E2138 with carbide phase embedded in a ferritic/pearlitic matrix.
• the components 150, 160, 200 may comprise components of a rock drill (e.g., a rifle nut 210 (see FIG. 3), a splined nut, a rifle piston, a chuck, etc.), including, without limitation, any of the components of the rock drill disclosed in El.S. Patent Nos. 3,055,441 or 2,061,807, the entire contents of both of which are hereby incorporated by reference herein.
• the components 150, 160, 200 may comprise one or more components of a slurry pump (e.g., rotor, vane, impeller, pump housing, volute), including, without limitation, any of the components of the slurry pump disclosed in U.S. Patent No. 5,797,724, which is hereby incorporated herein in its entirety.

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• 2019
  • 2019-05-09 EP EP19799218.3A patent/EP3790693A4/en not_active Withdrawn
  • 2019-05-09 JP JP2020557207A patent/JP2021526584A/ja active Pending
  • 2019-05-09 KR KR1020207035426A patent/KR20210040283A/ko not_active Abandoned
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