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公开(公告)号:US11685983B2
公开(公告)日:2023-06-27
申请号:US16504621
申请日:2019-07-08
申请人: Terves, LLC
发明人: Andrew J. Sherman , Nicholas Farkas
IPC分类号: C23F1/06 , C22C23/00 , C22F1/06 , C21D10/00 , B82Y30/00 , E02D27/38 , C22C23/02 , C22C49/04 , B22D27/00 , B22D27/08 , B22D19/14 , B22D27/11 , C22C1/03 , B22D27/02 , C22C23/06 , C22C26/00 , C22C1/04 , B22D21/00 , C22C47/08 , B22D25/06 , B22D23/06 , B22D21/04 , C22C49/02 , B22F1/062 , C22C1/10
CPC分类号: C22F1/06 , B22D19/14 , B22D21/007 , B22D21/04 , B22D23/06 , B22D25/06 , B22D27/00 , B22D27/02 , B22D27/08 , B22D27/11 , B82Y30/00 , C21D10/00 , C22C1/03 , C22C1/0408 , C22C23/00 , C22C23/02 , C22C23/06 , C22C26/00 , C22C47/08 , C22C49/04 , E02D27/38 , B22F1/062 , B22F2998/10 , B22F2999/00 , C22C1/1047 , C22C49/02 , C22C2026/002 , B22F2999/00 , C22C47/08 , B22F2202/01 , B22F2999/00 , C22C1/0408 , C22C2026/002 , B22F2998/10 , C22C1/1047 , B22F1/054 , B22F2998/10 , C22C1/1047 , B22F1/0547 , B22F2998/10 , C22C1/1047 , B22F1/0551 , B22F2998/10 , B22F1/0551 , C22C1/1047 , B22F2998/10 , B22F1/0547 , C22C1/1047 , B22F2998/10 , B22F1/054 , C22C1/1047
摘要: A castable, moldable, or extrudable magnesium-based alloy that includes one or more insoluble additives. The insoluble additives can be used to enhance the mechanical properties of the structure, such as ductility and/or tensile strength. The final structure can be enhanced by heat treatment, as well as deformation processing such as extrusion, forging, or rolling, to further improve the strength of the final structure as compared to the non-enhanced structure. The magnesium-based composite has improved thermal and mechanical properties by the modification of grain boundary properties through the addition of insoluble nanoparticles to the magnesium alloys. The magnesium-based composite can have a thermal conductivity that is greater than 180 W/m-K, and/or ductility exceeding 15-20% elongation to failure.
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公开(公告)号:US11788172B1
公开(公告)日:2023-10-17
申请号:US18316300
申请日:2023-05-12
发明人: Zhiyong You , Aoxue Jiang
CPC分类号: C22C1/1068 , C22C1/1005 , C22C1/1047 , C22C23/02
摘要: Disclosed is a preparation method of a magnesium matrix composite reinforced with SiC particles, belonging to the technical field of metallurgical materials, including the following steps: (1) carrying out oxidation pretreatment on SiC particles; (2) laying a piece of magnesium alloy on a bottom, laying a layer of oxidized SiC particles, then repeating a laying operation of a layer of magnesium alloy and a layer of SiC particles until the magnesium alloy and the SiC particles are completely laid, introducing inert gases, heating and melting, then performing cinder scrapping; (3) cooling to a semisolid temperature of the magnesium alloys for semisolid mechanical stirring, heating, and mechanically stirring again; (4) cooling again to the semisolid temperature of the magnesium alloys, then casting into a blank; and (5) heating the blank to the semisolid temperature of the magnesium alloys and extruding to obtain the magnesium matrix composite reinforced with SiC particles.
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公开(公告)号:US20240102132A1
公开(公告)日:2024-03-28
申请号:US18255599
申请日:2021-12-03
申请人: ME Global Inc.
发明人: Aaron James Garland , Joaquin Aguilar Santillan , Antony Pieter , Shayne Allen Berns , Mark Dexter Hines , Ricardo Rodrigo Leiva lllanes , Benjamin Zimmerman , Daniel William Ruffelle
CPC分类号: C22C1/1068 , B22D19/0081 , C22C1/1047 , C22C29/005 , C22C29/12 , C22C33/00 , C22C33/006
摘要: A metal matrix composite to high tolerate wear as a property has been produced by infiltration casting of a Fe Alloy and a spinel ceramic by using a material design for i) metal transport phenomena conditions, ii) predefined wetting and capillarity and iii) processing child insert/mother casting methodology to produce a final casting in shape and form to meet the needs of a mining end user.
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4.
公开(公告)号:US20240117470A1
公开(公告)日:2024-04-11
申请号:US18542502
申请日:2023-12-15
发明人: Shengqiang MA , Ping LV , Xudong CUI , Yusheng LIU , Xuebin HE , Jiaxu CHEN , Jiankang ZHANG , Jiandong XING , Wenmin NIU
CPC分类号: C22C18/04 , B21C23/002 , C22C1/1047 , C22C32/0068
摘要: A high-thermal conductivity composite material is AlNp/ZA27 composite material, including 2%, 4%, 6%, or 8% by volume of aluminum nitride (AlN) ceramic particles and zinc-aluminium-27 (ZA27) alloy. The ZA27 alloy includes 70.52-71.08% by weight of Zn, 25.58˜27.65% by weight of Al, 1.27˜3.45% by weight of Cu, and 0.50% or less by weight of Mg. In the preparation of the high-thermal conductivity composite material, an as-cast AlNp/ZA27 composite material is subjected to homogenizing annealing and reciprocating extrusion.
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公开(公告)号:US11852415B2
公开(公告)日:2023-12-26
申请号:US17287724
申请日:2018-10-24
IPC分类号: F27D27/00 , C22C1/10 , C22C32/00 , F27D3/18 , F27D3/08 , F27D13/00 , F16D65/16 , F16D65/12 , F16D65/02 , F27D3/00
CPC分类号: F27D27/00 , C22C1/1036 , C22C32/0063 , F16D65/125 , F27D3/08 , F27D3/18 , F27D13/00 , C22C1/1047 , F16D2065/1308 , F16D2200/003 , F16D2200/0047 , F27D2003/0006 , F27D2003/0054 , F27D2003/0083
摘要: A system of obtaining an aluminium melt including SiC particles for use when moulding vehicle parts, e.g. brake disks, the system comprises a pre-processing tank (2), configured to receive SiC particles and to apply a pre-processing procedure to pre-process the SiC particles; a SiC particle transport member (4) configured to transport the pre-processed SiC particles from the pre-processing tank (2) to a crucible (6) of a melting furnace device (8), and the melting furnace device (8) is configured to receive and melt solid aluminium, e.g. aluminium slabs, and to hold an aluminium melt (10) and to receive said pre-processed SiC particles (12). The system also comprises a tube-like SiC particle mixing arrangement (14) defining and enclosing an elongated mixing chamber (16), the mixing arrangement (14) is configured to be mounted in said crucible (6) and structured to receive into said mixing chamber (16) said pre-processed SiC particles (12) via a first inlet (18) and said aluminium melt (10) via at least one second inlet (20), and to apply a mixing procedure by rotating a rotatable mixing member (22) arranged in said mixing chamber (16) about said longitudinal axis A, wherein said pre-processed SiC particles are mixed together with the aluminium melt in said mixing chamber. The mixing arrangement (14) is provided with at least one outlet (26) to feed out the mixture from said mixing chamber into said crucible.
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公开(公告)号:US11674208B2
公开(公告)日:2023-06-13
申请号:US16826561
申请日:2020-03-23
申请人: Terves, LLC
发明人: Andrew J. Sherman , Nicholas Farkas
IPC分类号: C22C23/00 , C22F1/06 , C21D10/00 , B82Y30/00 , E02D27/38 , C22C23/02 , C22C49/04 , B22D27/00 , B22D27/08 , B22D19/14 , B22D27/11 , C22C1/03 , B22D27/02 , C22C23/06 , C22C26/00 , C22C1/04 , B22D21/00 , C22C47/08 , B22D25/06 , B22D23/06 , B22D21/04 , C22C49/02 , B22F1/062 , C22C1/10
CPC分类号: C22F1/06 , B22D19/14 , B22D21/007 , B22D21/04 , B22D23/06 , B22D25/06 , B22D27/00 , B22D27/02 , B22D27/08 , B22D27/11 , B82Y30/00 , C21D10/00 , C22C1/03 , C22C1/0408 , C22C23/00 , C22C23/02 , C22C23/06 , C22C26/00 , C22C47/08 , C22C49/04 , E02D27/38 , B22F1/062 , B22F2998/10 , B22F2999/00 , C22C1/1047 , C22C49/02 , C22C2026/002 , B22F2999/00 , C22C47/08 , B22F2202/01 , B22F2999/00 , C22C1/0408 , C22C2026/002 , B22F2998/10 , C22C1/1047 , B22F1/054 , B22F2998/10 , C22C1/1047 , B22F1/0547 , B22F2998/10 , C22C1/1047 , B22F1/0551
摘要: A castable, moldable, or extrudable magnesium-based alloy that includes one or more insoluble additives. The insoluble additives can be used to enhance the mechanical properties of the structure, such as ductility and/or tensile strength. The final structure can be enhanced by heat treatment, as well as deformation processing such as extrusion, forging, or rolling, to further improve the strength of the final structure as compared to the non-enhanced structure. The magnesium-based composite has improved thermal and mechanical properties by the modification of grain boundary properties through the addition of insoluble nanoparticles to the magnesium alloys. The magnesium-based composite can have a thermal conductivity that is greater than 180 W/m-K, and/or ductility exceeding 15-20% elongation to failure.
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