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公开(公告)号:US10208238B2
公开(公告)日:2019-02-19
申请号:US14954518
申请日:2015-11-30
IPC分类号: C09K5/14 , B01J27/22 , C04B35/10 , C04B35/563 , C04B35/565 , C04B35/58 , C04B35/583 , C04B35/622 , C04B35/628 , C04B35/80 , C22C49/14 , D01F9/08
摘要: Methods of producing continuous (or discontinuous) boron carbide fibers. The method comprises reacting a continuous or discontinuous carbon fiber material and a boron oxide gas within a temperature range of from approximately 1400° C. to approximately 2200° C. Articles including such partially or fully converted fibers may be provided, including such reinforcing fibers in a matrix of ceramic (a CMC), in metal (a MMC), or other matrix (e.g., polymer, etc.).
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公开(公告)号:US20210269366A1
公开(公告)日:2021-09-02
申请号:US17179642
申请日:2021-02-19
IPC分类号: C04B35/622 , B82Y30/00 , C04B35/565 , C04B35/571 , C04B35/573 , C01B32/956
摘要: Methods of producing silicon carbide, and other metal carbide materials. The method comprises reacting a carbon material (e.g., fibers, or nanoparticles, such as powder, platelet, foam, nanofiber, nanorod, nanotube, whisker, graphene (e.g., graphite), fullerene, or hydrocarbon) and a metal or metal oxide source material (e.g., in gaseous form) in a reaction chamber at an elevated temperature ranging up to approximately 2400° C. or more, depending on the particular metal or metal oxide, and the desired metal carbide being produced. A partial pressure of oxygen in the reaction chamber is maintained at less than approximately 1.01×102 Pascal, and overall pressure is maintained at approximately 1 atm.
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公开(公告)号:US20180051396A1
公开(公告)日:2018-02-22
申请号:US15795619
申请日:2017-10-27
发明人: John E. Garnier
IPC分类号: D01F9/08 , C04B35/565 , C04B35/622 , C04B35/628 , C04B35/80 , D01F8/00 , C04B35/56 , C08K7/04 , D01F11/12
摘要: A method of producing, from a continuous or discontinuous (e.g., chopped) carbon fiber, partially to fully converted metal carbide fibers. The method comprises reacting a carbon fiber material with at least one of a metal or metal oxide source material at a temperature greater than a melting temperature of the metal or metal oxide source material (e.g., where practical, at a temperature greater than the vaporization temperature of the metal or metal oxide source material). Additional methods, various forms of carbon fiber, metal carbide fibers, and articles including the metal carbide fibers are also disclosed.
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公开(公告)号:US20190077718A1
公开(公告)日:2019-03-14
申请号:US16030145
申请日:2018-07-09
发明人: John E. Garnier
IPC分类号: C04B35/80 , C04B35/573 , C04B35/591 , C04B37/00
CPC分类号: C04B35/806 , C04B35/571 , C04B35/573 , C04B35/589 , C04B35/591 , C04B35/62863 , C04B35/62865 , C04B35/62868 , C04B35/62897 , C04B37/005 , C04B38/00 , C04B2111/00362 , C04B2111/00431 , C04B2111/00793 , C04B2111/00801 , C04B2111/0081 , C04B2111/00862 , C04B2235/383 , C04B2235/386 , C04B2235/3865 , C04B2235/3882 , C04B2235/524 , C04B2235/5244 , C04B2235/5248 , C04B2235/526 , C04B2235/5264 , C04B2235/5292 , C04B2235/5296 , C04B2235/5436 , C04B2235/767 , C04B2235/80 , C04B2235/9607 , C04B38/0061 , C04B38/0074
摘要: Ceramic composite materials that are reinforced with carbide fibers can exhibit ultra-high temperature resistance. For example, such materials may exhibit very low creep at temperatures of up to 2700° F. (1480° C.). The present composites are specifically engineered to exhibit matched thermodynamically stable crystalline phases between the materials included within the composite. In other words, the reinforcing fibers, a debonding interface layer disposed over the reinforcing fibers, and the matrix material of the composite may all be of the same crystalline structural phase (all hexagonal), for increased compatibility and improved properties. Such composite materials may be used in numerous applications.
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公开(公告)号:US20160122252A1
公开(公告)日:2016-05-05
申请号:US14954518
申请日:2015-11-30
CPC分类号: C09K5/14 , B01J27/22 , C04B35/10 , C04B35/563 , C04B35/565 , C04B35/58071 , C04B35/583 , C04B35/62277 , C04B35/6286 , C04B35/803 , C04B35/806 , C04B2235/46 , C04B2235/48 , C04B2235/5212 , C04B2235/5248 , C04B2235/5264 , C04B2235/79 , C22C49/14 , D01F9/08 , Y10T428/2916
摘要: Methods of producing continuous (or discontinuous) boron carbide fibers. The method comprises reacting a continuous or discontinuous carbon fiber material and a boron oxide gas within a temperature range of from approximately 1400° C. to approximately 2200° C. Articles including such partially or fully converted fibers may be provided, including such reinforcing fibers in a matrix of ceramic (a CMC), in metal (a MMC), or other matrix (e.g., polymer, etc.).
摘要翻译: 生产连续(或不连续)碳化硼纤维的方法。 该方法包括在约1400℃至约2200℃的温度范围内使连续或不连续的碳纤维材料和氧化硼气体反应。可以提供包括这种部分或全部转化的纤维的物品,包括这样的增强纤维 陶瓷(CMC),金属(MMC)或其它基体(例如聚合物等)的基质。
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公开(公告)号:US09803296B2
公开(公告)日:2017-10-31
申请号:US14615685
申请日:2015-02-06
发明人: John E. Garnier
IPC分类号: C04B41/45 , D01F9/08 , D01F8/00 , C08K7/04 , C04B35/56 , C04B35/565 , C04B35/622 , C04B35/628 , C04B35/80 , D01F11/12
CPC分类号: D01F9/08 , C04B35/56 , C04B35/565 , C04B35/62277 , C04B35/6286 , C04B35/62897 , C04B35/806 , C04B2235/32 , C04B2235/3201 , C04B2235/3203 , C04B2235/3206 , C04B2235/3208 , C04B2235/3217 , C04B2235/3224 , C04B2235/3225 , C04B2235/3227 , C04B2235/3229 , C04B2235/3232 , C04B2235/3239 , C04B2235/3241 , C04B2235/3244 , C04B2235/3251 , C04B2235/3256 , C04B2235/3258 , C04B2235/3262 , C04B2235/3272 , C04B2235/3409 , C04B2235/3418 , C04B2235/40 , C04B2235/402 , C04B2235/404 , C04B2235/405 , C04B2235/421 , C04B2235/428 , C04B2235/5248 , C04B2235/5252 , C04B2235/5264 , C04B2235/5284 , C04B2235/5292 , C08K7/04 , D01F8/00 , D01F11/123 , D01F11/127 , D10B2101/12 , D10B2101/14
摘要: A method of producing, from a continuous or discontinuous (e.g., chopped) carbon fiber, partially to fully converted metal carbide fibers. The method comprises reacting a carbon fiber material with at least one of a metal or metal oxide source material at a temperature greater than a melting temperature of the metal or metal oxide source material (e.g., where practical, at a temperature greater than the vaporization temperature of the metal or metal oxide source material). Additional methods, various forms of carbon fiber, metal carbide fibers, and articles including the metal carbide fibers are also disclosed.
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公开(公告)号:US20160265143A1
公开(公告)日:2016-09-15
申请号:US14615685
申请日:2015-02-06
发明人: John E. Garnier
CPC分类号: D01F9/08 , C04B35/56 , C04B35/565 , C04B35/62277 , C04B35/6286 , C04B35/62897 , C04B35/806 , C04B2235/32 , C04B2235/3201 , C04B2235/3203 , C04B2235/3206 , C04B2235/3208 , C04B2235/3217 , C04B2235/3224 , C04B2235/3225 , C04B2235/3227 , C04B2235/3229 , C04B2235/3232 , C04B2235/3239 , C04B2235/3241 , C04B2235/3244 , C04B2235/3251 , C04B2235/3256 , C04B2235/3258 , C04B2235/3262 , C04B2235/3272 , C04B2235/3409 , C04B2235/3418 , C04B2235/40 , C04B2235/402 , C04B2235/404 , C04B2235/405 , C04B2235/421 , C04B2235/428 , C04B2235/5248 , C04B2235/5252 , C04B2235/5264 , C04B2235/5284 , C04B2235/5292 , C08K7/04 , D01F8/00 , D01F11/123 , D01F11/127 , D10B2101/12 , D10B2101/14
摘要: A method of producing, from a continuous or discontinuous (e.g., chopped) carbon fiber, partially to fully converted metal carbide fibers. The method comprises reacting a carbon fiber material with at least one of a metal or metal oxide source material at a temperature greater than a melting temperature of the metal or metal oxide source material (e.g., where practical, at a temperature greater than the vaporization temperature of the metal or metal oxide source material). Additional methods, various forms of carbon fiber, metal carbide fibers, and articles including the metal carbide fibers are also disclosed.
摘要翻译: 从连续或不连续(例如切碎的)碳纤维生产部分地完全转化的金属碳化物纤维的方法。 该方法包括使碳纤维材料与金属或金属氧化物源材料中的至少一种在大于金属或金属氧化物源材料的熔融温度的温度下反应(例如,在实际情况下,在大于蒸发温度的温度下 的金属或金属氧化物源材料)。 还公开了另外的方法,各种形式的碳纤维,金属碳化物纤维和包括金属碳化物纤维的制品。
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公开(公告)号:US09272913B2
公开(公告)日:2016-03-01
申请号:US14570927
申请日:2014-12-15
CPC分类号: C01B31/36 , B82Y30/00 , C01B32/956 , C04B35/565 , C04B35/571 , C04B35/573 , C04B35/62281 , C04B35/806 , C04B2235/428 , C04B2235/46 , C04B2235/48 , C04B2235/5244 , C04B2235/5248 , C04B2235/526 , C04B2235/5264 , C04B2235/5284 , C04B2235/5445 , C04B2235/616 , C04B2235/72 , C04B2235/767 , Y10T428/249924 , Y10T428/249928 , Y10T428/24993 , Y10T428/249974 , Y10T428/2918 , Y10T428/292 , Y10T428/2933 , Y10T428/2958 , Y10T428/2964 , Y10T428/2967 , Y10T428/2975
摘要: Methods of producing silicon carbide fibers. The method comprises reacting a continuous carbon fiber material and a silicon-containing gas in a reaction chamber at a temperature ranging from approximately 1500° C. to approximately 2000° C. A partial pressure of oxygen in the reaction chamber is maintained at less than approximately 1.01×102 Pascal to produce continuous alpha silicon carbide fibers. Continuous alpha silicon carbide fibers and articles formed from the continuous alpha silicon carbide fibers are also disclosed.
摘要翻译: 生产碳化硅纤维的方法。 该方法包括使反应室中的连续碳纤维材料和含硅气体在约1500℃至约2000℃的温度下反应。反应室中氧的分压保持在小于约 1.01×102帕斯卡,以生产连续的α碳化硅纤维。 还公开了连续的α碳化硅纤维和由连续的α碳化硅纤维形成的制品。
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公开(公告)号:US10954167B1
公开(公告)日:2021-03-23
申请号:US16261246
申请日:2019-01-29
IPC分类号: C04B35/565 , C04B35/622 , B82Y30/00 , C04B35/571 , C04B35/573 , C04B35/80 , C01B32/956
摘要: Methods of producing silicon carbide, and other metal carbide materials. The method comprises reacting a carbon material (e.g., fibers, or nanoparticles, such as powder, platelet, foam, nanofiber, nanorod, nanotube, whisker, graphene (e.g., graphite), fullerene, or hydrocarbon) and a metal or metal oxide source material (e.g., in gaseous form) in a reaction chamber at an elevated temperature ranging up to approximately 2400° C. or more, depending on the particular metal or metal oxide, and the desired metal carbide being produced. A partial pressure of oxygen in the reaction chamber is maintained at less than approximately 1.01×102 Pascal, and overall pressure is maintained at approximately 1 atm.
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公开(公告)号:US10793478B2
公开(公告)日:2020-10-06
申请号:US16030145
申请日:2018-07-09
发明人: John E. Garnier
IPC分类号: C04B35/80 , C04B35/573 , C04B35/591 , C04B37/00 , C04B35/628 , C04B35/571 , C04B38/00 , C04B35/589 , C04B111/00
摘要: Ceramic composite materials that are reinforced with carbide fibers can exhibit ultra-high temperature resistance. For example, such materials may exhibit very low creep at temperatures of up to 2700° F. (1480° C.). The present composites are specifically engineered to exhibit matched thermodynamically stable crystalline phases between the materials included within the composite. In other words, the reinforcing fibers, a debonding interface layer disposed over the reinforcing fibers, and the matrix material of the composite may all be of the same crystalline structural phase (all hexagonal), for increased compatibility and improved properties. Such composite materials may be used in numerous applications.
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