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1. 发明授权

US09540716B2 Composite powder of carbide/blending metal 有权
标题翻译：复合粉末的碳化物/混合金属
公开(公告)号：US09540716B2
公开(公告)日：2017-01-10
申请号：US14592658
申请日：2015-01-08
申请人： INDUSTRIAL TECHNOLOGY RESEARCH INSTITUTE
发明人： Chi-San Chen , Chih-Chao Yang , Lik-Hang Chau , Ching-Chang Hsieh , Yen-Yu Hou
IPC分类号： C22C29/06 , C22C29/08 , C22C29/10 , C22C49/11 , B22F3/105 , C22C49/06 , C22C49/08 , C22C49/02 , C22C49/14 , B33Y70/00
CPC分类号： C22C29/08 , B22F3/1055 , B33Y70/00 , C22C29/06 , C22C29/067 , C22C29/10 , C22C49/02 , C22C49/06 , C22C49/08 , C22C49/11 , C22C49/14 , Y02P10/295
摘要： A composite powder is provided. The composite powder comprises 80-97 wt % of carbide and 3-20 wt % of blending metal powder comprising cobalt and a first metal powder, wherein the first metal powder is formed of one of aluminum, titanium, iron, nickel, or a combination thereof, and the amount of cobalt is 90-99% of total blending metal powder.
摘要翻译：提供复合粉末。复合粉末包含80-97重量％的碳化物和3-20重量％的包含钴和第一金属粉末的共混金属粉末，其中第一金属粉末由铝，钛，铁，镍或组合中的一种形成钴的总量为共混金属粉末的90-99％。

2. 发明授权

US09320602B2 Compressed fiber structural material and method for producing the same 有权
标题翻译：压缩纤维结构材料及其制造方法
公开(公告)号：US09320602B2
公开(公告)日：2016-04-26
申请号：US14345668
申请日：2012-03-09
申请人： Noboru Nakayama , Masaomi Horita , Naoki Izawa , Hiroto Tamai , Naoto Saito , Yuki Usui , Nobuhide Ogihara
发明人： Noboru Nakayama , Masaomi Horita , Naoki Izawa , Hiroto Tamai , Naoto Saito , Yuki Usui , Nobuhide Ogihara
IPC分类号： A61F2/28 , C22C49/11 , B22F3/00 , C22F1/18 , A61L27/04
CPC分类号： A61F2/28 , A61F2002/2835 , A61F2310/00023 , A61F2310/00425 , A61L27/04 , B22F3/002 , C22C49/11 , C22F1/183
摘要： Provided is a method for easily producing a lamellar compressed fiber structural material which has mechanical characteristics close to those of in vivo bone and which is capable of easily increasing osteoblast even when a difference in strength exists. In order to solve the issues, the method for producing compressed fiber structural material 1, includes: a step of preparing biocompatible fiber 14 having an average diameter of 5 μm-50 μm and an aspect ratio of 20-500; and a step of molding compressed fiber structural material 1 by cold pressing/shearing biocompatible fiber 14, compressed fiber structural material 1 having an average pore diameter that is in the range of 60 μm-100 μm inclusive and a void fraction that is in the range of 25%-50% inclusive, both obtained by measurement in accordance with the mercury penetration method. Further, it is preferable for the cold pressing/shearing is performed by controlling a compressive pressure in the range of 200 MPa-2000 MPa, a shearing stroke length in the range of 0.2 mm-5 mm and a shearing velocity in the range of 0.5 mm/min-5 mm/min.
摘要翻译：本发明提供一种容易制造层状压缩纤维结构材料的方法，其具有接近体内骨的机械特性，并且即使存在强度差也能够容易地增加成骨细胞。为了解决这些问题，制造压缩纤维结构材料1的方法包括：制备平均直径为5μm〜50μm，长径比为20-500的生物相容性纤维14的工序; 以及通过冷压/剪切生物相容性纤维14成型压缩纤维结构材料1的步骤，平均孔径在60μm-100μm范围内的压缩纤维结构材料1和在该范围内的空隙率为25％-50％，均为根据汞渗透法测量得到的。此外，优选通过将压缩压力控制在200MPa〜2000MPa，剪切行程长度在0.2mm-5mm范围内，剪切速度在0.5的范围内进行冷压/剪切 mm / min-5mm / min。

3. 发明授权

US09096034B2 Syntactic metal matrix materials and methods 有权
标题翻译：句法金属基体材料及方法
公开(公告)号：US09096034B2
公开(公告)日：2015-08-04
申请号：US13445810
申请日：2012-04-12
申请人： Andrew J. Sherman , Brian Doud
发明人： Andrew J. Sherman , Brian Doud
IPC分类号： B32B5/18 , B21D31/00
CPC分类号： B22F3/1112 , B21D31/00 , B32B5/16 , B32B5/18 , B32B5/20 , C22C32/0036 , C22C32/0078 , C22C49/00 , C22C49/06 , C22C49/11
摘要： A syntactic metal foam composite that is substantially fully dense except for syntactic porosity is formed from a mixture of ceramic microballoons and matrix forming metal. The ceramic microballoons have a uniaxial crush strength and a much higher omniaxial crush strength. The mixture is continuously constrained while it is consolidated. The constraining force is less than the omniaxial crush strength. The substantially fully dense syntactic metal foam composite is then constrained and deformation worked at a substantially constant volume. The deformation working is typically performed at a yield strength that is adjusted by way of selecting a working temperature at which the yield strength is approximately less than the omniaxial crush strength of the included ceramic microballoons. This deformation causes at least work hardening and grain refinement in the matrix metal.
摘要翻译：由陶瓷微球和基体形成金属的混合物形成除了手征孔隙之外基本上完全致密的复合金属泡沫复合材料。陶瓷微球具有单轴挤压强度和更高的全向挤压强度。混合物在固结时不断受到限制。约束力小于全向挤压强度。然后基本上完全致密的复合金属泡沫复合材料被约束并以基本恒定的体积进行变形。变形加工通常以屈服强度进行，该屈服强度通过选择屈服强度近似小于所包含的陶瓷微球的全向挤压强度的工作温度进行调整。该变形至少导致基体金属中的加工硬化和晶粒细化。

4. 发明申请

US20130149183A1 HIGH-STRENGTH TITANIUM ALLOY MEMBER AND PRODUCTION METHOD FOR SAME 审中-公开
标题翻译：高强度钛合金会员及其生产方法
公开(公告)号：US20130149183A1
公开(公告)日：2013-06-13
申请号：US13817087
申请日：2011-08-15
申请人： Yuji Araoka , Tohru Shiraishi , Yoshiki Ono
发明人： Yuji Araoka , Tohru Shiraishi , Yoshiki Ono
IPC分类号： C22C14/00 , B22F1/00
CPC分类号： C22C14/00 , B22F1/004 , B22F1/0081 , B22F1/0088 , B22F3/14 , B22F3/24 , B22F2003/248 , C22C47/14 , C22C49/11 , C22F1/183 , C23C8/02 , C23C8/24 , C23C8/80
摘要： A production method for a titanium alloy member includes preparing a titanium alloy material for sintering as a raw material of a sintered body; nitriding the titanium alloy material for sintering, thereby forming a nitrogen compound layer and/or a nitrogen solid solution layer in a surface layer of the titanium alloy material for sintering and yielding a nitrogen-containing titanium alloy material for sintering; mixing the titanium alloy material for sintering and the nitrogen-containing titanium alloy material for sintering, thereby yielding a titanium alloy material for sintering mixed with nitrogen-containing titanium alloy material; sintering the titanium alloy material for sintering mixed with nitrogen-containing titanium alloy material, thereby bonding the material each other and dispersing nitrogen contained in the nitrogen-containing titanium alloy material for sintering in a condition in which nitrogen is uniformly dispersed into an entire inner portion of the sintered body by solid solution.
摘要翻译：钛合金构件的制造方法包括制备用于烧结的钛合金材料作为烧结体的原料; 对用于烧结的钛合金材料进行氮化，从而在用于烧结的钛合金材料的表面层中形成氮化合物层和/或氮固溶体层，并产生用于烧结的含氮钛合金材料; 混合用于烧结的钛合金材料和用于烧结的含氮钛合金材料，从而产生用含氮钛合金材料混合的烧结钛合金材料; 烧结用于与含氮钛合金材料混合的钛合金材料，从而将材料彼此粘合并将氮气均匀分散在氮气均匀分散的条件中分散在整个内部的状态下分散在用于烧结的含氮钛合金材料中的氮的固体溶液。

5. 发明申请

US20100143691A1 HIGH HEAT CONDUCTION COMPOSITE MATERIAL 有权
标题翻译：高导热复合材料
公开(公告)号：US20100143691A1
公开(公告)日：2010-06-10
申请号：US12595397
申请日：2008-03-06
申请人： Kazuaki Katagiri , Akiyuki Shimizu , Terumitsu Imanishi , Toyohiro Sato , Nobuhito Nakama , Atsushi Kakitsuji , Katsuhiko Sasaki
发明人： Kazuaki Katagiri , Akiyuki Shimizu , Terumitsu Imanishi , Toyohiro Sato , Nobuhito Nakama , Atsushi Kakitsuji , Katsuhiko Sasaki
IPC分类号： B32B5/02
CPC分类号： C22C47/025 , B32B5/30 , B32B2262/106 , B32B2264/105 , B32B2264/107 , B32B2307/302 , B32B2307/306 , B32B2307/714 , B32B2457/00 , B82Y30/00 , B82Y40/00 , C01B32/15 , C04B35/111 , C04B35/486 , C04B35/5607 , C04B35/5611 , C04B35/5626 , C04B35/565 , C04B35/58014 , C04B35/58071 , C04B35/58078 , C04B35/581 , C04B35/587 , C04B35/645 , C04B35/803 , C04B35/806 , C04B35/83 , C04B2235/5248 , C04B2235/526 , C04B2235/5264 , C04B2235/5268 , C04B2235/5272 , C04B2235/5288 , C04B2235/666 , C04B2235/9607 , C22C47/14 , C22C49/02 , C22C49/06 , C22C49/08 , C22C49/11 , C22C49/14 , Y10S977/742 , Y10S977/776 , Y10S977/777 , Y10T428/139 , Y10T428/1393 , Y10T428/1397 , Y10T428/249927 , Y10T428/249928 , Y10T428/249929 , Y10T428/24995
摘要： A composite material being excellent in heat conductivity is provided. In order to realize this, a fibrous carbon material made of fine tube form structures constituted with single-layer or multiple-layer graphene is present to form a plurality of layers within a substrate made from a spark plasma sintered body of a metal powder, a mixed powder of a metal and ceramics, or a ceramic powder. The fibrous carbon material constituting each layer is made of a mixture obtained by mixing a small amount of a small diameter fiber 2 having an average diameter of 100 nm or less with a large diameter fiber 1 having an average diameter of 500 nm to 100 μm.
摘要翻译：提供导热性优异的复合材料。为了实现这一点，存在由由单层或多层石墨烯构成的细管形结构体制成的纤维状碳材料，在由金属粉末的火花等离子体烧结体制成的基板内形成多个层，金属和陶瓷的混合粉末，或陶瓷粉末。构成各层的纤维状碳材料由平均直径为100nm以下的少量小直径纤维2与平均直径为500nm〜100μm的大直径纤维1混合而成的混合物构成。

6. 发明授权

US07588179B2 Bonding of carbon fibers to metal inserts for use in composites 失效
标题翻译：将碳纤维粘合到用于复合材料的金属嵌件上
公开(公告)号：US07588179B2
公开(公告)日：2009-09-15
申请号：US11730373
申请日：2007-03-30
申请人： Allen H. Simpson , Mark L. La Forest , Alexander Mukasyan , Douglas J. Steinke
发明人： Allen H. Simpson , Mark L. La Forest , Alexander Mukasyan , Douglas J. Steinke
IPC分类号： B23K31/02
CPC分类号： B29C70/70 , B29C70/683 , B29K2063/00 , B29K2705/12 , B29K2707/04 , C22C47/14 , C22C49/11 , C22C49/14
摘要： Resin-impregnated carbon fiber composites containing metal inserts. Carbon fibers or a carbon fiber preform are bonded to a metal structural member. Once the carbon fiber-metal bond is established, the fiber-metal assembly or hybrid preform is impregnated with resin, to form an article in which bonding between the metal structural member and the composite remainder of the article is greatly enhanced. In a process embodiment, a metal insert, e.g. a steel insert, is provided in contact with particulate carbide-forming metal, e.g. titanium, and with carbon fiber segments. Then an electric current is passed through the carbide-forming metal particles and carbon fibers to heat them to a temperature above the melting point of the carbide-forming metal. This initiates an exothermic reaction, which forms liquid phase metal carbide. Subsequently the liquid phase metal carbide is cooled and solidified, thereby bonding the carbon fiber segments to the metal insert.
摘要翻译：含有金属插入物的树脂浸渍碳纤维复合材料。碳纤维或碳纤维预成型体结合到金属结构件上。一旦建立了碳纤维 - 金属粘结剂，纤维 - 金属组件或混合预型体就被树脂浸渍，形成一种制品，其中金属结构件与制品的复合材料的其余部分之间的粘合得到极大的提高。在工艺实施例中，金属插入件，例如，提供与插入颗粒状碳化物的金属接触的钢插件。钛和碳纤维段。然后使电流通过碳化物形成金属颗粒和碳纤维，将其加热到高于碳化物形成金属的熔点的温度。这引发了一种形成液相金属碳化物的放热反应。随后将液相金属碳化物冷却并固化，从而将碳纤维段粘合到金属插入物上。

7. 发明申请

US20080069716A1 MICRON SIZE POWDERS HAVING NANO SIZE REINFORCEMENT 有权
标题翻译：具有纳米尺寸增强的麦克风尺寸粉末
公开(公告)号：US20080069716A1
公开(公告)日：2008-03-20
申请号：US11531771
申请日：2006-09-14
申请人： Bhanumathi Chelluri , Edward Arlen Knoth , Edward John Schumaker , Ryan D. Evans , James. L. Maloney
发明人： Bhanumathi Chelluri , Edward Arlen Knoth , Edward John Schumaker , Ryan D. Evans , James. L. Maloney
IPC分类号： B22F3/12
CPC分类号： C22C1/1084 , B22F1/0014 , B22F1/02 , B22F2009/043 , B22F2998/10 , C22C32/0047 , C22C32/0084 , C22C47/14 , C22C49/11 , B22F9/04 , B22F3/02 , B22F3/10
摘要： An improved sintered material and product. A nanometer size reinforcement powder is mixed with a micron size titanium or titanium alloy powder. After the reinforcement powder is generally uniformly dispersed, the powder mixture is compacted and sintered, causing the nano reinforcement to react with the titanium or titanium alloy, producing a composite material containing nano and micron size precipitates that are uniformly distributed throughout the material.
摘要翻译：一种改进的烧结材料和产品。将纳米尺寸的增强粉末与微米级的钛或钛合金粉末混合。在增强粉末通常均匀分散后，粉末混合物被压实和烧结，导致纳米增强材料与钛或钛合金反应，产生均匀分布在整个材料中的纳米和微米级沉淀物的复合材料。

8. 发明授权

US06949216B2 Rapid manufacturing of carbon nanotube composite structures 有权
标题翻译：碳纳米管复合结构的快速制造
公开(公告)号：US06949216B2
公开(公告)日：2005-09-27
申请号：US10000917
申请日：2001-10-24
申请人： Craig A. Brice , Frederick J. Herman
发明人： Craig A. Brice , Frederick J. Herman
IPC分类号： B22F3/00 , B29C70/12 , B29C70/38 , C04B35/80 , C22C1/10 , C22C49/14 , B29C41/02 , B23K26/00 , B22F1/00
CPC分类号： B22F1/00 , B22F3/1055 , B29C64/153 , B29C70/12 , B29C70/305 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y70/00 , B33Y80/00 , B82Y30/00 , C04B35/803 , C22C1/10 , C22C47/14 , C22C49/11 , C22C49/12 , C22C49/14 , C22C2026/002 , Y02P10/295 , Y10S977/89 , Y10T428/12486 , Y10T428/249927 , Y10T428/249928 , Y10T428/2918
摘要： A system for fabricating a free form structure of a composite material including carbon nanotubes. The system includes a discharge assembly and a composite formation device operatively linked with the discharge assembly. The discharge assembly dispenses a fusing agent such as for example a high energy density emission, a laser emission or a particle beam emission. The composite formation device includes a composite generator and an arranger in operative engagement with a composite generator. The composite generator engages with the fusing agent so as to create a composite nodal element. The composite nodal element includes a matrix and a multiplicity of fibers formed of carbon nanotubes dispersed throughout the matrix. The arranger positions one node relative to another to define the free form structure.
摘要翻译：一种用于制造包括碳纳米管的复合材料的自由形式结构的系统。该系统包括排出组件和与排出组件可操作地连接的复合成形装置。放电组件分配熔化剂，例如高能量密度发射，激光发射或粒子束发射。复合材料形成装置包括复合发生器和与复合发电机操作性接合的装配器。复合发生器与定影剂接合以形成复合节点元件。复合节点元件包括基体和分布在整个基体中的碳纳米管形成的多根纤维。编排者将一个节点相对于另一个节点定位自由形式结构。

9. 发明申请

US20020053257A1 Rapid manufacturing of carbon nanotube composite structures 有权
标题翻译：碳纳米管复合结构的快速制造
公开(公告)号：US20020053257A1
公开(公告)日：2002-05-09
申请号：US10000917
申请日：2001-10-24
申请人： Lockheed Martin Corporation
发明人： Craig A. Brice , Frederick J. Herman
IPC分类号： B22F001/00 , C08L001/00 , C08J003/00 , C04B035/00 , C22C032/00 , B22F003/00 , C22C001/00 , B29C035/04
CPC分类号： B22F1/00 , B22F3/1055 , B29C64/153 , B29C70/12 , B29C70/305 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y70/00 , B33Y80/00 , B82Y30/00 , C04B35/803 , C22C1/10 , C22C47/14 , C22C49/11 , C22C49/12 , C22C49/14 , C22C2026/002 , Y02P10/295 , Y10S977/89 , Y10T428/12486 , Y10T428/249927 , Y10T428/249928 , Y10T428/2918
摘要： A system for fabricating a free form structure of a composite material including carbon nanotubes. The system includes a discharge assembly and a composite formation device operatively linked with the discharge assembly. The discharge assembly dispenses a fusing agent such as for example a high energy density emission, a laser emission or a particle beam emission. The composite formation device includes a composite generator and an arranger in operative engagement with a composite generator. The composite generator engages with the fusing agent so as to create a composite nodal element. The composite nodal element includes a matrix and a multiplicity of fibers formed of carbon nanotubes dispersed throughout the matrix. The arranger positions one node relative to another to define the free form structure.
摘要翻译：一种用于制造包括碳纳米管的复合材料的自由形式结构的系统。该系统包括排出组件和与排出组件可操作地连接的复合成形装置。放电组件分配熔化剂，例如高能量密度发射，激光发射或粒子束发射。复合材料形成装置包括复合发生器和与复合发电机操作性接合的装配器。复合发生器与定影剂接合以形成复合节点元件。复合节点元件包括基体和分布在整个基体中的碳纳米管形成的多根纤维。编排者将一个节点相对于另一个节点定位自由形式结构。

10. 发明授权

US5271776A Asymmetrical method for hiping filament reinforced annular objects 失效
标题翻译：髋部长丝增强环形物体的不对称方法
公开(公告)号：US5271776A
公开(公告)日：1993-12-21
申请号：US842685
申请日：1992-02-27
申请人： Paul A. Siemers , Stephen F. Rutkowski
发明人： Paul A. Siemers , Stephen F. Rutkowski
IPC分类号： B30B5/02 , B21K1/76 , B23P6/00 , C22C47/00 , C22C47/16 , C22C47/18 , C22C49/11 , C22C49/12 , B32B15/14
CPC分类号： B23P6/002 , B21K1/761 , C22C47/16 , C22C49/11 , C22C49/12 , Y10T29/49801 , Y10T29/49982
摘要： A method for asymmetrically consolidating a ring structure having a filamentary reinforcement embedded in a plasma sprayed deposited matrix is taught. The method involves fabricating a filament reinforced plasma sprayed deposit matrix structure and asymmetrically consolidating the structure. The asymmetric consolidation is accomplished by placing a thicker and/or stronger can surface on the outer portions of the ring structure and a thinner and/or weaker can structure on the inner and side surfaces of the reinforced ring structure. The HIPing of the reinforced ring structure with the asymmetric can results in a preferential compaction of the ring from the inside toward the outside and avoids the buckling of and damage to the reinforcement filaments on the outer portions of the structure.
摘要翻译：教导了一种用于不对称地固结嵌入等离子体喷镀的基体中的具有丝状增强材料的环结构的方法。该方法包括制造长丝增强等离子体喷涂沉积基质结构并且不对称地固结结构。非对称固结通过在环结构的外部部分上放置更厚和/或更强的罐表面以及在增强环结构的内表面和侧表面上更薄和/或更弱的罐结构来实现。具有不对称性的加强环结构的HIPing可以导致环从内向外的优先压实，并避免结构外部的增强细丝的翘曲和损坏。

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