RAPID SYNTHESIS OF SILICON CARBIDE-CARBON COMPOSITES
    1.
    发明申请
    RAPID SYNTHESIS OF SILICON CARBIDE-CARBON COMPOSITES 有权
    快速合成碳化碳复合材料

    公开(公告)号:US20100032286A1

    公开(公告)日:2010-02-11

    申请号:US12533706

    申请日:2009-07-31

    IPC分类号: C25B1/00

    摘要: Production of pore-free carbon/carbon-silicon carbide composite materials with mechanical properties making them suitable for use in such applications as the production of aircraft landing system brake components including brake discs. The method includes: providing a porous carbon-carbon composite preform; surrounding the porous carbon-carbon composite preform with silicon powder to form an intermediate construct; applying a uniaxial load to the construct; applying direct electrical current to an assembly containing the loaded construct of porous carbon-carbon preform surrounded by silicon powder, thereby melting the silicon powder and infiltrating the pores of the carbon-carbon preform with liquid silicon; and initiating a combustion-type reaction between the silicon and carbon in the preform, thereby forming silicon carbide in the preform.

    摘要翻译: 生产具有机械性能的无孔碳/碳 - 碳化硅复合材料,使其适用于诸如生产飞机着陆系统制动部件(包括制动盘)的应用。 该方法包括:提供多孔碳 - 碳复合预型体; 用硅粉围绕多孔碳 - 碳复合预制件以形成中间构件; 对结构施加单轴载荷; 将直流电流施加到包含由硅粉包围的多孔碳 - 碳预制件的负载构造物的组件上,由此熔化硅粉末并用液态硅渗透碳 - 碳预型体的孔隙; 并在预成型件中引发硅和碳之间的燃烧型反应,从而在预成型件中形成碳化硅。

    Rapid synthesis of silicon carbide-carbon composites
    2.
    发明授权
    Rapid synthesis of silicon carbide-carbon composites 有权
    快速合成碳化硅 - 碳复合材料

    公开(公告)号:US09321692B2

    公开(公告)日:2016-04-26

    申请号:US12533706

    申请日:2009-07-31

    摘要: Production of pore-free carbon/carbon-silicon carbide composite materials with mechanical properties making them suitable for use in such applications as the production of aircraft landing system brake components including brake discs. The method includes: providing a porous carbon-carbon composite preform; surrounding the porous carbon-carbon composite preform with silicon powder to form an intermediate construct; applying a uniaxial load to the construct; applying direct electrical current to an assembly containing the loaded construct of porous carbon-carbon preform surrounded by silicon powder, thereby melting the silicon powder and infiltrating the pores of the carbon-carbon preform with liquid silicon; and initiating a combustion-type reaction between the silicon and carbon in the preform, thereby forming silicon carbide in the preform.

    摘要翻译: 生产具有机械性能的无孔碳/碳 - 碳化硅复合材料,使其适用于诸如生产飞机着陆系统制动部件(包括制动盘)的应用。 该方法包括:提供多孔碳 - 碳复合预型体; 用硅粉围绕多孔碳 - 碳复合预制件以形成中间构件; 对结构施加单轴载荷; 将直流电流施加到包含由硅粉包围的多孔碳 - 碳预制件的负载构造物的组件上,由此熔化硅粉末并用液态硅渗透碳 - 碳预型体的孔隙; 并在预成型件中引发硅和碳之间的燃烧型反应,从而在预成型件中形成碳化硅。

    Bonding of carbon fibers to metal inserts for use in composites
    3.
    发明授权
    Bonding of carbon fibers to metal inserts for use in composites 失效
    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

    IPC分类号: B23K31/02

    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。

    Bonding of carbon fibers to metal inserts for use in composites
    4.
    发明申请
    Bonding of carbon fibers to metal inserts for use in composites 失效
    将碳纤维粘合到用于复合材料的金属嵌件上

    公开(公告)号:US20080283174A1

    公开(公告)日:2008-11-20

    申请号:US11730373

    申请日:2007-03-30

    IPC分类号: B32B38/00 B32B37/06

    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。

    Synthesis of orthopaedic implant materials
    8.
    发明授权
    Synthesis of orthopaedic implant materials 失效
    矫形植入材料的合成

    公开(公告)号:US06896846B1

    公开(公告)日:2005-05-24

    申请号:US10284435

    申请日:2002-10-31

    摘要: A method for synthesis of biomedical alloys has been developed based on combustion phenomena. This low pressure combustion synthesis (LPCS) technique may be used for production of Co-based and other metal-based alloys, which cover the entire range of orthopaedic implants, including total hip and knee replacements, as well as hone screws, plates, and wires. A unique aspect of the method is that combustion synthesis under low ambient gas pressure allows one to produce pore-free (>99% theoretical density) alloys with high purity and precise chemical and phase compositions.

    摘要翻译: 已经基于燃烧现象开发了合成生物医药合金的方法。 这种低压燃烧合成(LPCS)技术可用于生产Co基和其他金属基合金,其覆盖整个矫形植入物的范围,包括全髋关节和膝关节置换术,以及螺钉,板和 电线 该方法的独特之处在于,在低环境气体压力下的燃烧合成允许生产具有高纯度和精确化学和相组成的无孔(> 99%理论密度)合金。

    Bonding of carbon-carbon composites using titanium carbide
    10.
    发明授权
    Bonding of carbon-carbon composites using titanium carbide 有权
    使用碳化钛粘结碳 - 碳复合材料

    公开(公告)号:US07858187B2

    公开(公告)日:2010-12-28

    申请号:US11391255

    申请日:2006-03-29

    IPC分类号: B32B9/00

    摘要: Method of joining carbon-carbon composite pieces together, e.g. in the refurbishment of aircraft brake discs. The method includes the steps of: providing a first carbon-carbon composite piece and a second carbon-carbon composite piece, wherein the second carbon-carbon composite piece has a surface that is complementary to a surface of said first carbon-carbon composite piece; providing a layer of a mixture of titanium powder and carbon powder on the first complementary mating surface; arranging the second carbon-carbon composite piece on the powder layer such that the second complementary mating surface is matched to the first complementary mating surface, thereby forming a construct of the first carbon-carbon composite piece, the powder layer, and the second carbon-carbon composite piece; placing the construct into a press and applying pressure to the construct to press together the two pieces joined at their complementary surfaces; and applying an electrical current to the powder in the construct to initiate an oxidation-reduction reaction, thereby bonding the carbon-carbon composite pieces together.

    摘要翻译: 将碳 - 碳复合材料片连接在一起的方法,例如 在飞机制动盘的翻新。 该方法包括以下步骤:提供第一碳 - 碳复合片和第二碳 - 碳复合片,其中所述第二碳 - 碳复合片具有与所述第一碳 - 碳复合片的表面互补的表面; 在第一互补配合表面上提供钛粉末和碳粉末的混合物层; 将第二碳 - 碳复合片布置在粉末层上,使得第二互补配合表面与第一互补配合表面匹配,由此形成第一碳 - 碳复合片,粉末层和第二碳 - 碳复合片的构造, 碳复合片; 将构造物放置在压力机中并向构件施加压力以将在其互补表面处接合的两个块压在一起; 并向构件中的粉末施加电流以引发氧化还原反应,从而将碳 - 碳复合材料片粘合在一起。