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91. 发明授权

US08136642B2 Brake disk with intermediate layer 有权
标题翻译：具有中间层的制动盘
公开(公告)号：US08136642B2
公开(公告)日：2012-03-20
申请号：US11589807
申请日：2006-10-31
申请人： Andreas Kienzle , Ingrid Kratschmer
发明人： Andreas Kienzle , Ingrid Kratschmer
IPC分类号： F16D65/10
CPC分类号： F16D69/02 , B32B18/00 , C04B35/573 , C04B35/6267 , C04B35/62863 , C04B35/62873 , C04B35/62878 , C04B35/806 , C04B35/83 , C04B2235/383 , C04B2235/428 , C04B2235/48 , C04B2235/5248 , C04B2235/526 , C04B2235/5268 , C04B2235/9607 , C04B2237/363 , C04B2237/365 , C04B2237/38 , C04B2237/385 , C04B2237/70 , F16D65/12 , F16D69/023 , F16D2065/132
摘要： Carbon-ceramic brake disks that comprise several layers, whereby at least one layer is used as a bearing element and at least one layer acts as a friction layer, whereby the bearing element and at least one friction layer are separated by an intermediate layer, characterized in that the intermediate layer has reinforcement fibers in the form of fiber bundles, whereby the fiber bundles are encased by a layer that consists of a mixture of silicon carbide, silicon and carbon, which can be obtained by heat treatment of a mixture that consists of silicon powder and a carbonized resin or carbonized pitch at a temperature of 900° C. up to 1700° C. in an environment devoid of oxidizing agents. A process for their manufacture and use, in particular in automotive brake systems.
摘要翻译：碳陶瓷制动盘包括几层，其中使用至少一层作为轴承元件，并且至少一层用作摩擦层，由此轴承元件和至少一个摩擦层由中间层分离，其特征在于中间层具有纤维束形式的增强纤维，由此纤维束被由碳化硅，硅和碳的混合物组成的层包围，该层可以通过热处理由硅粉末和碳化树脂或碳化沥青，在900℃至1700℃的温度下，在没有氧化剂的环境中。其制造和使用的过程，特别是在汽车制动系统中。

92. 发明授权

US08101272B1 Armor shell and fabrication methods 有权
标题翻译：装甲壳和制作方法
公开(公告)号：US08101272B1
公开(公告)日：2012-01-24
申请号：US11901360
申请日：2007-09-17
申请人： Wayde R. Schmidt
发明人： Wayde R. Schmidt
IPC分类号： B32B9/00 , B32B27/04 , B32B27/12 , B32B17/12 , B32B18/00
CPC分类号： C04B35/573 , B33Y80/00 , C04B35/62272 , C04B35/62281 , C04B35/62873 , C04B35/62876 , C04B35/62878 , C04B35/62884 , C04B2235/5244 , C04B2235/5248 , C04B2235/5264 , C04B2235/614 , C04B2235/656 , C04B2235/6562 , C04B2235/6565 , C04B2235/6586 , F41H5/0414 , Y10S428/911 , Y10T29/49826 , Y10T428/24983 , Y10T428/249924 , Y10T428/249928 , Y10T428/249929 , Y10T428/24994 , Y10T428/249945 , Y10T428/24995 , Y10T428/2918 , Y10T428/2933 , Y10T428/30
摘要： A refractory ceramic composite for an armor shell, comprising a ceramic core that is formable to replicate a portion of a three dimensional surface, e.g., of an aircraft, to provide ballistic protection. A method of making a shell of refractory ceramic armor capable of conforming to the geometry is provided. The shell is formed by forming a mold to replicate the surface area; arranging a ceramic core on the mold; and removing the mold to leave said ceramic core, and heat treating the ceramic core to a desired hardness. The ceramic core is in the shape of the surface area.
摘要翻译：一种用于铠装壳的耐火陶瓷复合材料，包括可形成以复制例如飞行器的三维表面的一部分的陶瓷芯，以提供防弹。提供了一种制造能够符合几何形状的耐火陶瓷装甲壳的方法。壳体通过形成模具来复制表面区域而形成; 在模具上布置陶瓷芯; 并移除模具以离开所述陶瓷芯，并将陶瓷芯热处理成所需的硬度。陶瓷芯是表面积的形状。

93. 发明授权

US08057880B2 Non-oxide selectively porous materials 有权
标题翻译：非氧化物选择性多孔材料
公开(公告)号：US08057880B2
公开(公告)日：2011-11-15
申请号：US11969543
申请日：2008-01-04
申请人： Miklos P. Petervary , Min Zhou Berbon
发明人： Miklos P. Petervary , Min Zhou Berbon
IPC分类号： B32B3/24
CPC分类号： B32B38/04 , B26F1/24 , B32B18/00 , B32B2038/047 , C04B35/571 , C04B35/806 , C04B2235/5244 , C04B2235/5248 , C04B2237/365 , C04B2237/38 , C04B2237/385 , C04B2237/561 , C04B2237/62 , Y10S425/037 , Y10T428/24322 , Y10T428/24339 , Y10T428/249969 , Y10T428/249981
摘要： A process for providing pores in a structure and a structure according to any selected physical characteristics. Generally pins or pore forming members may be positioned in a laminate preform and the laminate preform formed into a laminate structure including the pins therein. The pins generally include a size, density, distribution, angle, or other characteristic that is desired in the final laminate structure. After the laminate is formed the pins are then removed from the laminate according to a process which does not harm selected physical characteristics of the laminate structure.
摘要翻译：根据任何选定的物理特性在结构和结构中提供孔的方法。通常，销或成孔构件可以定位在层叠预制件中，并且层压预制件形成为包括其中的销的层压结构。销通常包括最终层压结构中所需的尺寸，密度，分布，角度或其它特性。在层压体形成之后，根据不损害层压结构的选定物理特性的方法，从层压板中取出销。

94. 发明授权

US08043720B2 Process of producing a ceramic matrix composite article and article formed thereby 有权
标题翻译：制造由此形成的陶瓷基复合制品和制品的方法
公开(公告)号：US08043720B2
公开(公告)日：2011-10-25
申请号：US12420686
申请日：2009-04-08
申请人： Gregory Scot Corman , Henry Charles McGuigan , Milivoj Konstantin Brun
发明人： Gregory Scot Corman , Henry Charles McGuigan , Milivoj Konstantin Brun
IPC分类号： B32B7/02 , B32B9/04 , B32B29/00
CPC分类号： C04B38/0032 , B32B18/00 , C04B35/573 , C04B35/62863 , C04B35/62868 , C04B35/62871 , C04B35/62873 , C04B35/62894 , C04B35/632 , C04B35/638 , C04B35/806 , C04B35/83 , C04B2111/343 , C04B2235/3826 , C04B2235/422 , C04B2235/428 , C04B2235/5244 , C04B2235/5248 , C04B2235/526 , C04B2235/5264 , C04B2235/5268 , C04B2235/5272 , C04B2235/614 , C04B2235/616 , C04B2235/80 , C04B2237/361 , C04B2237/363 , C04B2237/365 , C04B2237/368 , C04B2237/38 , C04B2237/61 , C04B2237/704 , Y10T428/24983 , Y10T428/30 , Y10T428/31996 , C04B14/386 , C04B35/565
摘要： A CMC article and process for producing the article to have a layer on its surface that protects a reinforcement material within the article from damage. The method entails providing a body containing a ceramic reinforcement material in a matrix material that contains a precursor of a ceramic matrix material. A fraction of the reinforcement material is present and possibly exposed at a surface of the body. The body surface is then provided with a surface layer formed of a slurry containing a particulate material but lacking the reinforcement material of the body. The body and surface layer are heated to form the article by converting the precursor within the body to form the ceramic matrix material in which the reinforcement material is contained, and by converting the surface layer to form the protective layer that covers any fraction of the reinforcement material exposed at the body surface.
摘要翻译： CMC制品和用于生产制品的方法，以在其表面上具有保护制品内的增强材料免受损害的层。该方法需要在含有陶瓷基体材料的前体的基体材料中提供含有陶瓷增强材料的主体。增强材料的一部分存在并且可能暴露在身体的表面。然后，身体表面设置有由含有颗粒材料但缺乏身体的增强材料的浆料形成的表面层。通过将体内的前体转化以形成其中包含增强材料的陶瓷基体材料，并且通过转化表面层以形成覆盖增强材料的任何部分的保护层来加热主体和表面层以形成制品材料暴露在身体表面。

95. 发明申请

US20110180946A1 TITANIUM CARBIDE AS A FRICTION AND WEAR MODIFIER IN FRICTION MATERIALS 有权
标题翻译：碳化钛作为摩擦材料的摩擦和磨损改性剂
公开(公告)号：US20110180946A1
公开(公告)日：2011-07-28
申请号：US12410903
申请日：2009-03-25
申请人： Allen H. Simpson , Slawomir T. Fryska , Mark L. La Forest , Nabil Abu Gharbieh
发明人： Allen H. Simpson , Slawomir T. Fryska , Mark L. La Forest , Nabil Abu Gharbieh
IPC分类号： C01B31/22
CPC分类号： F16D69/023 , B82Y30/00 , C04B35/5611 , C04B35/806 , C04B35/83 , C04B2235/48 , C04B2235/5248 , C04B2235/5445 , C04B2235/5454 , C04B2235/96 , Y10T428/213
摘要： Methods of making a carbon-carbon composite preforms, particularly suitable as brake discs in aircraft landing systems, by combining titanium carbide particles ranging in size from 0.01 to 10 microns in diameter, resinous binder, and carbon fibers or carbon fiber precursors in a mold, and subsequently subjecting the combined components to pressure and heat to carbonize the resinous binder by methods, thereby providing the carbon-carbon composite preform having particulate titanium carbide uniformly distributed throughout its mass. Prior to combining the titanium carbide and the binder with the fibers in this process, the particulate titanium carbide may be mixed with liquid binder, the resulting TiC/binder mixture may then solidified, and the resulting solid TiC/binder mixture may be ground into a fine powder for use in the process. Also, compositions for preparing a carbon-carbon composite friction materials, and methods of improving wear and dynamic stability in a carbon-carbon composite brake discs.
摘要翻译：通过将尺寸范围为0.01至10微米直径的碳化钛颗粒，树脂粘合剂和模具中的碳纤维或碳纤维前体组合制备碳 - 碳复合预制件，特别适用于飞机着陆系统中的制动盘的方法，并随后使组合的组分进行加压和加热以通过方法使树脂粘合剂碳化，由此提供碳 - 碳复合预成型体，其中颗粒状碳化钛均匀地分布在其整个质量中。在该方法中将碳化钛与粘合剂与纤维结合之前，可将颗粒碳化钛与液体粘合剂混合，然后使所得到的TiC /粘合剂混合物固化，并将所得固体TiC /粘合剂混合物研磨成精细粉末用于该过程。另外，用于制备碳 - 碳复合材料摩擦材料的组合物，以及改善碳 - 碳复合制动盘中的磨损和动态稳定性的方法。

96. 发明授权

US07939046B2 Microporous graphite foam and process for producing same 有权
标题翻译：微孔石墨泡沫及其制造方法
公开(公告)号：US07939046B2
公开(公告)日：2011-05-10
申请号：US10872933
申请日：2004-06-21
申请人： Philip Christopher Theriault
发明人： Philip Christopher Theriault
IPC分类号： C01B31/00 , C01B31/04 , B29C65/00
CPC分类号： C04B38/0054 , C04B35/83 , C04B38/0022 , C04B2111/00793 , C04B2111/0081 , C04B2111/00844 , C04B2111/00853 , C04B2111/40 , C04B2235/48 , C04B2235/5248 , C04B38/0074
摘要： A process for producing a microporous graphite foam including a matrix of graphite fibers joined by a graphitized graphite-forming precursor. In one embodiment, the process includes providing a plurality of graphite fibers; mixing the graphite fibers with a graphite-forming precursor; compressing the mixture; forming a precursor matrix comprising the graphite fiber and the graphite-forming precursor; first heating the matrix to a temperature at which the graphite-forming precursor is carbonized, forming a carbonized matrix; and second heating the carbonized matrix to a temperature at which the carbonized graphite-forming precursor is graphitized, forming the microporous graphite foam. The graphite foam has one or more of pore sizes less than about ten microns, low bulk density, high physical strength and good machinability, while also having the desirable characteristics of graphite, including high thermal conductivity, electrical conductivity and solderability.
摘要翻译：一种生产微孔石墨泡沫的方法，其包括通过石墨化石墨形成前体连接的石墨纤维的基体。在一个实施方案中，该方法包括提供多个石墨纤维; 将石墨纤维与形成石墨的前体混合; 压缩混合物; 形成包含石墨纤维和形成石墨的前体的前体基质; 首先将基质加热到石墨形成前体碳化的温度，形成碳化基质; 并且将碳化基质第二次加热到碳化石墨形成前体被石墨化的温度，形成微孔石墨泡沫体。石墨泡沫具有小于约十微米，低堆积密度，高物理强度和良好机械加工性的孔径中的一种或多种，同时具有包括高导热性，导电性和可焊性的石墨所需的特性。

97. 发明授权

US07799715B2 Boron carbide ceramic and manufacturing method thereof 有权
标题翻译：碳化硼陶瓷及其制造方法
公开(公告)号：US07799715B2
公开(公告)日：2010-09-21
申请号：US12209851
申请日：2008-09-12
申请人： Ken Hirota , Yoshihiro Nakayama , Shingo Nakane
发明人： Ken Hirota , Yoshihiro Nakayama , Shingo Nakane
IPC分类号： C04B35/563 , C04B35/80
CPC分类号： C04B35/563 , C04B35/62685 , C04B35/645 , C04B2235/3217 , C04B2235/421 , C04B2235/422 , C04B2235/5248 , C04B2235/526 , C04B2235/5264 , C04B2235/5268 , C04B2235/5445 , C04B2235/604 , C04B2235/6562 , C04B2235/6565 , C04B2235/6567 , C04B2235/6581 , C04B2235/666 , C04B2235/77 , C04B2235/80 , C04B2235/96
摘要： Boron carbide ceramics produced by spark sintering methods have more desirable mechanical properties than conventionally produced carbides. The boron carbide ceramics include amorphous boron, amorphous carbon, and Al2O3 powder as a sintering aid. The boron carbides may also contain a carbon nano fiber in a nearly homogeneously dispersed state. The sintered compact has a relative density of a boron carbide ceramic of approximately not less than 99%. The boron carbide ceramics are prepared preferably by subjecting a mixed powder of the starting raw materials and the carbon nano fiber to simultaneous synthesis and sintering using the spark plasma sintering method.
摘要翻译：通过火花烧结法生产的碳化硼陶瓷具有比常规生产的碳化物更理想的机械性能。碳化硼陶瓷包括无定形硼，无定形碳和作为烧结助剂的Al 2 O 3粉末。碳化硼也可以含有几乎均匀分散状态的碳纳米纤维。烧结体的碳化硼陶瓷的相对密度约为99％以上。优选通过使用放电等离子体烧结法使起始原料和碳纳米纤维的混合粉末同时进行合成和烧结来制备碳化硼陶瓷。

98. 发明授权

US07758779B2 Reinforced resin-derived carbon foam 失效
标题翻译：增强树脂衍生的碳泡沫
公开(公告)号：US07758779B2
公开(公告)日：2010-07-20
申请号：US11321739
申请日：2005-12-29
申请人： Douglas J. Miller , Irwin C. Lewis , Richard L. Shao , Mehmet Suha Yazici
发明人： Douglas J. Miller , Irwin C. Lewis , Richard L. Shao , Mehmet Suha Yazici
IPC分类号： C01B31/02 , C08G8/10
CPC分类号： C08G8/10 , C04B35/83 , C04B38/0022 , C04B2111/00431 , C04B2111/00853 , C04B2111/00939 , C04B2111/2046 , C04B2111/52 , C04B2235/48 , C04B2235/483 , C04B2235/5248 , C04B2235/787 , C08J9/0085 , C08J2203/06 , C08J2361/06 , Y10S521/919 , Y10T428/30 , C04B38/0064 , C04B38/0074 , C04B38/08
摘要： A reinforced carbon foam material is formed from carbon fibers incorporated within a carbon foam's structure. First, carbon fiber bundles are combined with a liquid resol resin. The carbon fiber bundles separate into individual carbon fiber filaments and disperse throughout the liquid resol resin. Second, the carbon fiber resin mixture is foamed thus fixing the carbon fibers in a permanent spatial arrangement within the phenolic foam. The foam is then carbonized to create a carbon fiber reinforced foam with improved graphitic characteristics as well as increased strength. Optionally, various additives can be introduced simultaneously with the addition of the carbon fiber bundles into the liquid resol, which can improve the graphitic nature of the final carbon foam material and/or increase the foam's resistance to oxidation.
摘要翻译：增强碳泡沫材料由掺入碳泡沫结构中的碳纤维形成。首先，将碳纤维束与液体甲醛树脂组合。碳纤维束分成单独的碳纤维长丝，并分散在整个液体甲醛树脂中。第二，将碳纤维树脂混合物发泡，从而将酚醛泡沫塑料中的永久性空间布置的碳纤维固定。然后将泡沫碳化以产生具有改善的石墨特性以及增加的强度的碳纤维增强泡沫。任选地，可以将各种添加剂同时引入，将碳纤维束加入到液体甲醇溶胶中，这可以改善最终的碳泡沫材料的石墨性质和/或增加泡沫的抗氧化性。

99. 发明申请

US20100179049A1 SILICON CARBIDE-SILICON CARBIDE FIBER COMPOSITE AND MAKING METHOD 审中-公开
标题翻译：碳化硅碳化硅纤维复合材料和制造方法
公开(公告)号：US20100179049A1
公开(公告)日：2010-07-15
申请号：US12726181
申请日：2010-03-17
申请人： Hirofumi FUKUOKA , Susumu Ueno , Toshio Okada , Meguru Kashida
发明人： Hirofumi FUKUOKA , Susumu Ueno , Toshio Okada , Meguru Kashida
IPC分类号： C04B35/577
CPC分类号： C04B35/83 , C04B2235/3418 , C04B2235/425 , C04B2235/428 , C04B2235/5248 , C04B2235/6562 , C04B2235/6581 , Y10T428/292
摘要： A silicon carbide-silicon carbide fiber composite consists of silicon carbide particles and silicon carbide fibers. The composite has excellent oxidation resistance and finds a wide range of application as heat resistant material. The silicon carbide conversion method is simple and consistent enough to ensure production of silicon carbide-silicon carbide fiber composites with minimized variation in quality.
摘要翻译：碳化硅 - 碳化硅纤维复合材料由碳化硅颗粒和碳化硅纤维组成。该复合材料具有优异的抗氧化性，可广泛应用于耐热材料。碳化硅转换方法简单和一致，足以确保碳化硅 - 碳化硅纤维复合材料的生产，质量变化最小化。

100. 发明授权

US07723248B2 Ceramic composite material and method for producing same 有权
标题翻译：陶瓷复合材料及其制造方法
公开(公告)号：US07723248B2
公开(公告)日：2010-05-25
申请号：US10595577
申请日：2004-10-22
申请人： Tomoyuki Ueno , Masashi Yoshimura
发明人： Tomoyuki Ueno , Masashi Yoshimura
IPC分类号： C04B35/52 , C04B35/00
CPC分类号： C04B35/645 , B82Y30/00 , C04B35/117 , C04B35/185 , C04B35/443 , C04B35/486 , C04B35/488 , C04B35/52 , C04B35/522 , C04B35/524 , C04B35/528 , C04B35/565 , C04B35/575 , C04B35/581 , C04B35/584 , C04B35/593 , C04B35/597 , C04B35/6261 , C04B35/6303 , C04B35/80 , C04B2235/3206 , C04B2235/3217 , C04B2235/3222 , C04B2235/3225 , C04B2235/3246 , C04B2235/3256 , C04B2235/3463 , C04B2235/3826 , C04B2235/3839 , C04B2235/3843 , C04B2235/3847 , C04B2235/3856 , C04B2235/3865 , C04B2235/3869 , C04B2235/3873 , C04B2235/3886 , C04B2235/404 , C04B2235/422 , C04B2235/424 , C04B2235/425 , C04B2235/427 , C04B2235/5248 , C04B2235/5288 , C04B2235/5436 , C04B2235/5445 , C04B2235/656 , C04B2235/658 , C04B2235/6581 , C04B2235/767 , C04B2235/77 , C04B2235/781 , C04B2235/786 , C04B2235/80 , C04B2235/96 , C04B2235/963
摘要： Highly wear-resistant, low-friction ceramic composites suited for machining-tool, sliding-component, and mold-die materials are made available. The ceramic composites characterized are constituted from a phase having carbon of 3 μm or less, preferably 30 nm or less, average crystal-grain size as the principal component, and a ceramic phase (with the proviso that carbon is excluded). The ceramic phase is at least one selected from the group made up of nitrides, carbides, oxides, composite nitrides, composite carbides, composite oxides, carbonitrides, oxynitrides, oxycarbonitrides, and oxycarbides of Al, Si, Ti, Zr, Hf, V, Nb, Ta, Cr, Mo and W. The ceramic composites are produced by sintering the source-material powders at a sintering temperature of 800 to 1500° C. and a sintering pressure of 200 MPa or greater.
摘要翻译：提供了适用于加工工具，滑动部件和模具模具材料的高度耐磨，低摩擦的陶瓷复合材料。表征的陶瓷复合体由碳为3μm以下，优选为30nm以下，平均结晶粒径为主要成分的相和陶瓷相（条件是不排除碳）构成。陶瓷相是选自由氮化物，碳化物，氧化物，复合氮化物，复合碳化物，复合氧化物，碳氮化物，氮氧化物，碳氮氧化物和Al，Si，Ti，Zr，Hf，V， Nb，Ta，Cr，Mo和W.通过在800〜1500℃的烧结温度和200MPa以上的烧结压力下烧结源材料粉末来制造陶瓷复合体。

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