公开(公告)号：US20090324966A1

公开(公告)日：2009-12-31

申请号：US10999438

申请日：2004-11-29

申请人： Bodo Benitsch ,  Eugen Pfitzmaier

发明人： Bodo Benitsch ,  Eugen Pfitzmaier

IPC分类号： F41H5/04 ,  B32B37/00

CPC分类号： F41H5/0435 ,  Y10T428/239 ,  Y10T428/24124 ,  Y10T428/24529 ,  Y10T428/24628

摘要： A multilayer armor plating material contains a single-piece or multi-piece ceramic or metallic layer which, as seen in the direction of attack, is followed by a rear supporting layer of glass fiber-reinforced plastic (GRP) and/or of carbon fiber-reinforced plastic (CRP). As seen in the direction of attack the ceramic or metallic layer is preceded by a front supporting layer of glass fiber-reinforced plastic (GRP) and/or carbon fiber-reinforced plastic (CRP). As a result, the steel or ceramic layer is optimally embedded in a composite between the front and rear supporting layers and thereby supported. This in particular protects the ceramic or steel material from harmful vibrations caused by repeated impact of projectiles, on account of the higher rigidity of the structure reducing the vibration amplitudes.

摘要翻译： 多层铠装电镀材料包含单件或多块陶瓷或金属层，从攻击方向看，其后是玻璃纤维增​​强塑料（GRP）和/或碳纤维的后支撑层 - 增强塑料（CRP）。 从攻击方向看，陶瓷或金属层之前是玻璃纤维增​​强塑料（GRP）和/或碳纤维增强塑料（CRP）的前支撑层。 结果，钢或陶瓷层最佳地嵌入在前支撑层和后支撑层之间的复合材料中，从而被支撑。 这尤其是保护陶瓷或钢材不受弹丸重复撞击造成的有害振动，这是由于结构的刚度较高而降低了振动幅度。

公开(公告)号：US07238414B2

公开(公告)日：2007-07-03

申请号：US10852960

申请日：2004-05-24

申请人： Bodo Benitsch ,  Michael Heine ,  Sven Schweizer ,  Rainer Zimmermann-Chopin

发明人： Bodo Benitsch ,  Michael Heine ,  Sven Schweizer ,  Rainer Zimmermann-Chopin

IPC分类号： B32B17/12 ,  B32B3/14

CPC分类号： F41H5/0428 ,  B32B18/00 ,  B32B2315/02 ,  C04B35/522 ,  C04B35/573 ,  C04B35/83 ,  C04B2235/38 ,  C04B2235/3821 ,  C04B2235/3826 ,  C04B2235/3843 ,  C04B2235/3847 ,  C04B2235/386 ,  C04B2235/3873 ,  C04B2235/48 ,  C04B2235/5248 ,  C04B2235/526 ,  C04B2235/5264 ,  C04B2235/5272 ,  C04B2237/365 ,  C04B2237/38 ,  C04B2237/385 ,  C04B2237/584 ,  C04B2237/61 ,  Y10T428/166 ,  Y10T428/249924 ,  Y10T428/249928

摘要： A fiber-reinforced composite body containing a first zone made of a ceramic matrix, which predominantly contains silicon carbide and, optionally, silicon and/or carbon and/or compounds thereof, and containing a second zone, which is located on a surface of the ceramic matrix zone and formed form a fiber-reinforced C/SiC ceramic. The fiber length decreases from the exterior of the fiber-reinforced ceramic zone up to the first zone and, optionally, up to one or more other zones that are arranged on the second zone. A method for producing the composite body is characterized by involving a joint infiltration at least of the first zone and of the second zone with liquid silicon and by the carrying out of a siliconization. A composite body of this type can be used, in particular, as armoring in the civil or military sectors.

摘要翻译： 一种纤维增强复合体，其包含由陶瓷基体制成的第一区域，该第一区域主要含有碳化硅和任选的硅和/或碳和/或其化合物，并且包含第二区，其位于 陶瓷基体区并形成纤维增强C / SiC陶瓷。 纤维长度从纤维增强陶瓷区域的外部直到第一区域，并且可选地，直到布置在第二区域上的一个或多个其它区域减小。 复合体的制造方法的特征在于，至少使第一区域和第二区域与液态硅进行接合渗透，并且进行硅化。 这种复合体可以用于民用或军事部门的装甲。

公开(公告)号：US20070116939A1

公开(公告)日：2007-05-24

申请号：US10852960

申请日：2004-05-24

申请人： Bodo Benitsch ,  Michael Heine ,  Sven Schweizer ,  Rainer Zimmermann-Chopin

发明人： Bodo Benitsch ,  Michael Heine ,  Sven Schweizer ,  Rainer Zimmermann-Chopin

IPC分类号： D04H13/00 ,  D04H5/00

CPC分类号： F41H5/0428 ,  B32B18/00 ,  B32B2315/02 ,  C04B35/522 ,  C04B35/573 ,  C04B35/83 ,  C04B2235/38 ,  C04B2235/3821 ,  C04B2235/3826 ,  C04B2235/3843 ,  C04B2235/3847 ,  C04B2235/386 ,  C04B2235/3873 ,  C04B2235/48 ,  C04B2235/5248 ,  C04B2235/526 ,  C04B2235/5264 ,  C04B2235/5272 ,  C04B2237/365 ,  C04B2237/38 ,  C04B2237/385 ,  C04B2237/584 ,  C04B2237/61 ,  Y10T428/166 ,  Y10T428/249924 ,  Y10T428/249928

摘要： A fiber-reinforced composite body containing a first zone made of a ceramic matrix, which predominantly contains silicon carbide and, optionally, silicon and/or carbon and/or compounds thereof, and containing a second zone, which is located on a surface of the ceramic matrix zone and formed form a fiber-reinforced C/SiC ceramic. The fiber length decreases from the exterior of the fiber-reinforced ceramic zone up to the first zone and, optionally, up to one or more other zones that are arranged on the second zone. A method for producing the composite body is characterized by involving a joint infiltration at least of the first zone and of the second zone with liquid silicon and by the carrying out of a siliconization. A composite body of this type can be used, in particular, as armoring in the civil or military sectors.

摘要翻译： 一种纤维增强复合体，其包含由陶瓷基体制成的第一区域，该第一区域主要含有碳化硅和任选的硅和/或碳和/或其化合物，并且包含第二区，其位于 陶瓷基体区并形成纤维增强C / SiC陶瓷。 纤维长度从纤维增强陶瓷区域的外部直到第一区域，并且可选地，直到布置在第二区域上的一个或多个其它区域减小。 复合体的制造方法的特征在于，至少使第一区域和第二区域与液态硅进行接合渗透，并进行硅化。 这种复合体可以用于民用或军事部门的装甲。

公开(公告)号：US07128963B2

公开(公告)日：2006-10-31

申请号：US10617640

申请日：2003-07-10

申请人： Bodo Benitsch

发明人： Bodo Benitsch

IPC分类号： B32B9/00

CPC分类号： F41H5/0414 ,  Y10T428/24942 ,  Y10T428/249953 ,  Y10T428/249955 ,  Y10T428/249956 ,  Y10T428/249957 ,  Y10T428/249967 ,  Y10T428/249969 ,  Y10T428/249981 ,  Y10T428/249987 ,  Y10T428/24999 ,  Y10T442/2623

摘要： A ceramic composite body includes at least two layers: material layer A and material layer B. Material layer A contains phases of a metal and the carbide of this metal. Material layer B contains silicon carbide that has been loosely bound by sintering. A method for fabricating the composite body is included and a protective armor against projectiles.

摘要翻译： 陶瓷复合体包括至少两层：材料层A和材料层B.材料层A包含金属的相和该金属的碳化物。 材料层B含有通过烧结松散结合的碳化硅。 包括一种制造复合体的方法和一种针对弹丸的防护装甲。

公开(公告)号：US20090239434A1

公开(公告)日：2009-09-24

申请号：US12478914

申请日：2009-06-05

申请人： Bodo Benitsch ,  Bernhard Heidenreich ,  Christian Zuber

发明人： Bodo Benitsch ,  Bernhard Heidenreich ,  Christian Zuber

IPC分类号： C04B35/573 ,  C04B35/80 ,  B32B5/02

CPC分类号： C04B35/83 ,  C04B2235/5256 ,  C04B2235/5268 ,  C04B2235/6562 ,  C04B2235/6565 ,  C04B2235/96 ,  Y10T428/30 ,  Y10T442/2984 ,  Y10T442/3528 ,  Y10T442/3976

摘要： A method of producing a fiber-reinforced carbide-ceramic component includes producing a carbonaceous article from at least one unidirectional tape by pyrolysis, infiltrating the carbonaceous article with carbide former, and coating the at least one unidirectional tape with a coating material being volatile in pyrolysis and/or providing the at least one unidirectional tape with a transverse thread system including transverse threads composed of a material being volatile in pyrolysis. A fiber-reinforced carbide ceramic component is also provided.

摘要翻译： 纤维增强碳化物 - 陶瓷组分的制造方法包括通过热解从至少一个单向带生产碳质制品，用碳化物形成剂渗透碳质制品，并用热解中挥发的涂料涂覆至少一个单向带 和/或提供至少一个单向带，该横向线系统包括由在热解中挥发的材料构成的横向线。 还提供了一种纤维增强碳化陶瓷组件。

公开(公告)号：US07323668B2

公开(公告)日：2008-01-29

申请号：US11080712

申请日：2005-03-15

申请人： Bodo Benitsch

发明人： Bodo Benitsch

IPC分类号： H05B6/22

CPC分类号： H05B6/101

摘要： A workpiece carrier for the inductive heating of workpieces contains ceramic materials at least at bearing surfaces which come into contact with the workpieces. The ceramic materials are distinguished by a high dimensional stability, low thermal and electrical conductivity and a high resistance to thermal shocks. A process for producing a ceramic material for a workpiece carrier obtains a suitable ceramic material by infiltrating a porous carbon skeleton with silicon. Processes for inductive heating and inductive hardening of workpieces with the workpiece carrier are also provided.

摘要翻译： 用于工件的感应加热的工件载体至少在与工件接触的轴承表面处包含陶瓷材料。 陶瓷材料的特征在于高尺寸稳定性，低导热性和导电性以及高耐热冲击性。 制造用于工件载体的陶瓷材料的方法通过用硅渗透多孔碳骨架获得合适的陶瓷材料。 还提供了用于工件载体的工件的感应加热和感应淬火的工艺。

公开(公告)号：US20050242089A1

公开(公告)日：2005-11-03

申请号：US11080712

申请日：2005-03-15

申请人： Bodo Benitsch

发明人： Bodo Benitsch

IPC分类号： H05B6/02 ,  H05B6/10

CPC分类号： H05B6/101

摘要： A workpiece carrier for the inductive heating of workpieces contains ceramic materials at least at bearing surfaces which come into contact with the workpieces. The ceramic materials are distinguished by a high dimensional stability, low thermal and electrical conductivity and a high resistance to thermal shocks. A process for producing a ceramic material for a workpiece carrier obtains a suitable ceramic material by infiltrating a porous carbon skeleton with silicon. Processes for inductive heating and inductive hardening of workpieces with the workpiece carrier are also provided.

摘要翻译： 用于工件的感应加热的工件载体至少在与工件接触的轴承表面处包含陶瓷材料。 陶瓷材料的特征在于高尺寸稳定性，低导热性和导电性以及高耐热冲击性。 制造用于工件载体的陶瓷材料的方法通过用硅渗透多孔碳骨架获得合适的陶瓷材料。 还提供了用于工件载体的工件的感应加热和感应淬火的工艺。

公开(公告)号：US07627953B2

公开(公告)日：2009-12-08

申请号：US11820145

申请日：2007-06-18

申请人： Norbert Richter ,  Stefan Baumann ,  Bodo Benitsch ,  Thomas Schmidt ,  Franz Fendt

发明人： Norbert Richter ,  Stefan Baumann ,  Bodo Benitsch ,  Thomas Schmidt ,  Franz Fendt

IPC分类号： G01B5/16 ,  C04B35/52

CPC分类号： C04B35/83 ,  C04B35/522 ,  C04B35/573 ,  C04B35/62209 ,  C04B2235/422 ,  C04B2235/428 ,  C04B2235/77 ,  C04B2235/80 ,  C04B2235/96 ,  C04B2235/9607 ,  G01B1/00 ,  G01B3/38 ,  Y10T29/49007

摘要： A method of producing a calibrating body, gage or measuring device, preferably a screw-thread measuring device, at least partially including a C—SiC material constructed of a porous, carbon-containing material with infiltrated liquid Si, includes converting the Si at least partially to SiC by reaction with carbon. The C—SiC material is produced from a C—C material based on carbon felt material produced by pressing monofibers or fiber fragments irregularly entwined with each other. A calibrating body, gage or measuring device, preferably a screw-thread measuring device, is also provided.

摘要翻译： 至少部分地包括由具有渗透液体Si的多孔含碳材料构成的C-SiC材料的校准体，量规或测量装置，优选螺纹测量装置的制造方法包括将Si至少 通过与碳反应部分地转化为SiC。 C-SiC材料是由C-C材料制成的，该C-C材料基于通过压制单个纤维或彼此不规则地缠结的纤维碎片产生的碳毡材料。 还提供了校准体，量规或测量装置，优选地是螺纹测量装置。

公开(公告)号：US20070266572A1

公开(公告)日：2007-11-22

申请号：US11820145

申请日：2007-06-18

申请人： Norbert Richter ,  Stefan Baumann ,  Bodo Benitsch ,  Thomas Schmid ,  Franz Fendt

发明人： Norbert Richter ,  Stefan Baumann ,  Bodo Benitsch ,  Thomas Schmid ,  Franz Fendt

IPC分类号： G01B1/00 ,  G01R3/00

CPC分类号： C04B35/83 ,  C04B35/522 ,  C04B35/573 ,  C04B35/62209 ,  C04B2235/422 ,  C04B2235/428 ,  C04B2235/77 ,  C04B2235/80 ,  C04B2235/96 ,  C04B2235/9607 ,  G01B1/00 ,  G01B3/38 ,  Y10T29/49007

摘要： A method of producing a calibrating body, gage or measuring device, preferably a screw-thread measuring device, at least partially including a C-SiC material constructed of a porous, carbon-containing material with infiltrated liquid Si, includes converting the Si at least partially to SiC by reaction with carbon. The C-SiC material is produced from a C-C material based on carbon felt material produced by pressing monofibers or fiber fragments irregularly entwined with each other. A calibrating body, gage or measuring device, preferably a screw-thread measuring device, is also provided.

摘要翻译： 至少部分地包括由具有渗透液体Si的多孔含碳材料构成的C-SiC材料的校准体，量规或测量装置，优选螺纹测量装置的制造方法包括将Si至少 通过与碳反应部分地转化为SiC。 C-SiC材料是由C-C材料制成的，该C-C材料基于通过压制单个纤维或彼此不规则地缠结的纤维碎片产生的碳毡材料。 还提供了校准体，量规或测量装置，优选地是螺纹测量装置。

公开(公告)号：US20060062984A1

公开(公告)日：2006-03-23

申请号：US10613822

申请日：2003-07-03

申请人： Bodo Benitsch ,  Udo Gruber ,  Sven Schweizer ,  Peter Winkelmann

发明人： Bodo Benitsch ,  Udo Gruber ,  Sven Schweizer ,  Peter Winkelmann

IPC分类号： D04H13/00

CPC分类号： B29C70/088 ,  B29K2995/0017 ,  B32B5/22 ,  C04B35/573 ,  C04B35/83 ,  C04B2235/75 ,  F02K9/34 ,  F02K9/97 ,  F05D2300/224 ,  F05D2300/2261 ,  F05D2300/603 ,  F05D2300/614 ,  Y10T428/2495 ,  Y10T428/249924 ,  Y10T428/249928 ,  Y10T428/24994 ,  Y10T428/30

摘要： Multilayer composite for combustion chambers or nozzles of missiles, comprising an interior layer in contact with the combustion gases and an outer layer, wherein the interior layer is a fiber-reinforced ceramic whose matrix comprises phases of carbon and/or phases of silicon carbide and the outer layer is a polymer reinforced with carbon fibers, process for producing the same and combustion chambers and nozzles for missiles made of this composite

摘要翻译： 用于燃烧室或导弹喷嘴的多层复合材料，包括与燃烧气体接触的内层和外层，其中内层是纤维增强陶瓷，其基体包含碳和/或碳化硅相和 外层是用碳纤维增强的聚合物，其制造方法以及由该复合材料制成的导弹的燃烧室和喷嘴