Abstract: A thermal insulation body made of a material having carbonized fibers and/or graphitized fibers is particularly suited for lining a high-temperature furnace. The thermal insulation body is assembled from at least two component parts, wherein at least two assembled component parts each have at least one connection element and the connection elements of the at least two assembled component parts interengage positively to form an undercut.

Abstract: A thermal insulation body is made from a material that includes carbonized fibers and/or graphitized fibers. A sheet-like molding that is made of the material is provided. The molding has at least one first curved portion and at least one second curved portion. The two or more curved portions have an opposite curvature relative to one another, based on at least one spatial direction. Then the first curved portion is separated from the second curved portion, in that the molding is split so as to obtain at least one first curved individual part and a second curved individual part. The individual parts are joined to form a thermal insulation body such that said body has a curvature which continues in a uniform manner based on the spatial direction.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: The mean pore number of conventional open-celled PUR foams having at least 8 ppi can be significantly reduced if the foam is stored in a liquid compound having an aromatic skeleton and at least one hydroxy group or in another compound dissolved in a solvent. During the treatment, the foam experiences an increase in volume of at least 10% without the pores collapsing. Ceramic foams produced from open-celled PUR foam having a mean pore count of less than 8 ppi are particularly suitable as flame zone structure for pore burners.

Abstract: 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.

Abstract: A process uses ground wood charcoal having a particle size of not more than 40 ?m as a starting material for producing dense, compact, homogeneous and isotropic ceramic bodies containing a high content of silicon carbide and a geometric density of at least 2.80 g/cm3. A homogeneous mixture is formed from the ground wood charcoal and a carbonizable binder for forming the ceramic bodies.

Abstract: 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.

Abstract: A friction disc, in particular a brake or clutch disc, includes carbon fiber-reinforced ceramic composite material with at least one top surface formed as a friction surface. At least part of the friction surface is formed of a different material, in particular of a carbon-containing material. The different material exhibits lower wear and oxidation resistance than that of the rest of the friction surface and a supporting zone of the friction disc. A visual, audible or mechanical signal is produced under operating conditions due to comparatively greater wear. The signal provides a warning that the service life of the friction disc is being exceeded. A process for producing the friction disc is also provided.

Abstract: Ceramic composite materials have unidirectional alignment of the reinforcing fibers. The ratio of the volume of the fiber strands of the reinforcing fibers to the volume of the matrix is at least 0.5. A process for their production involves initially coating the fiber strands or rovings of the reinforcing fibers with a sacrificial polymer. The coated fiber strands are processed with binder resins into unidirectionally reinforced CFK molded parts. The formed CFK bodies are carbonized to form CFC bodies. The CFC bodies are then silicized with liquid silicon. The liquid silicon diffuses into the pores formed in the CFC body and combines there at least partially with the carbon to form silicon carbide. The sacrificial polymer is pyrolized. The ceramic composite materials also can be used in fiber-reinforced ceramic structural parts.

Abstract: Ceramic composite materials have unidirectional alignment of the reinforcing fibers. The ratio of the volume of the fiber strands of the reinforcing fibers to the volume of the matrix is at least 0.5. A process for their production involves initially coating the fiber strands or rovings of the reinforcing fibers with a sacrificial polymer. The coated fiber strands are processed with binder resins into unidirectionally reinforced CFK molded parts. The formed CFK bodies are carbonized to form CFC bodies. The CFC bodies are then silicized with liquid silicon. The liquid silicon diffuses into the pores formed in the CFC body and combines there at least partially with the carbon to form silicon carbide. The sacrificial polymer is pyrolized. The ceramic composite materials also can be used in fiber-reinforced ceramic structural parts.

Abstract: 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.

Abstract: 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.

Abstract: 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

Abstract: 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.

Abstract: A ceramic antiballistic layer which can be produced as a large-area, optionally curved component is able to withstand a multi-hit attack from hits spaced apart by a short distance at the target. The ceramic antiballistic layer has a continuous surface on a side which faces the attack, whereas a surface which faces away from the attack has a segmented structure. The segmented structure starts from the surface and extends into the interior of the protective layer but does not penetrate all the way through the layer as far as the opposite surface, which faces the attack. Processes for producing such a layer and a protective device having the layer are also provided.

Abstract: A calibrating consists at least in part of a carbon fiber composite body. The composite body is formed from a porous material from a carbon-containing matrix, into which carbon fibers are embedded, this matrix is thickened by fluid infiltration of Si, which is essentially converted by reaction with carbon to SiC. The overall portion of Si and SIC is a maximum of 60% by volume. The carbon fibers have a minimum length of 3 mm.