초록 ▼

A movable structural component for a thermomechanically stressed assembly at least partially from fiber reinforced ceramic is disclosed, wherein the movable structural component comprises at least one structural element made by an polymer infiltration and pyrolysis process and at least one structura

A movable structural component for a thermomechanically stressed assembly at least partially from fiber reinforced ceramic is disclosed, wherein the movable structural component comprises at least one structural element made by an polymer infiltration and pyrolysis process and at least one structural element made by an chemical phase infiltration process.

대표청구항 ▼

1. A process for producing a movable structural component for a thermomechanically stressed assembly comprising the steps of: forming at least one first structural element by a polymer infiltration and pyrolysis process; forming at least one second structural element by a chemical vapor infiltr

1. A process for producing a movable structural component for a thermomechanically stressed assembly comprising the steps of: forming at least one first structural element by a polymer infiltration and pyrolysis process; forming at least one second structural element by a chemical vapor infiltration process; and joining the first and second structural elements to the structural component; wherein when forming the at least one first structural element by a polymer infiltration and pyrolysis process, tailored fabrics from thermally highly stressable fibers are let onto positive molds or into forging dies, the tailored fabrics are impregnated with a fiber corresponding organic polymer resin, and cured at about 200° C. and about 5 bar and a formed green compact is subjected to a pyrolysis treatment at about 1,200° C. for producing a fiber reinforced matrix. 2. The process of claim 1, wherein the structural elements are joined by connecting elements produced by a chemical vapor infiltration process.3. The process of claim 1, wherein the structural element is at least partly provided with at least one protective layer made by chemical vapor deposition.4. A process for producing a movable structural component for a thermomechanically stressed assembly comprising the steps of: forming at least one first structural element by a polymer infiltration and pyrolysis process; forming at least one second structural element by a chemical vapor infiltration process; and joining the first and second structural elements to the structural component; wherein a fabric layer of thermally highly stressable fibers is provided at least partly and in a distance with an adhesive, the fabric layer is wound to an essentially tube shaped fiber preform of suitable diameter, the fiber preform being inserted into a chemical vapor infiltration reactor and being subjected to a gradient chemical vapor infiltration under the action of a methyltrichlorsilane/hydrogen process gas; wherein at the beginning of the process, a temperature gradient between about 700° C. inside the tube shaped fiber preform and about 1,150° C. in the reactor space is adjusted. 5. The process of claim 4, wherein the thermally highly stressable fibers are chosen from the group consisting of carbon, silicon carbide, aluminum oxide, mullite and polyborosilazane fibers.6. A process for producing a movable structural component for a thermomechanically stressed assembly comprising the steps of: forming at least one first structural element by a polymer infiltration and pyrolysis process; forming at least one second structural element by a chemical vapor infiltration process; and joining the first and second structural elements to the structural component; wherein when forming the at least one first structural element by a polymer infiltration and pyrolysis process, tailored fabrics from thermally highly stressable fibers are let onto positive molds or into forging dies, the tailored fabrics are impregnated with a fiber corresponding organic polymer resin, and cured at about 200° C. and about 5 bar and a formed green compact is subjected to a pyrolysis treatment at about 1,200° C. or 1600° C. depending on the temperature of use for producing a fiber reinforced matrix.