Patent classifications
C04B2237/405
CERAMIC MATERIAL BASED ON ZIRCONIUM OXIDE WITH FURTHER OXIDES
A ceramic material is provided by deliberately choosing the additions of oxides to form zirconium oxide, in particular for the use of a layer system which has a high resistance to sintering, high expansion tolerance and low thermal conductivity.
THERMOELECTRIC CONVERSION ELEMENT
A thermoelectric conversion element includes an element body formed of a thermoelectric conversion material of a silicide-based compound, and electrodes each formed on one surface of the element body and the other surface opposite the one surface. The electrodes are formed of a sintered body of a copper silicide, and the electrodes and the element body are directly joined.
ELECTRIC HEATING TYPE SUPPORT, EXHAUST GAS PURIFYING DEVICE, AND METHOD FOR PRODUCING ELECTRIC HEATING TYPE SUPPORT
An electric heating support includes an electrically conductive honeycomb structure having an outer peripheral wall and porous partition walls disposed on an inner side of the outer peripheral wall, the porous partition walls defining a plurality of cells, each cell penetrating from one end face to other end face to form a flow path. A pair of metal terminals are disposed so as to face each other across a central axis of the honeycomb structure, each metal terminal being joined to a surface of the honeycomb structure via a welded portion. The honeycomb structure is composed of ceramics and a metal. The honeycomb structure contains 40% by volume or less of the metal. The welded portion of the honeycomb structure has a surface containing 40% by volume or more of the metal.
Methods for repairing composite cylinders
Methods for repairing composite cylindrical components are provided. One exemplary method for repairing a cylindrical component defining an axial direction, a radial direction, and a circumferential direction includes removing a damaged region of the cylindrical component. A flange extending from a cylindrical body of the cylindrical component is included in the damaged region. One or more arc segments that extend along the circumferential direction are connected with the existing cylindrical component. At least one of the arc segments includes a prefabricated flange. One or more plies are laid up to connect the arc segments with the existing cylindrical component to repair the damaged region of the cylindrical body and the prefabricated flange formed integrally with one of the arc segments replaces the damaged portion of the flange. Repaired cylindrical components are also provided.
MECHANICAL CERAMIC MATRIX COMPOSITE (CMC) REPAIR
Various embodiments include a metal-repaired ceramic matrix composite (CMC) article, and a method of repairing a CMC article having a defect. Particular embodiments include a method including: removing a defect-containing portion of the CMC article; forming at least one opening in a remaining portion of the CMC article; preparing a metal repair preform for replacing at least the removed portion of the CMC article, wherein a portion of the metal repair preform complements the at least one opening; and attaching the metal repair preform to the remaining portion of the CMC article.
Method for joining dissimilar engine components
A method for joining engine components includes positioning a first plurality of thermal protection structures across a thermal protection space between a first thermal protection surface and a second thermal protection surface. The first and second engine components are locally joined by forming a first plurality of transient liquid phase (TLP) or partial transient liquid phase (PTLP) bonds along corresponding ones of the first plurality of thermal protection structures between the first thermal protection surface and the second thermal protection surface. The second thermal protection surface is formed from a second surface material different from a first surface material of the first thermal protection surface.
Method for Producing a Gas-Tight Metal-Ceramic Join and Use of the Gas-Tight Metal-Ceramic Join
A method for producing a gas-tight metal-ceramic join is disclosed. In an embodiment a method includes providing at least one ceramic main body having a first end face and a second end face, applying a metallization to at least a partial region of the end faces of the main body, applying a nickel layer to the metallized partial region of the end faces, applying a brazing paste to the metallized partial region of the first end face and/or the second end face of the main body, drying the brazing paste, and firing the brazing paste.
Electrode comprising heavily-doped ceria
An electrode can include a functional layer having an Ln.sub.2MO.sub.4 phase, where Ln is at least one lanthanide optionally doped with a metal and M is at least one 3d transition metal, and a heavily-doped ceria phase. In an embodiment, the ceria phase can be present in the functional layer in an amount of at least 40 vol % based on a total volume of the functional layer absent any porosity. An electrochemical device or a sensor device can include the electrode.
Heat-permeable tube containing ceramic matrix composite
The present invention relates to a heat-permeable tube which has a double-walled construction. The material of the interior wall contains ceramic matrix composite. The material of the exterior wall contains metal. The present invention further relates to the use of this tube in a rotary tube furnace and the use of the rotary tube furnace for thermal treatment of materials. Furthermore, the invention relates to the use of a single-walled tube containing ceramic matrix composite as rotary tube.
Coatings for Ceramic Substrates
A method of metallizing a ceramic substrate includes depositing a barrier layer onto the substrate, depositing a tie layer onto the barrier layer, and depositing a metal layer onto the tie layer to metallize the substrate. The barrier layer may include an oxygen rich material, a nitrogen rich material, or a carbon rich material.