Abstract:
The present invention relates to a photosensitive ceramic composite and a method for manufacturing a multilayer substrate using the composite. The photosensitive ceramic composite and manufacturing method of the present invention are applicable to circuit members and components for ceramic multilayer substrates for high-frequency wireless communication. The photosensitive ceramic composite contains inorganic particles and a photosensitive organic component. The inorganic particles have at least surface sections containing an inorganic material having a refractive index less than that of inner sections of the inorganic particles.
Abstract:
A method to control the post sinter distortion of free sintered multilayer ceramic substrates by placing a discrete non-densifying structure in the green ceramic laminate prior to sintering. One or several discrete non-densifying structures are placed on one or more ceramic greensheets which are then stacked and laminated to form a green ceramic laminate. The laminate is then sintered and the discrete non-densifying structure will locally control the dimensions of the free sintered multilayer ceramic substrate. The method can be used to control post sinter dimensions in MLC substrates manufactured as either single or multi-up substrates by placing the discrete non-densifying structure in the active area or in the kerf area between the individual product ups prior to sintering.
Abstract:
A green laminate for obtaining a multilayer substrate includes base material layer green sheets held between constraint layer green sheets. The green laminate includes constraint layer green sheets laminated on the outside of a laminate of base material layer green sheets, and cutting grooves are formed in the constraint layer green sheets. By burning the green laminate to obtain a sintered laminate, the difference between expansion and shrinkage behaviors due to the difference between the thermal expansion coefficients of the glass ceramic sintered layer and the ceramic powder fixed layer occurs in each of the regions divided by the cutting grooves, thereby relieving stress due to the difference between expansion and shrinkage behaviors.
Abstract:
The present invention is a low density hybrid airfoil comprising a temperature resistant exterior layer and a tough, high impact resistant interior layer. Specifically, the airfoil comprises a monolithic ceramic exterior layer and a fiber reinforced ceramic matrix composite interior layer. Both the monolithic ceramic and fiber reinforced ceramic matrix composite are low density materials. Additionally, the monolithic ceramic is a high temperature resistant material, and the fiber reinforced ceramic matrix composite is a relatively high impact resistant structure. Encapsulating the airfoil with a temperature resistant exterior layer protects the airfoil in a high temperature environment, and supporting the airfoil with a high impact resistant, fiber reinforced ceramic matrix composite improves the overall impact resistance of the airfoil thereby resulting in a tough, high temperature resistant, low density airfoil.
Abstract:
The present invention provides a dielectric ceramic composition, a capacitor using the composition and the producing method, of having a lower dielectric loss and a stable characteristics in high frequency bandwidth, and enabling to use a base metal or a carbon-based material as an electrode material by allowing sintering at a low temperate, thereby resulting in lower cost. The dielectric ceramic composition according to present invention, is characterized in comprising a main component of formula SrxBa1nullx(ZryTi1nully) O3 (where 0.8nullxnull1; 0.9nullynull1) to which MuO2 of 0.05-15 wt %, at least one of 0.001-5 wt % selected from the group consisting of Bi2O3PbO and Sb2O3 and a glass component of 0.5-15 wt % are added based on the weight of the main component.
Abstract translation:本发明提供一种电介质陶瓷组合物,使用该组合物和制造方法的电容器,其具有较低的介电损耗和高频带宽的稳定特性,能够使用贱金属或碳基材料作为电极 通过允许在低温下进行烧结从而导致较低成本的材料。 根据本发明的电介质陶瓷组合物的特征在于,其中MuO 2为0.05的式Sr x B a 1-x(ZryTi 1-y)O 3(其中0.8 <= x <= 1; 0.9 <= y <= 1) -15重量%,基于主成分的重量,添加选自Bi 2 O 3 PbO和Sb 2 O 3的0.001-5重量%和0.5〜15重量%的玻璃成分中的至少一种。
Abstract:
A shrinkage suppression layer used in the production of a ceramic substrate according to a non-shrinkage process provides favorable removal performance while sufficiently ensuring the restraining performance of the shrinkage suppression layer. Resin beads, which disappear at a temperature lower than the sintering temperature of a low-temperature sintering ceramic material of a base material layer to form open bores in a shrinkage suppression layer, are added to the shrinkage suppression layer and dispersed uniformly at least in a principal surface direction. The shrinkage suppression layer provides sufficient restraining performance to the base material layer in the step of firing, and after the firing, forms open bores, thereby improving the removal performance of the shrinkage suppression layer.
Abstract:
A shrinkage suppression layer used in the production of a ceramic substrate according to a non-shrinkage process provides favorable removal performance while sufficiently ensuring the restraining performance of the shrinkage suppression layer. Resin beads, which disappear at a temperature lower than the sintering temperature of a low-temperature sintering ceramic material of a base material layer to form open bores in a shrinkage suppression layer, are added to the shrinkage suppression layer and dispersed uniformly at least in a principal surface direction. The shrinkage suppression layer provides sufficient restraining performance to the base material layer in the step of firing, and after the firing, forms open bores, thereby improving the removal performance of the shrinkage suppression layer.
Abstract:
A method of producing a ceramic multilayer substrate involves producing a green composite laminate 11 containing first and second shrink-suppressing layers formed on the main surfaces of a green multilayer mother substrate 12 having a plurality of ceramic green layers 17 containing ceramic powder, the shrink-suppressing layers containing a sintering-difficult powder substantially incapable of being sintered under the sintering conditions for the ceramic powder; forming first grooves 16 extending from the first shrink-suppressing layer 13 side into a part of the multilayer mother substrate 12; firing the composite laminate 11; removing the first and second shrink-suppressing layers 13 and 14 and taking out the sintered multilayer mother substrate 11; and dividing the multilayer mother substrate 12 along the grooves 16, and obtaining a plurality of the ceramic multilayer substrates. Thereby, shrinkage in the plan direction at firing can be suppressed. Thus, a ceramic multilayer substrate having a high dimensional accuracy and a high reliability can be produced with a high production efficiency.
Abstract:
A method for producing a ceramic substrate which employs a cofiring process using restraint sheets in which a second ceramic green sheet 7 is laminated on a green ceramic substrate 30 so as to cover surface conductors 32 of the green ceramic substrate 30, the second ceramic green sheet 7 subsequently being integrated with the green ceramic substrate 30. Restraint sheets 9, which are not sintered at a sintering temperature at which the green ceramic substrate 30 is sintered, are laminated on corresponding opposite sides of the green ceramic substrate 30 so as to restrain the green ceramic substrate 30 together with the second ceramic green sheet 7. The second ceramic green sheet 7 and the green ceramic substrate 30 are fired at a temperature at which the second ceramic green sheet 7 and the green ceramic substrate 30 are integrally sintered, whereas the restraint sheets 9 are not sintered, to thereby yield a ceramic substrate 40. The restraint sheets 9 and a ceramic covering layer 7a which covers the surface conductors 32 are removed, to thereby expose the surface conductor layer 32. A plating layer 31 is formed on the surface conductor layer 32.
Abstract:
A method of alleviating edge curling when laminated structures comprising layers of green material having different shrinkage rates are sintered comprises applying to a face (18) of edges (14) the first layer (10) having the higher shrinkage rate green sinterable material, opposite to the second layer (12) having the lower shrinkage rate green sinterable material, an edge strip (16) of a green sinterable material also having a shrinkage rate lower than the first layer, and then firing the laminated structure. The edge strip may be partly or, advantageously, wholly embedded in the first layer. The sinterable materials of the second layer and edge strip may be the same or similar. The invention is particularly applicable to solid oxide fuel cell sub-structures in which the first layer is the anode layer and the second layer is the electrolyte layer.