C04B2237/365

COVER LID WITH SELECTIVE AND EDGE METALLIZATION
20170229361 · 2017-08-10 ·

A cover lid for use with a semiconductor package is disclosed. First, a polyamide mask is applied to one surface of the lid plate. Next, the exposed areas of the surface, as well as the sides of the lid plate, are metallized. The polyamide mask can then be removed. This reduces pullback and shrinkage of the metallized layer, while lowering the manufacturing cost and process times.

ALUMINUM/CERAMIC BONDING SUBSTRATE AND METHOD FOR PRODUCING SAME

There is provided an aluminum/ceramic bonding substrate having a ceramic substrate, an aluminum plate of an aluminum alloy which is bonded directly to one side of the ceramic substrate, an aluminum base plate of the aluminum alloy which is bonded directly to the other side of the ceramic substrate, and a plate-shaped reinforcing member which has a higher strength than that of the aluminum base plate and which is arranged in the aluminum base plate to be bonded directly to the aluminum base plate, wherein the aluminum alloy contains 0.01 to 0.2% by weight of magnesium, 0.01 to 0.1% by weight of silicon, and the balance being aluminum and unavoidable impurities.

Metal-ceramic substrate

A metal-ceramic substrate having at least one ceramic layer (2), which is provided on a first surface side (2a) with at least one first metallization (3) and on a second surface side (2b), opposite from the first surface side (2a), with a second metallization (4), wherein the first metallization (3) is formed by a film or layer of copper or a copper alloy and is connected to the first surface side (2a) of the ceramic layer (2) with the aid of a “direct copper bonding” process. The second metallization (4) is formed by a layer of aluminum or an aluminum alloy.

Honeycomb filter and method for producing honeycomb filter

An object of the present invention is to provide a honeycomb filter capable of achieving a combination of high collection efficiency and low pressure loss. The honeycomb filter comprises a ceramic honeycomb substrate in which a multitude of cells through which a fluid flows are disposed in parallel in a longitudinal direction and are separated by cell walls, each cell being sealed at an end section at either the fluid inlet side or the fluid outlet side, and a filter layer which, among the surfaces of the cell walls, is formed on the surface of the cell walls of those cells in which the end section at the fluid inlet side is open and the end section at the fluid outlet side is sealed by a sealing material, wherein the thickness of the filter layer increases gradually from the fluid inlet side toward the fluid outlet side.

ADAPTER ELEMENT FOR CONNECTING AN ELECTRONICS COMPONENT TO A HEAT SINK ELEMENT, SYSTEM COMPRISING AN ADAPTER ELEMENT OF THIS KIND, AND METHOD FOR PRODUCING AN ADAPTER ELEMENT OF THIS KIND
20220271498 · 2022-08-25 ·

An adapter element (10) for connecting an electronic component (30) to a heat sink element (20), including an insulation layer (15) extending along a main extension plane (HSE), and at least a first web element (11) and a second web element (12), which are arranged next to each other in a direction parallel to the main extension plane (HSE), forming a free area (13), which, in the assembled state, are arranged between the insulating layer (15) and the electronic component (30) in a direction running perpendicular to the main extension plane (HSE), and on whose front sides (18) facing away from the insulating layer (15) the electronic component (30) is arranged in the assembled state, wherein a distance (A) between the first web element (11) and the second web element (12), measured in a plane parallel to the main extension plane (HSE), is smaller than 350 μm.

METHOD FOR PRODUCING A DOUBLE-WALLED THERMOSTRUCTURAL MONOLITHIC COMPOSTE PART, AND PART PRODUCED
20170217843 · 2017-08-03 ·

A fibrous preform (1) is produced, provided with a sandwich structure comprising an intermediate flexible core (4) and two outer fibrous frames (2, 3), respectively arranged on opposing outer faces of said flexible core (4) and assembled by sections of wire (8, 9) passing through said fibrous frames (2, 3), said preform (1) being impregnated with resin. Said preform is then hardened and the core (4) is removed, preferably by pre-densification with chemical vapour infiltration, and the structure produced is then densified with liquid-phase infiltration.

METHOD FOR PRODUCING CERAMIC MATRIX COMPOSITE

A production method for a ceramic matrix composite is comprised of: compounding an aggregate powder including a ceramic and a binder including at least one of thermoplastic resins and waxes to form a composition of the aggregate powder and the binder; pressing the composition to form sheets; accumulating fabrics of reinforcement fibers including the ceramic and the sheets alternately; pressing an accumulated body of the fabrics and the sheets; and generating a matrix combining the reinforcement fibers together.

Ceramic structure for plasma processing apparatus and manufacturing method thereof
11456158 · 2022-09-27 · ·

A ceramic structure including a first conductive structure embedded therein and a second conductive structure embedded at a different depth from the first conductive structure is disclosed. In the ceramic structure, the first conductive structure and the second conductive structure are electrically connected to each other by an electrically conductive connection member capable of compensating for a vertical shrinkage rate of a ceramic sheet shape while being embedded therein when sintering the ceramic structure.

BIFURACTING LAYUP FOR AIRFOIL RIB, METHODS OF MANUFACTURE THEREOF AND ARTICLES COMPRISING THE SAME
20220266977 · 2022-08-25 ·

An airfoil comprises a wall that defines a leading edge and a trailing edge and one or more cavities located within the wall along with a rib that separates the cavities. The rib or the wall comprises a first split ply that comprises a consolidated section and two or more split sections; wherein the split sections emanate from the consolidated section; and where the split sections define the wall and the cavities of the airfoil.

Method for joining substrates

The invention relates to a method of joining substrates. It is the object of the invention in this respect to join substrates of substrate materials together without having to exert an increased effort for a coating with additional coating processes to be carried out and to be able to achieve a good quality of the join connection in so doing. In the method in accordance with the invention a pretreatment of at least one join surface of a substrate to be joined is carried out in low pressure oxygen plasma prior to the actual joining. On the joining, a contact force acts on the substrates to be joined in the range 2 kPa to 5 MPa and in this process a heat treatment is carried out at an elevated temperature of at least 100° C. and at under pressure conditions of a maximum of 10 mbar, preferably <10.sup.−3 mbar.