Abstract:
Method for producing a composite structure comprising the direct bonding of at least one first wafer with a second wafer, and comprising a step of initiating the propagation of a bonding wave, where the bonding interface between the first and second wafers after the propagation of the bonding wave has a bonding energy of less than or equal to 0.7 J/m2. The step of initiating the propagation of the bonding wave is performed under one or more of the following conditions: placement of the wafers in an environment at a pressure of less than 20 mbar and/or application to one of the two wafers of a mechanical pressure of between 0.1 MPa and 33.3 MPa. The method further comprises, after the step of initiating the propagation of a bonding wave, a step of determining the level of stress induced during bonding of the two wafers, the level of stress being determined on the basis of a stress parameter Ct calculated using the formula Ct=Rc/Ep, where: Rc corresponds to the radius of curvature (in km) of the two-wafer assembly and Ep corresponds to the thickness (in μm) of the two-wafer assembly. The method further comprises a step of validating the bonding when the level of stress Ct determined is greater than or equal to 0.07.
Abstract:
A method for manufacturing a semiconductor device includes providing a carrier and a semiconductor wafer having a first side and a second side opposite to the first side. The method includes applying a dielectric material to the carrier or the semiconductor wafer and bonding the semiconductor wafer to the carrier via the dielectric material. The method includes processing the semiconductor wafer and removing the carrier from the semiconductor wafer such that the dielectric material remains on the semiconductor wafer to provide a semiconductor device comprising the dielectric material.
Abstract:
An object of the invention is to provide a method for producing a conductive member having low electrical resistance, and the conductive member is obtained using a low-cost stable conductive material composition that does not contain an adhesive. A method for producing a semiconductor device in which silver or silver oxide provided on a surface of a base and silver or silver oxide provided on a surface of a semiconductor element are bonded, includes the steps of arranging a semiconductor element on a base such that silver or silver oxide provided on a surface of the semiconductor element is in contact with silver or silver oxide provided on a surface of the base, temporarily bonding the semiconductor element and the base by applying a pressure or an ultrasonic vibration to the semiconductor element or the base, and permanently bonding the semiconductor element and the base by applying heat having a temperature of 150 to 900° C. to the semiconductor device and the base.
Abstract:
Systems and methods are disclosed for providing an interconnection for extending high-temperature use in sensors and other electronic devices. The interconnection includes a semiconductor layer; an ohmic contact layer disposed on a first region of the semiconductor layer; an insulating layer disposed on a second region of the semiconductor layer, where the second region differs from the first region; a metal layer disposed above at least the insulating layer and the ohmic contact layer; and a connecting conductive region disposed on the metal layer and in vertical alignment with a third region of the semiconductor layer. The third region differs from the first region and is offset from the ohmic contact layer at the first region. The offset is configured to extend an operational lifetime of the interconnection apparatus, particularly when the interconnection apparatus is exposed to high temperature environments.
Abstract:
A high temperature, non-cavity package for non-axial electronics is designed using a glass ceramic compound with that is capable of being assembled and operating continuously at temperatures greater that 300-400° C. Metal brazes, such as silver, silver colloid or copper, are used to connect the semiconductor die, lead frame and connectors. The components are also thermally matched such that the packages can be assembled and operating continuously at high temperatures and withstand extreme temperature variations without the bonds failing or the package cracking due to a thermal mismatch.
Abstract:
The present invention relates to a GaN transistor, and a method of fabricating the same, in which a structure of a bonding pad is improved by forming an ohmic metal layer at edges of the bonding pad of a source, a drain, and a gate so as to be appropriate to wire-bonding or a back-side via-hole forming process. Accordingly, adhesive force between a metal layer of the bonding pad and a GaN substrate is enhanced by forming the ohmic metal at the edges of the bonding pad during manufacturing of the GaN transistor, thereby minimizing a separation phenomenon of a pad layer during the wire-bonding or back-side via-hole forming process, and improving reliability of a device.
Abstract:
The invention relates to a method for joining a semiconductor (20) to a substrate (10), comprising the following steps: •applying a first paste layer (1) of a sintering paste to the substrate; •heating and compressing the first paste layer to form a first sintered layer; •applying a second paste layer (2) of a sintering paste to the first sintered layer and arranging a semiconductor (20) on the second paste layer; •heating and compressing the second paste layer (2) to form a second sintered layer. The invention further relates to a semiconductor component produced by means of the method.
Abstract:
Bonding wire for semiconductor device use where both leaning failures and spring failures are suppressed by (1) in a cross-section containing the wire center and parallel to the wire longitudinal direction (wire center cross-section), there are no crystal grains with a ratio a/b of a long axis “a” and a short axis “b” of 10 or more and with an area of 15 μm2 or more (“fiber texture”), (2) when measuring a crystal direction in the wire longitudinal direction in the wire center cross-section, the ratio of crystal direction with an angle difference with respect to the wire longitudinal direction of 15° or less is, by area ratio, 50% to 90%, and (3) when measuring a crystal direction in the wire longitudinal direction at the wire surface, the ratio of crystal direction with an angle difference with respect to the wire longitudinal direction of 15° or less is, by area ratio, 50% to 90%. During the drawing step, a drawing operation with a rate of reduction of area of 15.5% or more is performed at least once. The final heat treatment temperature and the pre-final heat treatment temperature are made predetermined ranges.
Abstract:
A first substrate including a radius of curvature and a stressor layer is first provided. An outermost bowed, e.g., curved, surface of the first substrate is then brought into intimate contact with a surface of a second substrate. Bonding of the entirety of the first substrate to the second substrate is then achieved by reducing the radius of curvature of the first substrate by controlling the temperature at which bonding occurs.
Abstract:
Bonding wire for semiconductor device use where both leaning failures and spring failures are suppressed by (1) in a cross-section containing the wire center and parallel to the wire longitudinal direction (wire center cross-section), there are no crystal grains with a ratio a/b of a long axis “a” and a short axis “b” of 10 or more and with an area of 15 μm2 or more (“fiber texture”), (2) when measuring a crystal direction in the wire longitudinal direction in the wire center cross-section, the ratio of crystal direction with an angle difference with respect to the wire longitudinal direction of 15° or less is, by area ratio, 50% to 90%, and (3) when measuring a crystal direction in the wire longitudinal direction at the wire surface, the ratio of crystal direction with an angle difference with respect to the wire longitudinal direction of 15° or less is, by area ratio, 50% to 90%. During the drawing step, a drawing operation with a rate of reduction of area of 15.5% or more is performed at least once. The final heat treatment temperature and the pre-final heat treatment temperature are made predetermined ranges.