Patent application number | Description | Published |
20130019680 | MEMS STRUCTURE FOR AN ANGULAR RATE SENSOR - A micro-electromechanical system (MEMS) structure for an angular rate sensor, the structure being positioned between first and second silicon-insulator composite wafers formed of a plurality of structured silicon parts, electrically isolated from each other by an insulator material, the structure comprising: a mono-crystalline silicon substrate structured to form a sensing system and a frame, the sensing system being completely de-coupled from and surrounded by the frame, which is positioned between engaging surfaces of the first and second composite wafers such that the sensing system is hermetically sealed within a cavity defined by the first and second composite wafers and the frame, the sensing system including: two seismic masses having front and back surfaces; two driving beams, each having a first end attached to a seismic mass and a second end attached to the first and second composite wafers by means of fixed pedestals provided on the silicon substrate; and a bending spring arranged to directly connect between, and synchronise a primary motion of, the two seismic masses, each of the seismic masses being arranged to have a first degree of rotational freedom about an axis that is substantially perpendicular to the plane of the silicon substrate, and the seismic masses and driving beams being arranged to have a second degree of rotational freedom about an axis substantially coincident with the longitudinal axis of the driving beams; means for generating and detecting the primary motion consisting of a primary oscillation of the two seismic masses, in opposing phases, in the first degree of rotational freedom; and means of detecting a secondary motion consisting of a secondary oscillation of the two seismic masses, in opposing phases, in the second degree of rotational freedom, the means of generating and detecting the primary motion and the means of detecting a secondary motion being provided on both the front and back surfaces of each of the first and second seismic masses, wherein the sensing system is arranged such that, when the device is subjected to an angular velocity around a third axis that is substantially in the plane of the silicon substrate and perpendicular to the longitudinal axis of the beams, a Coriolis force arises which causes the secondary oscillation of the seismic masses. | 01-24-2013 |
20130026592 | FOCAL PLANE ARRAY AND METHOD FOR MANUFACTURING THE SAME - A method of forming a focal plane array by: forming a first wafer having sensing material provided on a surface, which is covered by a sacrificial layer, the sensing material being a thermistor material defining at least one pixel; providing supporting legs for the pixel within the sacrificial layer, covering them with a further sacrificial layer and forming first conductive portions in the surface of the sacrificial layer that are in contact with the supporting legs; forming a second wafer having read-out integrated circuit (ROIC), the second wafer being covered by another sacrificial layer, into which is formed second conductive portions in contact with the ROIC; bringing the sacrificial oxide layers of the first wafer and second wafer together such that the first and second conductive portions are aligned and bonding them together such that the sensing material is transferred from the first wafer to the second wafer when a sacrificial bulk layer of the first wafer is removed; and removing the sacrificial layers to release the pixel, with the supporting legs underneath it. | 01-31-2013 |
20130026596 | FOCAL PLANE ARRAY AND METHOD FOR MANUFACTURING THE SAME - A method of forming a focal plane array by: preparing a first wafer having sensing material provided on a surface, which is covered by a sacrificial layer; preparing a second wafer including read-out integrated circuit and a contact pad, which is covered by another sacrificial layer into which are formed support legs in contact with the contact pad, the support legs being covered with a further sacrificial layer; bonding the sacrificial layers of the first and second wafers together such that the sensing material is transferred from the first wafer to the second wafer when a sacrificial bulk layer of the first wafer is removed; defining a pixel in the sensing material and forming a conductive via through the pixel for providing a connection between an uppermost surface of the pixel and the supporting legs; and removing the sacrificial layers to release the pixel, with the supporting legs underneath it. | 01-31-2013 |
20130146994 | METHOD FOR MANUFACTURING A HERMETICALLY SEALED STRUCTURE - A method for providing hermetic sealing within a silicon-insulator composite wafer for manufacturing a hermetically sealed structure, comprising the steps of: patterning a first silicon wafer to have one or more recesses that extend at least partially through the first silicon wafer; filling said recesses with an insulator material able to be anodically bonded to silicon to form a first composite wafer having a plurality of silicon-insulator interfaces and a first contacting surface consisting of insulator material; and using an anodic bonding technique on the first contacting surface and an opposing second contacting surface to create hermetic sealing between the silicon-insulator interfaces, wherein the second contacting surface consists of silicon. | 06-13-2013 |