Fairchild Semiconductor Corporation

University of California

Qualcomm Mems Technologies, Inc.

Semiconductor Components Industries, LLC

Bei Technologies, Inc.

Snaptrack Incorporated

Custom Sensors & Technologies, Inc.

Cenk Acar

Ravindra Vaman Shenoy

Philip Jason Stephanou

Srinivasan Kodaganallur Ganapathi

Justin Phelps Black

Kurt Edward Petersen

Andrei M Shkel

John Gardner Bloomsburgh

Janusz Bryzek

Sandipan Maity

Brenton Simon

Minyao Mao

Lynn Edward Costlow

David William Burns

Sandeep Akkaraju

Asad M Madni

Nicholas Ian Buchan

Adam Schofield

David Lambe Marx

Kurt Peterson

In a general aspect, a micromachined gyroscope can include a substrate and a static mass suspended in an x-y plane over the substrate by a plurality of anchors attached to the substrate. The static mass can be attached to the anchors by anchor suspension flexures. The micromachined gyroscope can include a dynamic mass surrounding the static mass and suspended from the static mass by one or more gyroscope suspension flexures.

Micromachined multi-axis gyroscopes with reduced stress sensitivity

Techniques for compensating package stress of a proof mass are provided. In an example, a proof mass can be suspended from a substrate by a proof mass anchor. The first proof mass can have a major surface that defines a first plane. Portions of electrodes forming part of the proof mass can be symmetric with each other across a first line, wherein the first line bisects the first proof mass anchor, extends parallel to the first plane and extends between the first electrode and the second electrode.

Accelerometer techniques to compensate package stress

Implementations of an accelerometer component may include: a first Z proof mass rotatable about a first axis and coupled to an anchor, the first Z proof mass including a first plurality of electrodes. Implementations may include a second Z proof mass rotatable about the first axis and coupled to the anchor, the second Z proof mass including a second plurality of electrodes. An X-axis accelerometer subcomponent may be located within a perimeter of the first Z proof mass, and a Y-axis accelerometer subcomponent may be located within a perimeter of the second Z proof mass. The first plurality of electrodes and the second plurality of electrodes may be symmetrical about each of the first axis, a second axis perpendicular to the first axis, a third axis diagonal to the first axis and second axis, and a fourth axis diagonal to the first axis and second axis.

Multi-axis accelerometer with reduced stress sensitivity

This document discusses, among other things, a cap wafer and a via wafer configured to encapsulate a single proof-mass 3-axis gyroscope formed in an x-y plane of a device layer. The single proof-mass 3-axis gyroscope can include a main proof-mass section suspended about a single, central anchor, the main proof-mass section including a radial portion extending outward towards an edge of the 3-axis gyroscope sensor, a central suspension system configured to suspend the 3-axis gyroscope from the single, central anchor, and a drive electrode including a moving portion and a stationary portion, the moving portion coupled to the radial portion, wherein the drive electrode and the central suspension system are configured to oscillate the 3-axis gyroscope about a z-axis normal to the x-y plane at a drive frequency.

Micromachined monolithic 3-axis gyroscope with single drive

One example includes an integrated circuit including at least one electrical interconnects disposed on an elongate are extending away from a main portion of the integrated circuit and a microelectromechanical layer including an oscillating portion, the microelectromechanical layer coupled to the main portion of the integrated circuit, wherein the microelectromechanical layer includes a cap comprising a membrane that extends to the integrated circuit.

Sealed packaging for microelectromechanical systems

A method of fabricating a gyroscope may involve depositing conductive material on a substrate, forming an anchor on the substrate, forming a drive frame on the anchor and forming pairs of drive beams on opposing sides of the anchor. The drive beams may be configured to constrain the drive frame to rotate substantially in the plane of the drive beams. The method may involve forming a proof mass around the drive frame and forming a plurality of sense beams that connect the drive frame to the proof mass. The sense beams may be tapered sense beams having a width that decreases with increasing distance from the anchor. The tapered sense beams may be configured to allow sense motions of the proof mass in a sense plane substantially perpendicular to the plane of the drive beams in response to an applied angular rotation. Some components may be formed from plated metal.

Micromachined piezoelectric x-axis gyroscope

This document discusses among other things apparatus and methods for a proof mass including split z-axis portions. An example proof mass can include a center portion configured to anchor the proof-mass to an adjacent layer, a first z-axis portion configure to rotate about a first axis using a first hinge, the first axis parallel to an x-y plane orthogonal to a z-axis, a second z-axis portion configure to rotate about a second axis using a second hinge, the second axis parallel to the x-y plane, wherein the first z-axis portion is configured to rotate independent of the second z-axis portion.

MEMS proof mass with split Z-axis portions

This document refers to multi-die micromechanical system (MEMS) packages. In an example, a multi-die MEMS package can include a controller integrated circuit (IC) configured to couple to a circuit board, a MEMS IC mounted to a first side of the controller IC, a through silicon via extending through the controller IC between the first side and a second side of the controller IC, the second side opposite the first side, and wherein the MEMS IC is coupled to the through silicon via.

Multi-die MEMS package

This disclosure provides systems, methods and apparatus, including computer programs encoded on computer storage media, for making and using gyroscopes. Such gyroscopes may include a sense frame, a proof mass disposed outside the sense frame, a pair of anchors and a plurality of drive beams. The plurality of drive beams may be disposed on opposing sides of the sense frame and between the pair of anchors. The drive beams may connect the sense frame to the proof mass. The drive beams may be configured to cause torsional oscillations of the proof mass substantially in a first plane of the drive beams. The sense frame may be substantially decoupled from the drive motions of the proof mass. Such devices may be included in a mobile device, such as a mobile display device.

This document discusses, among other things, an inertial measurement system including a device layer including a single proof-mass 3-axis accelerometer, a cap wafer bonded to a first surface of the device layer, and a via wafer bonded to a second surface of the device layer, wherein the cap wafer and the via wafer are configured to encapsulate the single proof-mass 3-axis accelerometer. The single proof-mass 3-axis accelerometer can be suspended about a single, central anchor, and can include separate x, y, and z-axis flexure bearings, wherein the x and y-axis flexure bearings are symmetrical about the single, central anchor and the z-axis flexure is not symmetrical about the single, central anchor.

Micromachined 3-axis accelerometer with a single proof-mass

This disclosure provides systems, methods and apparatus, including computer programs encoded on computer storage media, for making and using gyroscopes. Such gyroscopes may include a central anchor, a sense frame disposed around the central anchor, a plurality of sense beams configured for connecting the sense frame to the central anchor and a drive frame disposed around and coupled to the sense frame. The gyroscope may include pairs of drive beams disposed on opposing sides of the sense frame. The gyroscope may include a drive frame suspension for substantially restricting a drive motion of the drive frame to that of a substantially linear displacement along the first axis. The sense frame may be substantially decoupled from drive motions of the drive frame. Such devices may be included in a mobile device, such as a mobile display device.

Micromachined piezoelectric z-axis gyroscope

An example include microelectromechanical die for sensing motion that includes a fixed portion, an anchor coupled to the fixed portion, a first nonlinear suspension member coupled to anchor on a side of the anchor, a second nonlinear suspension member coupled to the anchor on the same side of the anchor, the second nonlinear suspension member having a shape and location mirroring the first nonlinear suspension member about an anchor bisecting plane and a proof-mass that is planar, the proof mass suspended at least in part by the first nonlinear suspension member and the second nonlinear suspension member such that the proof-mass is rotable about the anchor and is slideable in a plane parallel to the fixed portion.

Flexure bearing to reduce quadrature for resonating micromachined devices

Various examples include microelectromechanical die for sensing motion that includes symmetrical proof-mass electrodes interdigitated with asymmetrical stator electrodes. Some of these examples include electrodes that are curved around an axis orthogonal to the plane in which the electrodes are disposed. An example provides vertical flexures coupling an inner gimbal to a proof-mass in a manner permitting flexure around a horizontal axis.

MEMS multi-axis gyroscope Z-axis electrode structure

The device layer of a 6-degrees-of-freedom (6-DOF) inertial measurement system can include a single proof-mass 6-axis inertial sensor formed in an x-y plane, the inertial sensor including: a main proof-mass section suspended about a single, central anchor; a central suspension system configured to suspend the 6-axis inertial sensor from the single, central anchor; and a drive electrode including a moving portion and a stationary portion, the moving portion coupled to the radial portion. The drive electrode and the central suspension system are configured to oscillate the 6-axis inertial sensor about a z-axis normal to the x-y plane.

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Cenk Acar