Analog Devices,inc.

Jeffrey A Gregory

Igor P Prikhodko

Charles Blackmer

Laura Cornelia Popa

John Albert Geen

Jinbo Kuang

Tyler Adam Dunn

Eugene Oh Hwang

Kemiao Jia

Bradley C Kaanta

Nikolay Pokrovskiy

Erdinc Tatar

See-Ho Tsang

Kuang L Yang

Thomas Kieran Nunan

Li Chen

Gaurav Vohra

Columnar multi-axis microelectromechanical systems (MEMS) devices (such as gyroscopes) balanced against undesired linear and angular vibration are described herein. In some embodiments, the columnar MEMS device may comprise at least two multiple-mass columns, each having at least three proof masses and being configured to sense rotation about a respective axis. The motion and mass of the proof masses may be controlled to achieve linear and rotational balancing of the MEMS device. The columnar MEMS device may further comprise one or more modular drive structures disposed alongside each multiple-mass column to facilitate displacement of the proof masses of a respective column. The MEMS devices described herein may be used to sense roll, yaw, and pitch angular rates.

3-axis gyroscope with rotational vibration rejection

Microelectromechanical system (MEMS) inertial sensors exhibiting reduced parasitic capacitance are described. The reduction in the parasitic capacitance may be achieved by forming localized regions of thick dielectric material. These localized regions may be formed inside trenches. Formation of trenches enables an increase in the vertical separation between a sense capacitor and the substrate, thereby reducing the parasitic capacitance in this region. The stationary electrode of the sense capacitor may be placed between the proof mass and the trench. The trench may be filled with a dielectric material. Part of the trench may be filled with air, in some circumstances, thereby further reducing the parasitic capacitance. These MEMS inertial sensors may serve, among other types of inertial sensors, as accelerometers and/or gyroscopes. Fabrication of these trenches may involve lateral oxidation, whereby columns of semiconductor material are oxidized.

Low-parasitic capacitance MEMS inertial sensors and related methods

Couplers for selectively coupling in-plane and out-of-plane motion between moving masses are provided herein. In particular, aspects of the present application provide for a coupler configured to couple in-plane motion between moving masses while decoupling out-of-plane motion between the moving masses. The selective couplers as described herein may be used in a device, such as a microelectromechanical systems (MEMS) inertial sensor. In some embodiments, a MEMS inertial sensor comprises a first mass configured to move in-plane, a second mass configured to move in-plane and out-of-plane, and a coupler coupling the first and second masses and comprising two levers coupled to an anchor point by respective tethers and coupled to each other by a spring.

Mechanism for selective coupling in microelectromechanical systems inertial sensors

Microelectromechanical systems (MEMS) devices (such as gyroscopes) configured to reject quadrature motion are described. Quadrature motion arises for example when the drive motion of a gyroscope couples to the sense motion of a gyroscope even in the absence of an angular motion. In some circumstances, quadrature motion may result from the fact that the springs used in a gyroscope have slanted sidewall, which can impart torque in the mechanics of the gyroscope. MEMS gyroscope of the type described herein may be configured to reject quadrature motion by using only springs oriented substantially parallel to the drive direction. One such spring includes only beams parallel the drive directions, and optionally. These MEMS gyroscopes may be used to sense, among others, roll and pitch angular rates.

MEMS gyroscopes with in-line springs and related systems and methods

Novel structural features applicable to a variety of inertial sensors. A composite ring composed of concentric subrings is supported by a compliant support structure suspending the composite ring relative to a substrate. The compliant support structure may either be interior or exterior to the composite ring. The compliant support may be composed of multiple substantially concentric rings coupled to neighboring rings by transverse members regularly spaced at intervals that vary with radius relative to a central axis of symmetry. Subrings making up the composite ring may vary in width so as to provide larger displacement amplitudes at intermediate radii, for example. In other embodiments, electrodes are arranged to reduce sensitivity to vibration and temperature, and shock stops are provided to preclude shorting in response to shocks.

Ring gyroscope structural features

Micromachined inertial devices are presented having multiple linearly-moving masses coupled together by couplers that move in a linear fashion when the coupled masses exhibit anti-phase motion. The couplers move in opposite directions of each other, such that one coupler on one side of the movable masses moves in a first linear direction and another coupler on the opposite side of the movable masses moves in a second linear direction opposite the first linear direction. The couplers ensure proper anti-phase motion of the masses.

Balanced runners synchronizing motion of masses in micromachined devices

Micromachined inertial devices are presented having multiple linearly-moving masses coupled together by couplers that move in a linear fashion when the coupled masses exhibit linear anti-phase motion. Some of the described couplers are flexural and provide two degrees of freedom of motion of the coupled masses. Some such couplers are positioned between the coupled masses. Using multiple couplers which are arranged to move in linearly opposite directions during linear anti-phase motion of the coupled masses provides momentum-balanced operation.

Flexural couplers for microelectromechanical systems (MEMS) devices

Synchronized mass gyroscope

The cap wafer for a MEMS device includes multiple electrically isolated electrodes that can be bonded and electrically connected to separate electrical contacts on a MEMS device wafer. The electrically isolated electrodes can be used for any of a variety of functions, such as for apply a force to a movable MEMS structure on the MEMS device wafer (e.g., for driving resonance of the movable MEMS structure or for adjusting a resonance or sense mode of the movable MEMS structure) or for sensing motion of a movable MEMS structure on the MEMS device wafer. Since the electrodes are electrically isolated, different electrodes may be used for different functions.

MEMS sensor cap with multiple isolated electrodes

One or more conductive shielding plates are formed in a standard ASIC wafer top metal layer, e.g., for blocking cross-talk from MEMS device structure(s) on the MEMS wafer to circuitry on the ASIC wafer when the MEMS device is capped directly by the ASIC wafer in a wafer-level chip scale package. Generally speaking, a shielding plate should be at least slightly larger than the MEMS device structure it is shielding (e.g., a movable MEMS structure such as an accelerometer proof mass or a gyroscope resonator), and the shielding plate cannot be in contact with the MEMS device structure during or after wafer bonding. Thus, a recess is formed to ensure that there is sufficient cavity space away from the top surface of the MEMS device structure. The shielding plate is electrically conductive and can be biased, e.g., to the same voltage as the opposing MEMS device structure in order to maintain zero electrostatic attraction force between the MEMS device structure and the shielding plate.

Apparatus and method for shielding and biasing in MEMS devices encapsulated by active circuitry

A method compensates for a sensitivity of an inertial sensor having a resonator and an accelerometer. The method includes adding a test signal to a quadrature tuning voltage applied to the resonator of the inertial sensor. The method also includes receiving a quadrature error signal from the accelerometer of the inertial sensor. The method also includes detecting a phase difference between the quadrature error signal and the test signal. The method also includes determining a bandwidth of the accelerometer based on the detected phase difference, the bandwidth indicating the sensitivity of the accelerometer.

Gyroscope that compensates for fluctuations in sensitivity

Methods and apparatus for sensing linear acceleration with a MEMS resonator mass, alone, or concurrently with sensing rate of rotation. A resonator mass, which may be a disk or a ring structure, is driven at a resonance frequency of one of the vibration modes of the resonator mass. The amplitude of vibration of that mode is sensed by a set of at least two drive-sense electrodes disposed at opposing positions across the resonator mass. A linear acceleration is derived based at least on a difference between signals of the opposing electrodes. Linear acceleration may be sensed in multiple orthogonal dimensions using multiple pairs of opposing electrodes. Rotation rate may be derived concurrently by sensing the energy coupled into an orthogonal mode of the resonator mass.

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Malden, MA, United States of America

Jeffrey A Gregory