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.

An inertial measurement apparatus has mechanically bendable beams that have an isosceles trapezoid cross-section. The apparatus has a resonant member having a perimeter at least partially defined by a sidewall slanted at a first angular value and at least one electrode disposed adjacent, and parallel, to the sidewall and separated therefrom by a capacitive gap.

A multi-axis accelerometer may include a proof mass, a first electrode set, and a second electrode set. The first electrode set may detect acceleration along a second axis of the accelerometer, and may include a first electrode (C1) and a second electrode (C2). The second electrode set may detect acceleration along a first axis of the accelerometer that is orthogonal to the second axis, and may include a third electrode (C3) and a fourth electrode (C4). Application of a force along only the second axis may result in the exhibition of a non-zero change in differential capacitance between at least C1 and C2, but a zero net change in the differential capacitance between at least C3 and C4. As such, the accelerometer may exhibit little or no cross axis sensitivity in response to the applied force.

A MEMS tri-axial accelerometer is provided with a sensing structure having: a single inertial mass, with a main extension in a horizontal plane defined by a first horizontal axis and a second horizontal axis and internally defining a first window that traverses it throughout a thickness thereof along a vertical axis orthogonal to the horizontal plane; and a suspension structure, arranged within the window for elastically coupling the inertial mass to a single anchorage element, which is fixed with respect to a substrate and arranged within the window, so that the inertial mass is suspended above the substrate and is able to carry out, by the inertial effect, a first sensing movement, a second sensing movement, and a third sensing movement in respective sensing directions parallel to the first, second, and third horizontal axes following upon detection of a respective acceleration component. In particular, the suspension structure has at least one first decoupling element for decoupling at least one of the first, second, and third sensing movements from the remaining sensing movements.

A sensing assembly device includes a substrate, a chamber above the substrate, a first piezoelectric gyroscope sensor positioned within the chamber, and a first accelerometer positioned within the chamber.

The structure enables two-directional sensing of accelerations with compact component dimensions and with minimal cross-axis sensitivity. The rotation mass includes a first frame and a second frame. In one sense direction, the structure employs a combined proof mass of the first frame and the second frame, which improves the signal to noise level achievable with said device dimensions. In the other sense direction, a detection structure with at least two sensing elements is used to detect displacements of the proof mass of the second frame. Due to the specific internal configuration of the detection structure, signal contributions of the sensing elements in the one direction cancel each other.

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.

A MEMS tri-axial accelerometer is provided with a sensing structure having: a single inertial mass, with a main extension in a horizontal plane defined by a first horizontal axis and a second horizontal axis and internally defining a first window that traverses it throughout a thickness thereof along a vertical axis orthogonal to the horizontal plane; and a suspension structure, arranged within the window for elastically coupling the inertial mass to a single anchorage element, which is fixed with respect to a substrate and arranged within the window, so that the inertial mass is suspended above the substrate and is able to carry out, by the inertial effect, a first sensing movement, a second sensing movement, and a third sensing movement in respective sensing directions parallel to the first, second, and third horizontal axes following upon detection of a respective acceleration component. In particular, the suspension structure has at least one first decoupling element for decoupling at least one of the first, second, and third sensing movements from the remaining sensing movements.

A microelectromechanical accelerometer is provided that includes one or more proof masses. The accelerometer also includes four sets of stator combs that form a set of four measurement capacitors together with rotor combs. Some rotor combs have a positive offset in a direction in the device plane in relation to stator, while others have a negative offset. Some rotor combs have a negative offset in a direction perpendicular to the device plane in relation to stator combs. Moreover, some stator combs have a negative offset in the direction perpendicular to the device plane in relation to rotor combs.

The embodiment relates to a physical quantity sensor that detects physical quantities in a first direction and a second direction which are in-plane directions and perpendicular to each other. The physical quantity sensor includes: a substrate; a first fixed electrode supporting portion; a first fixed electrode portion; a first movable electrode portion; a second fixed electrode supporting portion; a second movable electrode portion; and a first movable electrode supporting portion. The first movable electrode supporting portion is fixed to the substrate at a movable electrode fixing portion, extends in a first intersecting direction intersecting the first direction and the second direction, and supports the first movable electrode portion and the second movable electrode portion via a first spring.