Murata Manufacturing Co., Ltd.

Murata Electronics Oy

Vti Technologies Oy

Anssi Blomqvist

Ville-Pekka Rytkönen

Matti Liukku

Jaakko Ruohio

Altti Torkkeli

Heikki T Kuisma

Petri Klemetti

Kaisa Nera

Antti Lipsanen

Lasse Aaltonen

Ville Pekka Rytkönen

Leif Roschier

Hannu Vesterinen

Ulf Meriheinä

Pekka Kostiainen

Jouni Erkkilä

Marcus Rinkiö

Tommi Piirainen

Ossi Kauppinen

Tero Sillanpää

Mikko Partanen

Sten Stockmann

Matii Liukku

An accelerometer comprising a first proof mass and a second proof mass which are coupled to each other with a coupling structure which extends from the first proof mass to the second proof mass. The coupling structure synchronizes the movement of the first and second proof masses so that the first and second proof masses may be linearly displaced from their rest position in the x-direction, rotationally displaced in opposite in-plane directions and rotationally displaced in opposite out-of-plane directions.

Three-axis accelerometer with two masses

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.

In-plane and out-of-plane accelerometer

A gyrocompass device is provided for determining a heading relative to a surface of a rotating planetary body. The gyrocompass device includes one or more MEMS gyroscopes that are each fixed in an orientation on a substrate that is parallel to a first plane and that each provide three or more sense axes that lie within the first plane and are each offset from one another by an offset angle. Moreover, a heading determiner receives rotation rates from the three sense axes and determines the heading of the gyrocompass device relative to the surface of the rotating planetary body by fitting a sine or cosine function to the received rotation rates from the one or more MEMS gyroscopes.

MEMS gyrocompass

The invention relates to the field of microelectromechanical systems (MEMS) gyroscopes. The MEMS gyroscope of the present invention drives oscillation of at least one proof mass in a primary drive mode at a first frequency and in a secondary drive mode at a second frequency, different to the first frequency. The primary drive mode and secondary drive mode are orthogonal. Sense circuitry measures oscillation of the at least one proof mass in a sense mode, which is orthogonal to the primary drive mode and the secondary drive mode, in order to determine the angular rate of rotation of the MEMS gyroscope about sense axes parallel to the movement of the at least one proof mass in the primary and secondary drive modes.

MEMS gyroscope

A microelectromechanical accelerometer for measuring acceleration, comprising a first proof mass and ae second proof mass. The first proof mass is adjacent to the second proof mass. A suspension structure allows the first proof mass to undergo rotation out of the device plane about a first rotation axis and the suspension structure allows the second proof mass to undergo rotation out of the device plane about a second rotation axis. The first and second rotation axes are parallel to each other and define an x-direction which is parallel to the first and the second rotation axes and a y-direction which is perpendicular to the x-direction. The y-coordinate of the first rotation axis is greater than the y-coordinate of the second rotation axis by a nonzero distance D.

Seesaw accelerometer

An accelerometer for measuring acceleration in the direction of a z-axis which is perpendicular to an xy-plane, where a first proof mass is suspended from a first side anchor point with a first suspension structure which allows the first proof mass to undergo rotation about a first rotation axis. A second proof mass is suspended from a second side anchor point with a second suspension structure. The second suspension structure allows the second proof mass to undergo rotation about a second rotation axis. The torsion elements in the first and second suspension structure lie further away from the center of the accelerometer than the corresponding side anchor points from which the masses are suspended.

Accelerometer with two seesaws

A microelectromechanical gyroscope comprising first, second, third and fourth Coriolis masses, arranged in that order on an x-axis. In the primary oscillation mode, the Coriolis masses are configured to oscillate so that the second and third Coriolis masses move in linear translation along the x-axis away from a center point when the first and fourth Coriolis masses move in linear translation along the x-axis towards the first center point, and vice versa. When the gyroscope undergoes rotation about a y-axis which is perpendicular to the x-axis, the Coriolis masses are configured to oscillate so that the first, second, third and fourth Coriolis masses undergo vertical motion in a z-direction, wherein the first and third Coriolis masses move up when the second and fourth Coriolis masses move down, and vice versa.

Gyroscope with mass pairs

The present invention relates to MEMS (microelectromechanical systems) accelerometers, in particular to an accelerometer designed to reduce error in the accelerometer output. The MEMS accelerometer includes a proof mass, which is capable of movement along at least two perpendicular axes and at least one measurement structure. The proof mass is mechanically coupled to the measurement structure along the sense axis of the measurement structure, such that movement of the proof mass along the sense axis causes the moveable portion of the measurement structure to move, and is decoupled from the measurement structures along an axis or axes perpendicular to the sense axis of the measurement structure, such that movement of the proof mass perpendicular to the sense axis of the measurement structure does not cause the moveable portion of the measurement structure to move.

MEMS accelerometer with mechanically decoupled proof mass

A gyroscope comprises four Coriolis masses arranged around a center point where a lateral axis crosses a transversal axis orthogonally in the device plane. The first and second masses are aligned on the lateral axis, and the third and fourth masses are aligned on the transversal axis. The gyroscope further comprises four pairs of elongated mass elements. The mass elements of the first pair are transversally aligned on opposite sides of the lateral axis outside of the first mass. The mass elements of the second pair are transversally aligned on opposite sides of the lateral axis outside of the second mass. The mass elements of the third pair are laterally aligned on opposite sides of the first transversal axis outside of the third mass. The mass elements of the fourth pair are laterally aligned on opposite sides of the first transversal axis outside of the fourth mass.

Gyroscope with peripheral detection

A gyroscope with a first Coriolis mass quartet and a second Coriolis mass quartet arranged around two quartet center points, and two elongated mass elements or synchronization bars aligned with each other outside of each Coriolis mass. One end of each elongated mass element and synchronization bar is attached to the corresponding Coriolis mass. Each elongated mass element is suspended from a peripheral anchor point by a mass element suspension arrangement which allows said elongated mass element to undergo rotational motion both in the device plane and out of the device plane. Each elongated synchronization bar is suspended from a peripheral anchor point by a synchronization bar suspension arrangement which allows said elongated synchronization bar to undergo rotational motion both in the device plane and out of the device plane substantially around its midpoint.

Multiaxis gyroscope with supplementary masses

The invention relates to microelectromechanical systems (MEMS), and specifically to a mirror system, for example to be used in LiDAR (Light Detection and Ranging). The MEMS mirror system of the invention uses four suspenders, each of which is connected to the reflector body at two separate connection points which can be independently displaced by piezoelectric actuators. By actuating adjacent and opposite pairs of piezoelectric actuators, the reflector body can be driven to oscillated about two orthogonal axes.

Two-axis MEMS mirror with separated drives

The present invention provides a high-accuracy low-noise MEMS accelerometer by using at least two symmetric out-of-plane proof masses for both out-of-plane and in-plane axes. Movement of the proof masses in one or more in-plane sense axes is measured by comb capacitors with mirrored comb electrodes that minimise cross-axis error from in-plane movement of the proof mass out of the sense axis of the capacitor. The two out-of-plane proof masses rotate in opposite directions, thus maintaining their combined centre of mass at the centre of the accelerometer even as they rotate out of plane.

Low-noise multi-axis MEMS accelerometer

This disclosure describes a multiaxis gyroscope comprising a first proof mass quartet centered around a first quartet center point and a second proof mass quartet centered around a second quartet center point. The phase of the primary oscillation of each proof mass in the first proof mass quartet in relation to the first quartet center point is anti-phase in relation to the phase of the primary oscillation of the corresponding proof mass in the second proof mass quartet in relation to the second quartet center point. The phase of the primary oscillation of the first and second proof masses in each proof mass quartet in relation to the corresponding quartet center point is anti-phase in relation to the phase of the primary oscillation of the third and fourth proof masses in the same proof mass quartet in relation to the same quartet center point.

Vibration-robust multiaxis gyroscope

The present invention provides a high-accuracy low-noise MEMS accelerometer by using a larger, single proof mass to measure acceleration along two orthogonal axes. A novel arrangement of electrodes passively prevents cross axis error in the acceleration measurements. Novel arrangements of springs and a novel proof mass layout provide further noise reduction.

Low-noise multi axis MEMS accelerometer

The present invention relates to a capacitive MEMS gyroscope with drive-signal induced offset cancelling features. In a MEMS gyroscope of the type including force feedback circuitry, the drive signal is modulated according to a known modulation scheme or frequency. The modulation scheme/frequency of the drive signal is used by offset cancelling circuitry to determine the offset in the rate signal caused by the drive signal. The determined offset is subsequently removed from the rate signal.

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Helsinki, Finland

Anssi Blomqvist