The present application discloses an inertial sensor comprising a proof mass, an anchor, a flexible member and several sensing electrodes. The anchor is positioned on one side of the sensing, mass block in a first axis. The flexible member is connected to the anchor point and extends along the first axis towards the proof mass to connect the proof mass, in which the several sensing electrodes are provided. In this way, the present application can effectively solve the problems of high difficulty in the production and assembly of inertial sensors and poor product reliability thereof.

An inertial sensor is an inertial sensor for detecting a physical quantity based on a displacement in a Z axis when defining three axes perpendicular to each other as an X axis, a Y axis, and the Z axis, and is provided with a substrate, a movable body which is fixed to the substrate, oscillates around an oscillation axis along the X axis, and has two planes opposed to each other and side surfaces connecting the two planes to each other, and a limiter which is fixed to the substrate, and is opposed to the side surfaces of the movable body, wherein the movable body is provided with a resilient portion in a portion opposed to the limiter.

A micromechanical z-inertial sensor. The micromechical z-inertial sensor includes at least one first seismic mass element; and torsion spring elements joined to the first seismic mass element. In each case, first torsion spring elements are connected to a substrate, and second torsion spring elements are connected to the first seismic mass element. A first and a second torsion spring element in each case is joined to one another with the aid of a lever element. The lever element is designed to strike against a stop element.

A sensor includes a movable element adapted for rotational motion about a rotational axis due to acceleration along an axis perpendicular to a surface of a substrate. The movable element includes first and second ends, a first section having a first length between the rotational axis and the first end, and a second section having a second length between the rotational axis and the second end that is less than the first length. A motion stop extends from the second end of the second section. The first end of the first section includes a geometric stop region for contacting the surface of the substrate at a first distance away from the rotational axis. The motion stop for contacting the surface of the substrate at a second distance away from the rotational axis. The first and second distances facilitate symmetric stop performance between the geometric stop region and the motion stop.

A method for temperature compensation of a MEMS sensor. The method includes: in a balancing step, a temperature gradient is produced by a thermal element and a first and a second temperature are determined at a first and a second temperature measurement point, wherein a deflection of a movable structure produced by the temperature gradient is measured and a compensation value is ascertained dependent on the first and second temperature and the deflection; in a measurement step, a physical stimulus is measured by way of a deflection of the movable structure and a third and fourth temperature is determined at the first and second temperature measurement points; in a compensation step, a measured value of the physical stimulus is ascertained dependent on the measured deflection, the third and fourth temperature and the compensation value. A method is also provided including: a regulation step, and a measurement step.

A force sensor including a support, a test body, two strain gauges, mechanical transmission means between the test body and the strain gauges so that a movement of the test body applies a strain onto the strain gauges in a first direction of the plane of the sensor, the transmission means being hinged relative to the support about a second direction in the plane of the sensor, the test body being accommodated within a first volume, the strain gauges being accommodated within a second volume, insulated by sealed insulation means. The sensor includes a sacrificial layer, a nanometric layer, a protective layer and a micrometric layer. The test body and at least one portion of the support are formed in the substrate, the sealed insulation means are partially formed by the nanometric layer and by the sacrificial layer, and the strain gauges are formed in the nanometric layer.

An inertial sensor includes: a substrate; a fixing part arranged at one surface of the substrate; a moving element having an opening and configured to swing about a rotation axis along a first direction; a support beam supporting the moving element as the rotation axis in the opening of the moving element; and a support part supporting the support beam. The support part includes a first part fixed to the fixing part, and a second part formed only of a part not fixed to the fixing part. A length in the first direction of the second part is longer than a length in the first direction of the first part.

The present invention discloses a three-axis accelerometer. The three-axis accelerometer comprises: a substrate; at least one anchor block fixedly disposed on the substrate; a first X-axis electrode, a second X-axis electrode, a first Y-axis electrode, a second Y-axis electrode, a first Z-axis electrode and a second Z-axis electrode all fixedly disposed on the substrate; a framework suspended above the substrate and comprising a first beam column, a second beam column disposed opposite to the first beam column and at least one connecting beam connecting the first beam column and the second beam column; a proof mass suspended above the substrate; and at least one elastic connection component configured to elastically connect to the at least anchor block, the connecting beam, and the proof mass. The three-axis accelerometer can realize high-precision acceleration detection on three axes with only one proof mass, and in particular, can provide a fully differential detection signal for the Z axis, thereby greatly improving detection precision.

A self-calibration method for an accelerometer having a proof mass separated by a gap from a drive electrode and a sense electrode includes initializing the accelerometer to resonate, applying a first bias voltage to the sense electrode and a second bias voltage to the drive electrode to obtain a first scale factor, measuring a first acceleration over a first time interval, swapping the first bias voltage on the sense electrode with the second bias voltage previously on the drive electrode and the second bias voltage on the drive electrode with the first bias voltage previously on the sense electrode so that a bias voltage on the sense electrode is set to the second bias voltage and a bias voltage on the drive electrode is set to the second bias voltage to obtain a second scale factor, measuring a second acceleration over a second time interval, and calculating a true acceleration.

A micromechanical sensor. The sensor includes a substrate, a cap element situated on the substrate, at least one seismic mass that is deflectable orthogonal to the cap element, an internal pressure that is lower by a defined amount relative to the surrounding environment prevailing inside a cavity, and a compensating element designed to provide a homogenization of a temperature gradient field in the cavity during operation of the micromechanical sensor.