Gyro sensor and composite sensor comprising gyro sensor

• US 9,696,158 B2
• Filed: 11/27/2013
• Issued: 07/04/2017
• Est. Priority Date: 11/29/2012
• Status: Active Grant

• Current Assignee: DENSO Corporation, Kyoto University
• Original Assignee: DENSO Corporation, Kyoto University
• Inventors: Jomori, Tomoya, Tsuchiya, Toshiyuki
• Primary Examiner(s): Schmitt, Benjamin
• Application Number:
  US14/646,920
• Publication Number:
  US 20150308828A1
• Time in Patent Office: 1,315 Days
• Field of Search: 7350402, 7350412, 7350415
• CPC Class Codes: G01C 19/5705 using masses driven in reciprocating rotary motion about an axis
• CPC Class Codes: G01C 19/5712 the devices involving a micromechanical structure
• CPC Class Codes: G01C 19/574 the devices having two sensing masses in anti-phase motion
• CPC Class Codes: G01C 19/5747 each sensing mass being connected to a driving mass, e.g. driving frames

Abstract

In a gyro sensor, two detection weights are placed in an outer drive weight to be arranged in an x-axis direction and coupled to each other via a coupling spring. By thus coupling the two detection weights via the coupling spring, it is possible to separate an in-phase-mode resonant frequency fin and an anti-phase-mode resonant frequency fanti from each other. As a result, it is possible to provide the gyro sensor which can suppress an output error on receiving an impact and perform more precise angular velocity detection.

Claims

1. A gyro sensor comprising:

a substrate including a fixed portion;

a movable portion connected to the fixed portion via a support beam and including a drive weight having a mass portion, wherein a plane being parallel with a planar surface of the substrate and including an x-axis and a y-axis orthogonal to the x-axis is referred to as an xy plane, a direction along the x-axis is referred to as an x-axis direction, and a direction along the y-axis is referred to as a y-axis direction, and wherein, when an angular velocity is detected, the mass portion is reciprocally rotationally vibrated in the xy plane or reciprocally vibrated in the y-axis direction on the basis of a displacement of the support beam;

two detection weights connected to the drive weight via detection beams and arranged in the x-axis direction;

a coupling spring coupling the two detection weights to each other; and

detection electrodes placed to be spaced apart at predetermined distances from the two detection weights in a z-axis direction as a direction along a z-axis perpendicular to the xy plane,

wherein it is configured that, as a result of an application of the angular velocity, the two detection weights are vibrated oppositely in the z-axis direction to cause changes in the respective distances between the two detection weights and the detection electrodes and cause anti-phase changes in capacitance values of two capacitors formed between the two detection weights and the detection electrodes and, on the basis of the anti-phase changes in the capacitance values, the angular velocity is detected using a differential output of signals showing the changes in the two capacitance values, and

wherein the coupling spring includes torsion springs connected respectively to the two detection weights, and a middle rigid body coupling the torsion spring connected to one of the detection weights to the torsion spring connected to the other detection weight.

2. The gyro sensor according to claim 1, wherein each of the two detection weights has a cantilever structure in which one of two end portions of each detection weight is supported by and connected to a respective detection beam and, when the angular velocity is applied, the respective detection beam is used as a node to displace a one of the end portions of each detection weight that is opposite to the end portion connected to the respective detection beam.

3. The gyro sensor according to claim 2, wherein each of the two detection weights is connected to the respective detection beam on a side of each detection weight that is closer to a center of the mass portion.

4. The gyro sensor according to claim 1,

wherein the fixed portion includes driving fixed electrodes,

wherein the movable portion includes driving movable electrodes provided at an outer periphery of the mass portion configured to have an annular shape, and

wherein, during the detection of the angular velocity, electrostatic attraction forces are generated between the driving fixed electrodes and the driving movable electrodes to rotationally vibrate the drive weights about a center of the mass portion as a rotation center.

5. A composite sensor comprising:

a first gyro sensor which is the gyro sensor according to claim 1;

a second gyro sensor formed on the substrate to detect an angular velocity around the z-axis in the xy plane; and

an acceleration sensor formed on the substrate to detect an acceleration in one direction parallel with the xy plane,

wherein the first gyro sensor, the second gyro sensor, and the acceleration sensor are integrated in one chip.

6. The gyro sensor according to claim 1, wherein the two detection weights are spaced apart and symmetrical, and the coupling spring is located between the detection weights.

7. The gyro sensor according to claim 6, wherein the torsion springs are spaced apart and the middle rigid body is located between the torsion springs.

8. The gyro sensor according to claim 6, wherein each of the torsion springs has a rectangular-frame shape.

9. A gyro sensor comprising:

a substrate including a fixed portion;

a movable portion connected to the fixed portion via detection beams and including two detection weights each having a mass portion, wherein a plane being parallel with a planar surface of the substrate and including an x-axis and a y-axis orthogonal to the x-axis is referred to as an xy plane, a direction along the x-axis is referred to as an x-axis direction, and a direction along the y-axis is referred to as a y-axis direction, and wherein, when an angular velocity is detected, the mass portion is reciprocally rotationally rotated in the xy plane or reciprocally vibrated in the y-axis direction on the basis of a displacement of each of the detection beams;

two drive weights formed integrally with the two detection weights and arranged in the x-axis direction;

a coupling spring coupling the two detection weights to each other; and

detection electrodes placed to be spaced apart at predetermined distances from the two detection weights in a z-axis direction as a direction along a z-axis perpendicular to the xy plane,

wherein it is configured that, as a result of an application of the angular velocity, the two detection weights are vibrated oppositely in the z-axis direction to cause changes in the respective distances between the two detection weights and the detection electrodes and cause anti-phase changes in capacitance values of two capacitors formed between the two detection weights and the detection electrodes and, on the basis of the anti-phase changes in the capacitance values, the angular velocity is detected using a differential output of signals showing the changes in the two capacitance values, and

wherein the coupling spring includes torsion springs connected respectively to the two detection weights, and a middle rigid body coupling the torsion spring connected to one of the detection weights to the torsion spring connected to the other detection weight.

10. The gyro sensor according to claim 9, wherein the two detection weights are spaced apart and symmetrical, and the coupling spring is located between the detection weights.

11. The gyro sensor according to claim 10, wherein the torsion springs are spaced apart and the middle rigid body is located between the torsion springs.

12. The gyro sensor according to claim 10, wherein each of the torsion springs has a rectangular-frame shape.

13. The gyro sensor according to claim 9, wherein each of the two detection weights has a cantilever structure in which one of two end portions of each detection weight is supported by and connected to a respective one of the detection beams, and when the angular velocity is applied, the respective detection beam is used as a node to displace a one of the end portions of each detection weight that is opposite to the end portion connected to the respective detection beam.

14. The gyro sensor according to claim 13, wherein the one of two end portions of the detection weight supported by the respective detection beam is closer to the corresponding torsion spring of the coupling spring than the other of the two end portions of each detection weight.