INTEGRATED MICROELECTROMECHANICAL SYSTEMS (MEMS) VIBRATING MASS Z-AXIS RATE SENSOR

• US 20090114016A1
• Filed: 11/05/2007
• Published: 05/07/2009
• Est. Priority Date: 11/05/2007
• Status: Active Grant

• Current Assignee: Invensense Incorporated (TDK Corporation)
• Original Assignee: Invensense Incorporated (TDK Corporation)
• Inventors: SEEGER, Joe, NASIRI, Steven, BOROVIC, Bruno
• Granted Patent: US 7,677,099 B2
• Time in Patent Office: Days
• US Class Current: 73/504.120
• CPC Class Codes: G01C 19/5719 using planar vibrating masses driven in a translation vibration along an axis

Abstract

A sensor that measures angular velocity about an axis that is normal to a sensing plane of the sensor. The sensor comprises a sensing subassembly that includes a planar frame parallel to the sensing plane, a first proof mass disposed in the sensing plane, a second proof mass disposed in the sensing plane laterally to the first proof mass, and a linkage within the frame and connected to the frame. The linkage is connected to the first proof mass and to the second proof mass. The sensor further includes actuator for driving the first proof mass and the second proof mass into oscillation along a drive axis in the sensing plane. The sensor further includes a first transducer to sense motion of the frame in response to a Coriolis force acting on the oscillating first proof mass and the oscillating second proof mass.

Claims

1. A sensor configure to measure angular velocity about an axis that is normal to a sensing plane of the angular rate sensor, the angular rate sensor comprising:

a sensing subassembly comprising

a substantially planar frame parallel to the sensing plane;

a first proof mass disposed in the sensing plane;

a second proof mass disposed in the sensing plane laterally to the first proof mass; and

a linkage within the frame and connected to the frame, the linkage being connected to the first proof mass and to the second proof mass;

an actuator for driving the first proof mass and the second proof mass into oscillation along a drive axis in the sensing plane, the actuator to drive the first proof mass and the second proof mass 180 degrees out-of-phase;

a first transducer to sense motion of the frame in response to a Coriolis force acting on the oscillating first proof mass and the oscillating second proof mass; and

a base plate which is parallel to the sensing plane and to which the sensing subassembly is attached.

2. The sensor of claim 1, wherein:

the actuator comprises an electrostatic actuator; and

the first transducer comprises a capacitive sensor.

3. The sensor of claim 2, wherein the capacitive sensor comprises a plurality of interdigitated comb electrodes configured to differentially measure motion of the frame.

4. The sensor of claim 2, wherein the capacitive sensor comprises a plurality of parallel plate electrodes configured to differentially measure motion of the frame.

5. The sensor of claim 1, further comprising a plurality of flexures configured to connect the base plate to the frame such that the frame is able to rotate about a central axis normal to the sensing plane.

6. The sensor of claim 1, wherein:

coupling between the linkage and the first proof mass and coupling between the linkage and the second proof mass are compliant along the drive axis; and

coupling between the linkage and the frame is compliant along the drive axis.

7. The sensor of claim 1, wherein the first proof mass and the second proof mass are coupled to the frame.

8. The sensor of claim 1, wherein the sensing subassembly further includes:

a first actuator mass within the frame and coupled to the first proof mass; and

a second actuator mass within the frame and coupled to the second proof mass;

wherein the actuator respectively drives the first proof mass and the second proof mass into oscillation indirectly through the first actuator mass and the second actuator mass.

9. The sensor of claim 8, wherein the first actuator mass is coupled to the base plate and the second actuator mass is coupled to the base plate.

10. The sensor of claim 8, wherein the first actuator mass is coupled to the frame and the second actuator mass is coupled to the frame.

11. The sensor of claim 8, wherein:

the first actuator mass is rotatable around a first axis normal to the sensing plane and is able to move along the drive axis; and

the second actuator mass is rotatable around a second axis normal to the sensing plane and is able to move along the drive axis.

12. The sensor of claim 11, wherein coupling from the first proof mass to the linkage and coupling from the second proof mass to the linkage are compliant with respect to the rotation around the axis normal to the plane.

13. The sensor of claim 11, further comprising a first spring system and a second spring system configured to respectively amplify a substantially small oscillation of the first actuator mass and the second actuator mass into a substantially larger oscillation of the first proof mass and the second proof mass.

14. The sensor of claim 8, wherein:

the first actuator mass and the second actuator mass are able to substantially move only along the drive axis,

wherein the first proof mass is rigidly coupled to the first actuator mass along the drive axis such that the first actuator and the first proof mass move substantially together, and the second proof mass is rigidly coupled to the second actuator mass along the drive axis such that the second actuator and the second proof mass move substantially together, and

wherein the first proof mass is coupled to the first actuator mass such the first proof mass is rotatable around the drive axis, and the second proof mass is coupled to the second actuator mass such the second proof mass is rotatable around the drive axis.

15. The sensor of claim 14, wherein the coupling from the first proof mass to the linkage and the coupling from the second proof mass to the linkage is rigid with respect to the rotation around an axis normal to the sensing plane.

16. The sensor of claim 1, wherein the actuator comprises a plurality of differential drive electrodes.

17. The sensor of claim 1, wherein the actuator comprises a plurality of single-ended drive electrodes.

18. The sensor of claim 1, wherein the sensing subassembly further comprises a second transducer to sense the amplitude of the oscillation of the first proof mass and the second proof mass and provide feedback to the actuator for driving the oscillation of the first proof mass and the second proof mass at a resonant frequency.

19. The sensor of claim 18, wherein the second transducer is capacitive.

20. The sensor of claim 1, wherein the frame is substantially circular.

21. The sensor of claim 1, wherein the frame is substantially rectangular.

22. The sensor of claim 1, wherein the base plate comprises a single crystal silicon wafer.

23. The sensor of claim 22, wherein the base plate comprises an integrated CMOS wafer having drive and sense electronics.

24. The sensor of claim 23, wherein the sensor assembly further comprises a cover plate including a layer of insulator, the cover plate being attached to the sensing subassembly to form a complete hermetic seal enclosure of the first proof mass and the second proof mass.

25. The sensor of claim 24, further comprising anchors to anchor the sensing subassembly to the cover plate.

26. The sensor of claim 25, wherein the sensor assembly includes a seal ring that hermetically seals the sensing subassembly to the CMOS wafer via eutectic or metal bonding while maintaining a fixed gap between the base plate and the CMOS wafer.

27. The sensor of claim 26, wherein the sensor assembly further includes a plurality of stand offs that permit creation of electrical interconnects from the sensing subassembly to the CMOS wafer, the electrical interconnects being formed by the eutectic or metal bonding.

28. The sensor of claim 27, wherein the eutectic or metal bonding comprises an aluminum and germanium alloy.