Micromachined torsional gyroscope with anti-phase linear sense transduction

• US 20100095768A1
• Filed: 10/20/2008
• Published: 04/22/2010
• Est. Priority Date: 10/20/2008
• Status: Abandoned Application

• Current Assignee: Custom Sensors & Technologies Incorporated (Schneider Electric SE)
• Original Assignee: Custom Sensors & Technologies Incorporated (Schneider Electric SE)
• Inventors: Mao, Minyao, Acar, Cenk
• Application Number:
  US12/254,223
• Publication Number:
  US 20100095768A1
• Time in Patent Office: Days
• US Class Current: 73/504.04
• CPC Class Codes: G01C 19/56 Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
• CPC Class Codes: G01C 19/5712 the devices involving a micromechanical structure

Abstract

Micromachined gyroscope having a pair of masses disposed generally in a plane and driven for out-of-plane torsional oscillation about a pair of drive axes in the plane for sensing rotation about an input axis perpendicular to the drive axes. The masses are mounted for in-plane torsional movement about sense axes perpendicular to the drive axes and the input axis in response to Coriolis forces produced by rotation of the masses about the input axis. A link connects the two masses together for movement of equal amplitude and opposite phase both about the drive axes and about the sense axes. The masses are connected to transducers having input electrodes constrained for linear in-plane movement relative to stationary electrodes, with that torsional movement of the masses about the sense axes producing changes in capacitance between the input electrodes and the stationary electrodes.

Claims

1. A micromachined gyroscope, comprising:

a pair of masses disposed generally in a plane and driven for out-of-plane torsional oscillation about a pair of drive axes in the plane, an input axis perpendicular to the drive axes, sense axes perpendicular to the drive axes and the input axis, means mounting the masses for in-plane torsional movement about the sense axes in response to Coriolis forces produced by rotation of the masses about the input axis, a link connecting the two masses together for movement of equal amplitude and opposite phase both about the drive axes and about the sense axes, transducers having input electrodes constrained for linear in-plane movement relative to stationary electrodes, and link beams interconnecting the masses and the input electrodes so that torsional movement of the masses about the sense axes produces changes in capacitance between the input electrodes and the stationary electrodes.

2. The micromachined gyroscope of claim 1 wherein the transducers are positioned on opposite sides of each of the two masses and arranged such that the capacitances of the transducers on opposite sides of each mass change in an anti-phase manner and the capacitances of the transducers on the same sides of the two masses change in an in-phase manner.

3. The micromachined gyroscope of claim 1 wherein the masses are suspended from anchors disposed centrally of the masses, the transducers are located on opposite sides of the anchors, and the link beams are connected to the masses on sides of transducers farthest from the anchors.

4. The micromachined gyroscope of claim 1 wherein the masses are suspended from anchors disposed centrally of the masses, the transducers are located on opposite sides of the anchors, and the link beams are connected to the masses on sides of transducers closest to the anchors.

5. The micromachined gyroscope of claim 1 wherein the transducers have shuttles on which the input electrodes are mounted, with the link beams being connected to the shuttles and the shuttles being constrained for in-plane linear movement.

6. The micromachined gyroscope of claim 5 wherein the electrodes are in the form of generally planar, parallel plates, and the shuttles are suspended by beams which extend in a direction parallel to the plates and are flexible in a direction perpendicular to the plates.

7. The micromachined gyroscope of claim 6 wherein the shuttles are in the form of frames, the input electrode plates extend toward each other from opposite sides of the frames, and the stationary electrodes are in the form of spaced apart parallel plates which are mounted on anchors within the frames and interleaved with the input electrode plates.

8. The micromachined gyroscope of claim 6 wherein the stationary electrodes are in the form of spaced apart parallel plates which are mounted on stationary frames and extend toward each other from opposite sides of the frames, and the shuttles are positioned within the frames with the input electrode plates extending outwardly from the shuttles and being interleaved with the stationary electrode plates.

9. The micromachined gyroscope of claim 1 wherein transducers are positioned on opposite sides of each of the masses, with the transducers on one side having input electrodes on opposite sides of stationary electrodes and the transducers on the same sides of the masses having input electrodes on the same sides of stationary electrodes so that the capacitances of both transducers on the one side change in the same direction and the capacitances of the transducers on the same sides change in opposite directions in response to anti-phase torsional movement of the masses about the sense axes.

10. A micromachined gyroscope, comprising:

first and second masses disposed side-by-side in a plane, beams suspending the masses from anchors located centrally of the masses for torsional out-of-plane movement about a pair of drive axes in the plane and for torsional in-plane movement about sense axes perpendicular to the plane, means connecting the two masses together for movement of equal amplitude and opposite phase both about the drive axes and about the sense axes, with Coriolis forces produced by rotation of the masses about an input axis producing torsional movement of the masses about the sense axes, first and second transducers positioned on opposite sides of the first mass, third and fourth transducers positioned on opposite sides of the second mass, link beams interconnecting the masses and the transducers so that torsional movement of the masses about the sense axes produces changes in capacitance in the transducers corresponding to rotation of the masses about the input axis.

11. The micromachined gyroscope of claim 10 wherein the capacitances of the first and third transducers change in one direction and the capacitances of the second and fourth transducers change in an opposite direction in response to anti-phase movement of the masses about the sense axes.

12. The micromachined gyroscope of claim 11 including means for detecting a total change in the capacitances of the transducers in accordance with the relationship:

Δ

C=(C1+C3)−

(C2+C4),

where C1 and C3 are the capacitances of the first and third transducers and C2 and C4 are the capacitances of the second and fourth transducers.

13. A micromachined gyroscope, comprising:

a pair of masses disposed side-by-side in a plane, beams suspending the masses from anchors located centrally of the masses for torsional out-of-plane movement about a pair of drive axes in the plane and for torsional in-plane movement about sense axes perpendicular to the plane, means connecting the two masses together for movement of equal amplitude and opposite phase both about the drive axes and about the sense axes, with Coriolis forces produced by rotation of the masses about an input axis producing torsional movement of the masses about the sense axes, transducers positioned on opposite sides of each of the masses having input plates that extend toward each other from opposite sides of peripheral shuttle frames and stationary plates disposed within the frames and interleaved with the input plates, flexible beams constraining the shuttle frames for linear in-plane movement in directions perpendicular to the plates, and link beams interconnecting the masses and the shuttle frames so that torsional movement of the masses about the sense axes produces changes in capacitance between the input plates and the stationary plates.

14. The micromachined gyroscope of claim 13 wherein the link beams are connected to the masses on sides of the shuttle frames opposite the anchors.

15. The micromachined gyroscope of claim 13 wherein the capacitances of the transducers on opposite sides of each mass change in an anti-phase manner and the capacitances of the transducers on the same sides of the two masses change in an in-phase manner.

16. A micromachined gyroscope, comprising:

a pair of masses disposed side-by-side in a plane, beams suspending the masses from anchors located centrally of the masses for torsional out-of-plane movement about a pair of drive axes in the plane and for torsional in-plane movement about sense axes perpendicular to the plane, means connecting the two masses together for movement of equal amplitude and opposite phase both about the drive axes and about the sense axes, with Coriolis forces produced by rotation of the masses about an input axis producing torsional movement of the masses about the sense axes, transducers positioned on opposite sides of each of the masses having stationary plates extending toward each other from opposite sides of peripheral frames and input plates which are mounted on shuttles within the frames and interleaved with the stationary plates, flexible beams constraining the shuttles for linear in-plane movement in directions perpendicular to the plates, and link beams interconnecting the masses and the shuttles so that torsional movement of the masses about the sense axes produces changes in capacitance between the input plates and the stationary plates.

17. The micromachined gyroscope of claim 16 wherein the link beams are connected to the masses on the sides of transducers farthest from the anchors.

18. The micromachined gyroscope of claim 16 wherein the link beams are connected to the masses on the sides of transducers closest to the anchors.

19. The micromachined gyroscope of claim 16 wherein the capacitances of the transducers on opposite sides of each mass change in an anti-phase manner and the capacitances of the transducers on the same sides of the two masses change in an in-phase manner.