Dual axis rate sensor

• US 7,461,552 B2
• Filed: 10/23/2006
• Issued: 12/09/2008
• Est. Priority Date: 10/23/2006
• Status: Active Grant

• Current Assignee: Emcore Corporation
• Original Assignee: Custom Sensors & Technologies Incorporated (Schneider Electric SE)
• Inventors: Acar, Cenk
• Primary Examiner(s): Kwok; Helen C.
• Application Number:
  US11/552,006
• Publication Number:
  US 20080092652A1
• Time in Patent Office: 778 Days
• Field of Search: 735/040.2, 735/040.4, 735/041.2, 735/041.4, 735/040.8, 735/040.9, 735/10, 735/11
• US Class Current: 73/504.04
• CPC Class Codes: G01C 19/5712 the devices involving a micromechanical structure
• CPC Class Codes: G01P 15/125 by capacitive pick-up
• CPC Class Codes: G01P 15/18 in two or more dimensions
• CPC Class Codes: G01P 2015/084 the mass being suspended at more than one of its sides, e.g. membrane-type suspension, so as to permit multi-axis movement of the mass

Abstract

Angular rate sensor for detecting rotation about first and second mutually perpendicular axes which has first and second masses coupled together for torsional drive mode oscillation of equal amplitude and opposite phase about third axes which are perpendicular to the first and second axes. The first mass is mounted for oscillation about the second axis in response to Coriolis forces produced by rotation about the first axis, and the second mass is mounted for oscillation about the first axis in response to Coriolis forces produced by rotation about the second axis. In some disclosed embodiments, the rate sensor also includes a pair of accelerometer masses which are connected together for torsional movement of equal amplitude and opposite phase about axes parallel to the third axes in response to acceleration along the second axis and for torsional movement of equal amplitude and opposite phase about axes parallel to the second axis in response to acceleration along the third axes.

Claims

1. A rate sensor for detecting rotation about first and second mutually perpendicular axes, comprising first and second masses coupled together for torsional drive mode oscillation of equal amplitude and opposite phase about third axes which are perpendicular to the first and second axes, the first mass being mounted for oscillation about the second axis in response to Coriolis forces produced by rotation about the first axis, and the second mass being mounted for oscillation about the first axis in response to Coriolis forces produced by rotation about the second axis.

2. The rate sensor of claim 1 wherein the masses are generally planar and disposed side-by-side, with the first and second axes lying in a plane with the masses and the third axes being perpendicular to the plane.

3. The rate sensor of claim 1 wherein the masses are mounted in gimbals for torsional movement independently of each other about the first and second axes, and the gimbals are constrained for torsional movement of equal amplitude and opposite phase about the third axes.

4. The rate sensor of claim 3 including electrodes for driving the gimbals to oscillate torsionally about the third axes.

5. The rate sensor of claim 1 together with a pair of accelerometer masses which are connected together for torsional movement of equal amplitude and opposite phase about axes parallel to the third axes in response to acceleration along the second axis and for torsional movement of equal amplitude and opposite phase about axes parallel to the second axis in response to acceleration along the third axes.

6. A rate sensor for detecting rotation about first and second mutually perpendicular axes, comprising a generally planar substrate, first and second gimbals mounted on the substrate and constrained for in-plane torsional drive mode oscillation of equal amplitude and opposite phase about drive axes which are perpendicular to the first and second axes, first and second generally planar masses, torsionally flexible beams mounting the first mass in the first gimbal and constraining the first mass for in-plane drive mode oscillation with the first gimbal and for out-of-plane rotation about the first axis in response to Coriolis forces produced by rotation about the second axis, and torsionally flexible beams mounting the second mass in the second gimbal and constraining the second mass for in-plane drive mode oscillation with the second gimbal and for out-of-plane rotation about the second axis in response to Coriolis forces produced by rotation about the first axis.

7. The rate sensor of claim 6 wherein the gimbals are mounted on the substrate by beams which extend between the gimbals and anchors on the substrate and are flexible only in the plane of the gimbals.

8. The rate sensor of claim 7 wherein the anchors are positioned toward the centers of the masses.

9. The rate sensor of claim 6 including capacitor plates mounted on the substrate beneath the masses for monitoring the out-of-plane rotation of the masses about the first and second axes.

10. The rate sensor of claim 6 including a cap wafer bonded to the substrate, with the gimbals, the masses and the beams being hermetically sealed in a cavity in the cap wafer.

11. The rate sensor of claim 10 including electrical conductors passing through the substrate.

12. The rate sensor of claim 11 including bonding pads connected electrically to the conductors on the side of the substrate opposite the masses.

13. The rate sensor of claim 11 including balls of solder connected electrically to the conductors on the side of the substrate opposite the masses.

14. The rate sensor of claim 6 including a pair of generally planar accelerometer masses mounted on the substrate beside the first and second masses and connected together for in-plane rotation of equal amplitude and opposite phase about axes parallel to the drive axes in response to acceleration along the second axis and for out-of-plane rotation of equal amplitude and opposite phase about pivot axes parallel to the second axis in response to acceleration along the drive axes.

15. The rate sensor of claim 14 wherein the accelerometer masses are mounted on frames by torsionally flexible beams which extend along the pivot axes and constrain the accelerometer masses for in-plane rotation with the frames and for out-of-plane rotation relative to the frames, and the frames are mounted on the substrate by beams which constrain the frames for in-plane rotation.

16. The rate sensor of claim 14 wherein the accelerometer masses are formed in two sections with unequal moments of inertia about the pivot axes.

17. The rate sensor of claim 16 wherein the accelerometer masses are symmetrical in shape about the pivot axes but the two sections of each of the accelerometer masses have different masses.

18. The rate sensor of claim 14 including electrode plates on the substrate beneath the accelerometer masses for monitoring the out-of-plane rotation of the accelerometer masses, and slots opening through at least one surface of one of the sections of each of the accelerometer masses.

19. The rate sensor of claim 18 wherein portions of the accelerometer masses which are symmetrical in shape relative to the pivot axes overlap with the electrode plates to form capacitors for monitoring the out-of-plane movement of the accelerometer masses.

20. A device for monitoring rate of rotation about mutually perpendicular first and second axes which lie in a plane and acceleration along a third axis perpendicular to the plane and along an axis in the plane, comprising:

a substrate, first and second generally planar masses mounted side-by-side on the substrate and coupled together for in-plane torsional drive mode oscillation of equal amplitude and opposite phase about drive axes which are perpendicular to the plane, the first mass being mounted for out-of-plane rotational movement about the second axis in response to Coriolis forces produced by rotation about the first axis, and the second mass being mounted for out-of-plane torsional movement about the first axis in response to Coriolis forces produced by rotation about the second axis, a pair of accelerometer masses mounted on the substrate beside the first and second masses and connected together for in-plane rotation of equal amplitude and opposite phase about axes perpendicular to the plane in response to acceleration along an axis in the plane and for out-of-plane rotation of equal amplitude and opposite phase about pivot axes in the plane in response to acceleration along the third axis.

21. The rate sensor of claim 20 wherein the accelerometer masses are mounted for in-plane rotation about the axes perpendicular to the plane in response to acceleration along any one of the mutually perpendicular axes.

22. The rate sensor of claim 20 wherein the pivot axes are parallel to one of the mutually perpendicular axes.

23. The rate sensor of claim 20 wherein the first and second masses are mounted in gimbals for out-of-plane rotation independently of each other about the mutually perpendicular axes, and the gimbals are constrained for in-plane oscillation of equal amplitude and opposite phase about the drive axes.

24. The rate sensor of claim 20 wherein the accelerometer masses are mounted on frames by torsionally flexible beams which extend along the pivot axes and constrain the accelerometer masses for in-plane rotation with the frames and for out-of-plane rotation relative to the frames, and the frames are mounted on the substrate by beams which constrain the frames for in-plane rotation.

25. A device for monitoring acceleration along a first axis which lies in a plane and a second axis which is perpendicular to the plane, comprising:

a substrate, a pair of generally planar masses which are disposed in the plane, means mounting the masses on the substrate for in-plane torsional movement of equal amplitude and opposite phase about the second axis in response to acceleration along the first axis and for out-of-plane torsional movement of equal amplitude and opposite phase about pivot axes which lie in the plane in response to acceleration along the second axis.

26. The rate sensor of claim 25 wherein the masses are mounted on frames by torsionally flexible beams which extend along the pivot axes and constrain the masses for in-plane torsional movement with the frames and for out-of-plane torsional movement relative to the frames, and the frames are mounted on the substrate by beams which constrain the frames for in-plane torsional movement about the second axis.

27. The rate sensor of claim 25 wherein the masses are formed in two sections with unequal moments of inertia about the pivot axes.

28. The rate sensor of claim 27 wherein the masses are symmetrical in shape about the pivot axes but the two sections of each of the masses have different masses.

29. The rate sensor of claim 25 including electrode plates on the substrate beneath the masses for monitoring the out-of-plane movement of the masses, and slots opening through at least one surface of one of the sections of each of the masses.

30. The rate sensor of claim 29 wherein portions of the masses which are symmetrical in shape relative to the pivot axes overlap with the electrode plates to form capacitors for monitoring the out-of-plane movement of the masses.