IP Library Granted Patent US 7,017,410
Granted Patent B2
US 7,017,410 · App. 10/370,953 · Granted Mar 28, 2006

Isolated resonator gyroscope with a drive and sense plate

Assignees: The Boeing Company; California Institute of Technology
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,017,410
App. No.
10/370,953
Granted
Mar 28, 2006
Kind
B2
Abstract

The present invention discloses a resonator gyroscope comprising a vibrationally isolated resonator including a proof mass, a counterbalancing plate having an extensive planar region, and one or more flexures interconnecting the proof mass and counterbalancing plate. A baseplate is affixed to the resonator by the one or more flexures and sense and drive electrodes are affixed to the baseplate proximate to the extensive planar region of the counterbalancing plate for exciting the resonator and sensing movement of the gyroscope. The isolated resonator transfers substantially no net momentum to the baseplate when the resonator is excited.

Claims (84)

1. A resonator gyroscope, comprising:

an isolated resonator including:

a proof mass;

a counterbalancing plate having an extensive planar region; and

one or more flexures interconnecting the proof mass and counterbalancing plate;

a baseplate affixed to the resonator by the one or more flexures; and

drive and sense electrodes affixed to the baseplate proximate to the extensive planar region of the counterbalancing plate for exciting the resonator and sensing movement of the gyroscope;

wherein the isolated resonator transfers substantially no net momentum to the baseplate when the resonator is excited.

2. The resonator gyroscope comprising:

an isolated resonator including:

a proof mass;

a counterbalancing plate having an extensive planar region; and

one or more flexures interconnecting the proof mass and counterbalancing plate;

a baseplate affixed to the resonator by the one or more flexures;

a mounting frame attached to the baseplate through at least one isolation flexure: and

drive and sense electrodes affixed to the baseplate proximate to the extenstive planar region of the counterbalancing plate for exciting the resonator and sensing movement of the pyroscope:

wherein the isolated resonator transfers substantially no net momentum to the baseplate when the resonator is excited.

3. A resonator gyroscope comprising: an isolated resonator including:

a proof mass;

a counterbalancing plate having an extensive planar region; and

one or more flexures interconnecting the proof mass and counterbalancing plate, wherein each of the one or more flexures in a beam flexure attached to the proof mass at a first end and the counterbalancing plate at a second end;

a baseplate affixed to the resonator by the one or more flexures; and

drive and sense electrodes affixed to the baseplate proximate to the extensive planar region of the counterbalancing for exciting the resonator and sensing movement of the gyroscope;

wherein the isolated resonator transfers substantially no net momentum to the baseplate when the resonator is excited.

4. The resonator gyroscope comprising:

an isolated resonator including:

a proof mass, wherein the proof mass comprises a vertical protion, the vertical portion is a separate element bonded to a central plate portion, and the separate element comprises sapphire;

a counterbalancing plane having an extensive planar region: and

one or more flexures interconnecting the proof mass and counterbalancing plate;

a baseplate affixed to the resonantor by the one or more flexures; and

drive and sense electrodes affixed to the baseplate proximate to the extensive planar region of the counterbalancing plate for exciting the resonator and sensing movement of the gyroscope;

wherein the isolated resonator transfers substantially no net momentum to the baseplate when the resonator is excited.

5. The resonator gyroscope of claims 1 , 2 , 3 or 4 wherein the proof mass and counterbalancing plate each have a center mass and transverse inertia symmetry about an axis are substantially coincident and the proof mass and counterbalancing plate together form two differential rocking modes of vibrations transverse to the axis with substantially equal frequencies.

6. The resonator gyroscope of claims 1 , 2 , 3 or 4 , wherein the baseplate is rigid.

7. The resonator gyroscope of claims 1 , 2 , 3 or 4 , wherein the baseplate is flexible.

8. The resonator gyroscope of claims 1 , 2 , 3 or 4 , wherein the counterbalancing plate has a rocking inertia substantially compatable to that of the proof mass.

9. The resonator gyroscope of claims 1 , 2 , 3 or 4 , wherein the one or more flexures are integral to the counterbalancing plate.

10. The resonator gyroscope of claims 1 , 2 , 3 or 4 , wherein the proof mass, counterbalancing plate and baseplate are machined from silicon.

11. The resonator gyroscope of claim 3 , wherein each beam flexure is attached to the baseplate off center and nearer to the proof mass than an attachment point to the counterbalancing plate.

12. The resonator gyroscope of claim 4 , wherein the one or more flexure are integral to the central plate portion.

13. The resonator gyroscope of claim 4 , wherein the central plate portion, one or more flexures and the counterbalancing plate are produced by through- etching a precision-polished silicon wafer.

14. A method of producing a resonator gyroscope, comprising the steps of:

providing an isolated resonatory including:

a proof mass;

a counterbalancing plate having an extensive planar region: and

one or more flexures interconnecting the proof mass and counterbalancing plate;

affixing drive and sense electrodes to the baseplate: and

affixing the resonator to a baseplate by the one or more flexures such that the drive and sense electrodes are disposed proximate to the extensive planar region of the counterbalancing plate, wherein the sense electrodes are disposed around the periphery of the counterbalancing plate:

wherein the isolated resonatory transfers substantially no net momentum to the baseplate when the resonatory is excited.

15. A method of producing a resonator gyroscope, comprising the steps of:

providing an isolated resonatory including:

a proof mass;

a counterbalancing plate having an extensive planar region; and

one or more flexures interconnecting the proof mass and counterbalancing plate;

affixing drive and sense electrodes to the baseplate;

affixing the resonator to a baseplate by the oe oe more flexures such that the drive and sense electrodes are disposed proximate to the extensive planar region of the counterbalancing plate;

and

providing a mounting frame attached to the baseplate through at least one isolation flexure;

wherein the isolated resonator transfers substantially no net momentum to the baseplate when the resonator is excited. separate element bonded to the central plate portion.

16. A method of producing a resonator gyroscope, comprising the steps of:

providing an isolated resonator including:

a proof mass;

a counterbalancing plate having an extensive planar region: and

one or more flexures interconnecting the proof mass and counterbalancing plate, wherein each of the one or more flexures is a beam flexure attached to the proof mass at a first end and the counterbalancing at a second end;

affixing drive and sense electrodes to the baseplate: and

affixing the resonator to a baseplate by the one or more flexures such that the drive and sense electrodes are disposed proximate to the extensive planar region of the counterbalancing plate;

wherein the isolated resonator transfers substantially no net momentum to the baseplate when the resonator is excited.

17. A method of producing a resonator gyroscope, comprising the steps of:

providing an isolated resonator including:

a proof mass,

wherein the proof mass comprises a vertical portion, the vertical portion is a separate element bonded to a central plate portion, and the separate element comprises sapphire;

a counterbalancing plate having an extensive planar region; and

one or more flexures interconnecting the proof mass and counterbalancing plate; affixing drive and sense electrodes to the baseplate; and

affixing the resonator to a baseplate by the o ne or more flexures such that the drive and sense electrodes are disposed proximate to the extensive planar region of the counterbalancing plate;

wherein the isolated resonator transfers substantially no net momentum to the baseplate when the resonator is excited.

18. The method of claims 14 , 15 , 16 and 17 wherein the proof mass and counterbalancing plate have a center of mass and transverse inertia symmetry about an axis that are substantially coincident and the proof and the counterbalancing plate together from two differential rocking modes of vibration transverse to the axis with substantially equal frequencies.

19. The method of claim 14 , 15 , 16 and 17 , wherein the baseplate is rigid.

20. The method of claim 14 , 15 , 16 and 17 , wherein the baseplate is flexible.

21. The method of claim 14 , 15 , 16 and 17 , wherein the counterbalancing plate has a rocking inertia substantially compatible to that of the proof mass.

22. The method of claim 14 , 15 , 16 and 17 , wherein the one or more flexures are produced integral to the counterbalancing plate.

23. The method of claim 14 , 15 , 16 and 17 , wherein the steps of producing and affixing comprise machining the proof mass, counterbalancing plate and baseplate from silicon.

24. The method of claim 16 , wherein each beam flexure is attached to the baseplate off center and nearer to the proof than an attachment point to the counterbalancing plate.

25. The method of claim 17 , wherein the one or more flexure are integral to the central plate portion.

26. The method of claim 17 , wherein the central plate portion one or more flexure and the counterbalancing plate are produced by through etching a precision-polished silicon wafer.

Assignments (3)
CONFIRMATORY LICENSE Recorded Apr 29, 2003
From: CALIFORNIA INSTITUTE OF TECHNOLOGY
To: NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
Reel/Frame 014035/0759 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 20, 2003
From: CHALLONER, A. DORIAN
To: BOEING COMPANY, THE
Reel/Frame 013808/0401 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 20, 2003
From: SHCHEGLOV, KIRILL V.
To: CALIFORNIA INSTITUTE OF TECHNOLOGY
Reel/Frame 013810/0235 →
Continuity (2)
Continuation In Part 0992827900 · Aug 10, 2001
Related Publication 20030150267A1 · Aug 14, 2003