Vibrational gyroscope

• US 4,644,793 A
• Filed: 08/29/1985
• Issued: 02/24/1987
• Est. Priority Date: 09/07/1984
• Status: Expired due to Fees

• Current Assignee: Gec-Marconi Limited The Grove Warren Lane Stanmore Middlesex HA7 4LY England
• Original Assignee: Marconi Co Ltd (BAE Systems Plc)
• Inventors: Church, Peter D.
• Primary Examiner(s): Kreitman, Stephen A.
• Assistant Examiner(s): Oldham, Scott M.
• Application Number:
  US06/770,831
• Time in Patent Office: 544 Days
• Field of Search: 73/505, 310/321, 310/324
• US Class Current: 73/504.13
• CPC Class Codes: G01C 19/5691 of essentially three-dimensional vibrators, e.g. wine glass-type vibrators

Abstract

A vibrational gyroscope is provided with a vibrating member in the form of a flexible annular shell extending from a flat flexible plate. In use, the flat plate is vibrated and excites radial vibrations in the lip of the annular shell. When the gyroscope is rotated about the shell axis, the nodes of these radial vibrations shift around the circumference of the lip, due to the action of Coriolis forces. The radial nodes of the vibrations in the plate shift similarly and their movement is detected by sensing means on the plate, giving an indication of the rotation rate.

Claims

1. A vibrational gyroscope comprising a flat flexible plate, a flexible annular shell extending from said plate, driving means for causing said plate to vibrate in such a way as to excite radial vibration in said annular shell and sensing means for sensing changes in the vibration of said plate in response to changes in said radial vibrations induced by rotation about the shell axis.

2. A vibrational gyroscope as claimed in claim 1 wherein said annular shell is substantially cylindrical.

3. A vibrational gyroscope as claimed in claim 1 wherein said annular shell is substantially right cylindrical.

4. A vibrational gyroscope as claimed in claim 1 wherein said plate extends outside said annular shell.

5. A vibrational gyroscope as claimed in claim 1 wherein said plate is annular.

6. A vibrational gyroscope as claimed in claim 5 wherein said plate is supported by a mounting at a nodal point or line of a free vibration.

7. A vibrational gyroscope as claimed in claim 1 wherein said plate is supported by a mounting at its edge.

8. A vibrational gyroscope as claimed in claim 1 wherein said plate extends inside said shell.

9. A vibrational gyroscope as claimed in claim 1 wherein said plate is a disc.

10. A vibrational gyroscope as claimed in claim 1 wherein said annular shell extends from both sides of said plate.

11. A vibrational gyroscope as claimed in claim 1 wherein said driving means and said sensing means comprise respective sets of electrodes on a common body of piezoelectric material, said body being attached to said plate.

12. A vibrational gyroscope as claimed in claim 11 wherein said electrodes are provided with connection tabs located at a nodal region of said plate.

13. A vibrational gyroscope as claimed in claim 12 wherein said body of piezoelectric material is provided with damping electrodes for applying a damping signal to said shell via said plate for controlling the Q-factor of said radial vibrations.

14. A vibrational gyroscope as claimed in claim 13 wherein said body is composed of zinc oxide epitaxially deposited on said plate.

15. A vibrational gyroscope as claimed in claim 13 wherein said body is composed of lead zirconate titanate (P.Z.T.) bonded to said plate.

16. A vibrational gyroscope as claimed in claim 13 wherein said body is composed of lithium niobate.

17. A vibrational cyroscope as claimed in claim 11 wherein no part of said shell projects beyond that surface of said plate on which said body of piezoelectric material is mounted.

18. A vibrational gyroscope as claimed in claim 17 and further comprising an integrated circuit, said vibrational gyroscope being mounted on said integrated circuit and said integrated circuit incorporating driving and sensing circuitry associated with said driving and sensing electrodes.

19. A vibrational gyroscope as claimed in claim 18 wherein said integrated circuit is provided with input power terminals and one or more output terminals at which a signal is generated representative of rotation of the gyroscope.

20. A vibrational gyroscope as claimed in claim 19 wherein said integrated circuit is provided with one or more input terminals for controlling the sensitivity of the gyroscope.