Piezoelectric vibratory rate sensor

• US 5,056,366 A
• Filed: 12/26/1989
• Issued: 10/15/1991
• Est. Priority Date: 12/26/1989
• Status: Expired due to Term

• Current Assignee: Litton Systems Incorporated (Northrop Grumman Corporation)
• Original Assignee: Litton Systems Incorporated (Northrop Grumman Corporation)
• Inventors: Wyse, Stanley F., Fersht, Samuel N.
• Primary Examiner(s): CHAPMAN JR, JOHN E
• Application Number:
  US07/456,532
• Time in Patent Office: 658 Days
• Field of Search: 73/505, 73/517 B, 310/329
• US Class Current: 73/504.15
• CPC Class Codes: G01C 19/5607 using vibrating tuning forks double-ended tuning forks using planar vibrating masses suspended at opposite ends G01C19/5719

Abstract

A vibrating rotation rate sensor of the type that includes a generally-planar, H-shaped frame of piezoelectric material such as quartz. A first set of drive electrodes is fixed to a pair of upper tines and a second set of pickoff electrodes is fixed to a pair of lower tines. An array of control electrodes is fixed to the upper tine pair adjacent the cross-piece of the H-shaped frame. The control electrodes permit the application of control signals for nulling Coriolis-induced out-of-plane vibration of the upper tines allowing use of a resonant frame.

Claims

1. In a rotation rate sensor of the type that includes a generally planar and H-shaped sensor frame of piezoelectric material, said frame including an upper pair of tines and a lower pair of tines, said tines being joined to an intermediate cross-piece and further including a first array of drive electrodes fixed to said upper tines for transmitting electrical signals for driving said upper tines in-plane and a second array of pickoff electrodes fixed to said lower tines for transmitting electrical signals generated in said lower tines in response to Coriolis-induced out-of-plane bending thereof, the improvement comprising:

a) a third array of control electrodes for transmitting electrical signals for counteracting Coriolis-induced out-of-plane bending of said upper tines; and

b) said control electrodes are fixed to said upper tines adjacent said cross-piece.

2. A rotation rate sensor as defined in claim 1 further including:

a) a fourth array of scale factor electrodes, said electrodes being arranged to detect inplane bending; and

b) said array of scale factor electrodes is fixed to said upper tines.

3. A rotation rate sensor as defined in claim 2 fabricated of α

quartz.

4. A rotation rate sensor as defined in claim 3 wherein said generally planar sensor frame is a z-cut crystal.

5. A rotation rate sensor as defined in claim 4, including generally-planar pairs of pickoff electrodes located in the yz-plane and fixed to opposite sides of said lower tines.

6. A rotation rate sensor as defined in claim 5 wherein the top of each of said pickoff electrodes is adjacent said cross-piece.

7. A rotation rate sensor as defined in claim 6 wherein each of said pickoff sensors extends substantially the length of a lower tine.

8. A rotation rate sensor as defined in claim 7 further including:

a) an electrical circuit in communication with said pickoff electrodes; and

b) said circuit is arranged to provide an electrical current responsive to out-of-plane bending of said lower tines.

9. A rotation rate sensor as defined in claim 4 including generally-planar pairs of control electrodes located in the yz-plane and fixed to opposite sides of said upper tines.

10. A rotation rate sensor as defined in claim 9 wherein the bottom of each of said control electrodes is adjacent said cross-piece.

11. A rotation rate sensor as defined in claim 10 further including:

a) an electrical circuit in communication with said control electrodes; and

b) said circuit is arranged to accept a voltage signal for counteracting out-of-plane vibration of said upper tines.

12. A rotation rate sensor as defined in claim 4 including generally-planar pairs of scale factor electrodes located in the xy-plane and fixed to opposed faces of said upper tines.

13. A rotation sensor as defined in claim 12 wherein each of said pairs of scale factor electrodes includes a lower electrode and an upper electrode, each lower and upper electrode being fixed to a surface of an upper tine and separated by the drive electrode fixed to said surface of said tine.

14. A rotation sensor as defined in claim 13 wherein each lower scale factor electrode is located adjacent said cross-piece.

15. A rotation rate sensor as defined in claim 3 wherein said generally-planar sensor frame is an x-cut crystal.

16. A rotation rate sensor as defined in claim 15 including generally-planar pickoff electrodes located in the xy-plane and fixed to the inner sides of said lower tines.

17. A rotation rate sensor as defined in claim 16 wherein the top of each of said pickoff electrodes is adjacent said cross-pieces.

18. A rotation rate sensor as defined in claim 17 further characterized in that:

a) each of said lower tines includes a narrowed central portion;

b) said narrowed central portion is oriented in the xy-plane; and

c) said pickoff electrodes are located within said narrowed portions of said lower tines.

19. A rotation rate sensor as defined in claim 18 further including:

a) an electrical circuit in communication with said pickoff electrodes; and

b) said circuit is arranged to provide a voltage signal responsive to out-of-plane vibration of said lower tines.

20. A rotation rate sensor as defined in claim 15 including generally-planar control electrodes located on all surfaces of said upper tines.

21. A rotation rate sensor as defined in claim 20 further including:

a) an electrical circuit; and

b) said circuit is arranged to accept a voltage signal for nulling vibration of said upper tines.

22. A sensor comprising:

a) a generally planar and H-shaped sensor frame of piezoelectric material, said frame including an upper pair of tines and a lower pair of tines joined to an intermediate cross-piece;

b) at least one pickoff electrode fixed to said lower tines, said at least one electrode being arranged to transmit electrical signals generated within said frame of piezoelectric material in response to an inertial input;

c) at least one control electrode fixed to said frame, said at least one electrode being arranged to transmit electrical signals to said frame of piezoelectric material for counteracting the effect of said inertial input upon said frame; and

d) a feedback control circuit for accepting said signal from said at least one pickoff electrode and for generating and providing said counteracting signal to said at least one control electrode.