Frame assembly and dither drive for a coriolis rate sensor

• US 4,864,861 A
• Filed: 07/26/1988
• Issued: 09/12/1989
• Est. Priority Date: 07/17/1987
• Status: Expired due to Fees

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Sundstrand Data Control, Inc. (Rtx Corporation)
• Inventors: Hulsing, Rand H.
• Primary Examiner(s): Tokar, Michael J.
• Assistant Examiner(s): NOT, DEFINED
• Application Number:
  US07/224,566
• Time in Patent Office: 413 Days
• Field of Search: 73/517 R, 73/517 AV, 73/505
• US Class Current: 73/504.12
• CPC Class Codes: G01C 19/5769 Manufacturing; Mounting; Housings
• CPC Class Codes: G01C 19/5783 Mountings or housings not specific to any of the devices covered by groups G01C19/5607 - G01C19/5719
• CPC Class Codes: G01P 15/08 with conversion into electric or magnetic values
• CPC Class Codes: G01P 3/46 by measuring amplitude of generated current or voltage in general G01R19/00

Abstract

An apparatus for producing signals indicative of both a Coriolis rate and an acceleration along a preferred axis while decoupling extraneous vibration and motion that would introduce errors into the signals, and a driving mechanism for vibrating the apparatus at a dither frequency. The apparatus includes a parallelogram frame (50) including two accelerometer support surfaces (24, 26) on which are mounted two accelerometers (20 and 22) having their sensitive axes in parallel alignment. A driving mechanism (64) is connected to the parallelogram frame and is operative to drive the accelerometers at a desired frequency, causing them to vibrate back and forth in a direction substantially transverse to their sensitive axes. The driving mechanism includes a mounting plate (72) and a coil frame (66) on which are mounted two electromagnetic coils (70) having a "C" shaped core (80). The driving mechanism is mounted so that the core faces a pole piece (84) attached to the parallelogram frame and its moment of inertia is trimmed to equal that of the parallelogram frame. It is connected to the parallelogram by a link (88) and provides a reactionless driving force.

Claims

1. A drive mechanism for a Coriolis rate sensor comprising:

(a) a support plate including means for attaching the support plate to a supporting structure in a position adjacent the Coriolis rate sensor;

(b) a coil frame in which is mounted an electromagnetic coil, the coil frame being connected to the support plate along a flexure, the flexure having a bending axis about which the coil frame may pivot; and

(c) a core face on the electromagnetic coil being disposed proximate to and facing toward a corresponding pole face that is mounted on the Coriolis rate sensor.

2. The drive mechanism of claim 1 wherein the electromagnetic coil includes a "C" shaped core, both ends of the core being disposed proximate and facing the corresponding pole face.

3. The drive mechanism of claim 1 wherein the total inertia of the drive mechanism is made equal to the total inertia of the Coriolis rate sensor by adjusting the mass of the coil frame, thereby providing a reactionless assembly.

4. The drive mechanism of claim 1 wherein the center of gravity of the coil frame is aligned with the bending axis of the flexure.

5. The drive mechanism of claim 1 further comprising a solid link extending between the coil frame and the Coriolis rate sensor.

6. The drive mechanism of claim 1 wherein the core faces and their corresponding pole face are beveled at an acute angle relative to each other, to maintain a constant force center as the core faces and pole face are attracted toward each other.

7. The drive mechanism of claim 1 wherein two electro-magnetic coils are mounted in the coil frame, with the flexure disposed between the two electromagnetic coils, and where the electromagnetic coils are adapted to be alternately energized by a power supply.

8. A driver for a Coriolis rate sensor comprising:

(a) a frame including a fixed part adapted to mount on a supporting structure at one side of the Coriolis rate sensor, said frame further including a flexible joint permitting a movable part of the frame to pivot about a bending axis relative to the fixed part of the frame;

(b) an electromagnetic coil mounted on the movable part of the frame, including a core in close proximity to the Coriolis rate sensor; and

,

(c) a pole piece mounted on one side of the Coriolis rate sensor, juxtaposed opposite the core, said electromagnetic coil providing an attractive force that causes the movable part of the frame with the electromagnetic coil mounted on it and said one side of the Coriolis rate sensor to rock toward each other.

9. The driver of claim 8, wherein the core is "C" shaped, both ends of the core being disposed proximate the pole piece.

10. The driver of claim 9, wherein the pole piece comprises a bar that has a substantially planar pole face extending in length from at least one end of the core to the other.

11. The driver of claim 10, wherein the ends of the core and the opposite pole face are beveled at an acute angle, so that a constant force center is maintained between the two as the core and pole piece rock toward each other.

12. The driver a claim 8, wherein the total inertia of the frame and the electromagnetic coil is equal to the total inertia of the Coriolis rate sensor and the pole piece, so that together, the driver and the Corioliss rate sensor comprise a reactionless assembly with respect to the force provided by the electromagnet.

13. The driver of claim 8, wherein the center of gravity of the frame is aligned with the bending axis of the flexible joint.

14. The driver of claim 8, further comprising a solid link extending between the frame and the Coriolis rate sensor.

15. The driver of claim 8, further comprising another electromagnetic coil mounted on the movable part of the frame, and another pole piece mounted on the Coriolis rate sensor opposite thereto, the flexible joint being disposed intermediate the electromagnetic coils, said electromagnetic coils being alternately energized in time to effect a back and forth rocking motion of opposite ends of the Coriolis rate sensor.

16. A drive mechanism for causing a Coriolis rate sensor to rock back and forth, comprising:

(a) means for mounting the drive mechanism to a supporting structure adjacent the Coriolis rate sensor;

(b) electromagnetic means for providing a magnetic force; and

(c) pivot means, for pivotally connecting the electromagnetic means to the means for mounting, enabling the electromagnetic means to move relative to the supporting structure, rocking toward and away from the Corioliss rate sensor in response to the magnetic force.

17. The drive mechanism of claim 16, wherein the center of gravity of the drive mechanism is aligned with a bending axis of the pivot means.

18. The drive mechanism of claim 16, further comprising a pole piece mounted on the Coriolis rate sensor, wherein the electromagnetic means include a core face, both the core face and pole piece being beveled to maintain a constant force center between the core face and the pole piece as the electromagnetic means rock toward the Coriolis rate sensor.

19. The drive mechanism of claim 16, further comprising a solid link interconnecting the electromagnetic means and the Coriolis rate sensor.

20. The drive mechanism of claim 16, wherein the electromagnetic means comprise two electromagnets, each having a "C" shaped core oriented with core faces disposed at the ends of the core juxtaposed opposite a facing surface of a pole piece attached proximate opposite ends of the Coriolis rate sensor.

21. The drive mechanism of claim 20, wherein the electromagnets are alternately energized to rock first one end of the Coriolis rate sensor toward one of the electromagnets, and then the opposite end toward the other electromagnet.