Frame assembly and dither drive for a coriolis rate sensor

• US 4,782,700 A
• Filed: 07/17/1987
• Issued: 11/08/1988
• Est. Priority Date: 07/17/1987
• Status: Expired due to Fees

• Current Assignee: Alliedsignal Inc.
• Original Assignee: Sundstrand Data Control, Inc.
• Inventors: Hulsing, Rand H.
• Primary Examiner(s): Tokar, Michael J.
• Assistant Examiner(s): Bell, Robert P.
• Application Number:
  US07/075,039
• Time in Patent Office: 480 Days
• Field of Search: 73/517 AV, 73/505, 73/510, 73/514, 73/517 R
• 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. The accelerometer support surfaces are connected to opposite ends of a flex member (52), which includes six flexures (32, 34, 36, 38, 40, 42) having parallel bending axes. Two of the flexures (34, 38) are disposed at opposite ends of one side of each flexure member, and have a "long" axis that is substantially parallel to the sensitive axes of the accelerometers and aligned with a line connecting their centers of percussion. The centers of mass of the accelerometers and their associated supporting surfaces are coincident with the centers of percussion, and are rigidly connected by the two flexures and by one side (30) of each flex member. This solid metal path between the centers of percussion minimizes common mode errors. A driving mechanism (64) is connected to the parallelogram frame and is opertive 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 frame for use in a Coriolis rate sensor including two accelerometers each having a preferred axis, comprising:

two accelerometer carriers disposed on opposite sides of the frame and adapted for mounting the two accelerometers with their preferred axes in alignment;

two substantially parallel flex members, each extending between the two accelerometer carriers at opposite sides thereof, the flex members each including a cross brace disposed at their center, adapted for attaching the frame to a supporting structure, and further including a plurality of flexures having parallel bending axes, the flexures being disposed at the corners of a parallelogram, with one of the flexures connecting two sides of the parallelogram at each corner and one of the flexures disposed at each end of the cross brace and connecting the centers of two sides of the parallelogram, the flexures at each end of one of said two sides of each flex member being oriented to provide maximum stiffness on a line between the two carriers and disposed so that when the two accelerometers are mounted on the carriers, the centers of mass of each carrier and the accelerometer mounted thereon are aligned with the flexures at each end of said one side.

2. The frame of claim 1 wherein for each flex member, the moment of said one side of the flex member about the bending axis of the flexure connecting the cross brace to said one side equals the moment of the other of said two sides of the flex member about the bending axis of the flexure connecting the cross brace to said other side, thereby preventing a rotational torque being applied to the frame as a result of a vibrational component directed parallel to the preferred axes of the accelerometers.

3. The frame of claim 1 further comprising a base plate disposed in the center of the frame and connected to a center portion of each of the cross braces, one end of the base plate being adapted to attach to the supporting structure.

4. The frame of claim 3 wherein the center of the base plate defines a central plane through the frame that is intermediate both carriers, and wherein the frame is substantially symmetrical in both shape and mass about said plane, preventing a rotational torque from being applied to the frame as a result of a vibrational component directed transversely to the preferred axes and parallel to the bending axes of the flexures.

5. The frame of claim 3 further comprising at least one tuning strap connecting the accelerometer carriers to the base plate, and selected to have a stiffness balancing a cross axis compliance associated with the flexures.

6. The frame of claim 1 wherein the frame is substantially symmetrical in both shape and mass about a plane that is equidistant from and intermediate the flex member, providing a dynamic balance.

7. The frame of claim 1 further comprising means adapted for magnetically and mechanically coupling the flex members to a driving mechanism operative to vibrate the accelerometers back and forth.

8. A frame for use in a Coriolis rate sensor having two accelerometers mounted with their preferred axes in alignment, comprising:

(a) two accelerometer mounting pads disposed on opposite sides of the frame, each being adapted to mount one of the accelerometers so that their preferred axes are aligned;

(b) parallelogram means for linking the accelerometer mounting pads in parallel alignment and including a plurality of flexures enabling the accelerometer mounting pads and accelerometers mounted thereon to vibrate back and forth in a direction transverse to their preferred axes;

(c) attachment means for attaching a central portion of the frame to a supporting structure, the attachment means being pivotably connected to the parallelogram means by the plurality of flexures; and

(d) common mode connection means for rigidly connecting the two accelerometer mounting pads along a path that is aligned with a line extending through a center of percussion associated with each accelerometer, the common mode connection means comprising a portion of the parallelogram means and including a plurality of flexures oriented in alignment with said path and differently than other of the flexures of the parallelogram means, the orientation insuring that both accelerometers are subjected to the same motion directed along their preferred axes.

9. The frame of claim 8 wherein the center of percussion associated with each accelerometer is coincident with a center of gravity associated with each mounting pad and accelerometer, and wherein the centers of gravity of the accelerometers are rigidly connected by the common mode connection means along said path.

10. The frame of claim 8 wherein the attachment means comprise a base plate connected to the supporting structure at one end and to a central portion of the parallelogram means adjacent the other end.

11. The frame of claim 8 wherein the frame is symmetrical both in shape and mass about two orthogonal planes extending through the center of the frame, one of which is aligned with the preferred axes of the accelerometers.

12. The frame of claim 11 wherein the parallelogram means are dynamically balanced.

13. The frame of claim 8 further comprising means for compensating a cross axis compliance associated with the flexures to eliminate an error signal resulting from a non-common mode rotational tilting of the accelerometers that would otherwise be produced when the accelerometers vibrate back and forth.

14. A frame for use in a Coriolis rate sensor including two accelerometers each having a preferred axis, comprising:

two accelerometer carriers disposed on opposite sides of the frame and adapted for mounting the two accelerometers with their preferred axes in alignment;

two substantially parallel flex members, each extending between the two accelerometer carriers at opposite sides thereof, the flex members each including a cross brace disposed at their center, adapted for attaching the frame to a supporting structure, and a plurality of flexures having parallel bending axes, the flexures being disposed so as to define a parallelogram, by connecting the sides of the parallelogram at each of the corners of the parallelogram and connecting the cross brace to the centers of two of the sides of the parallelogram that extend transversely between the accelerometer carriers, one of said two sides of the parallelogram including flexures at each end that are oriented to provide maximum stiffness on a line between the two carriers and disposed so that when the two accelerometers are mounted on the carriers, the centers of mass of each carrier and the accelerometer mounted thereon, and a center of percussion associated with each accelerometer, are aligned with the flexures at each end of said one side.