Vibratory ring structure

Abstract

A method of tuning a vibratory ring structure includes determining an angular spacing for a pair of fine tuning holes of substantially the same size, located on or near the neutral axis of the vibratory ring structure, the angular offset being selected to reduce to an acceptable level the frequency split between the target normal mode and a further normal mode which is angularly offset relative to the target normal mode, and forming the pair of fine tuning holes in the vibratory ring structure at the determined angular spacing. A ring structure, for example, a gyroscope, tuned or balanced in this manner, is also disclosed.

Claims

1. A method of tuning a vibratory ring structure comprising determining an angular spacing for a pair of fine tuning holes of substantially the same size, located on or near the neutral axis of the vibratory ring structure, an angular offset being selected to reduce to an acceptable level the frequency split between the target normal mode and a further normal mode which is angularly offset relative to the target normal mode, and forming the pair of fine tuning holes in the vibratory ring structure at the determined angular spacing, wherein the pair of fine tuning holes are placed at a substantially equal angular offset from a radial anti-node of the target normal mode.

2. The method according to claim 1, wherein the pair of fine tuning holes are formed substantially symmetrically about a radial anti-node of the target normal mode.

3. The method according to claim 1, wherein the angular offset between the fine tuning holes is less than 45 degrees.

4. The method according to claim 1, further comprising the formation of at least one coarse tuning hole.

5. The method according to claim 4, wherein the coarse tuning hole is of substantially the same size as the fine tuning holes.

6. The method according to claim 1, wherein the tuning holes are formed by laser ablation.

7. The method according to claim 1, wherein the fine tuning holes are positioned so as to achieve balancing of the cos 2 modes.

8. A vibratory ring structure comprising a ring body tuned by the formation of a pair of fine tuning holes of substantially the same size, located on or near the neutral axis of the ring body, the fine tuning holes being positioned at an angular offset relative to one another that is selected to reduce to an acceptable level the frequency split between a target normal mode and a further normal mode of the ring body, the further normal mode being angularly offset relative to the target normal mode, wherein the pair of fine tuning holes are placed at a substantially equal angular offset from a radial anti-node of the target normal mode.

9. The vibratory ring structure according to claim 8, wherein the pair of fine tuning holes are formed substantially symmetrically about a radial anti-node of the target normal mode.

10. The vibratory ring structure according to claim 8, further comprising at least one coarse tuning hole.

11. The vibratory ring structure according to claim 10, wherein the coarse tuning hole is of substantially the same size as the fine tuning holes.

12. The vibratory ring structure according to claim 8, wherein the fine tuning holes are positioned so as to achieve balancing of the cos 2 modes.

13. The vibratory ring structure according to claim 8, wherein the ring body forms part of a gyroscope.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The invention will further be described, by way of example, with reference to the accompanying drawings, in which:

(2) FIG. 1 is a diagram illustrating a ring structure to which a known balancing technique has been applied;

(3) FIG. 2 is a graph showing the variation in quadrature bias over a range of temperatures for a sample of devices;

(4) FIG. 3 illustrates the application of a balancing technique in accordance with an embodiment of the invention to the ring structure of FIG. 1;

(5) FIGS. 4a and 4b illustrate the removal of material from different locations on a ring structure; and

(6) FIG. 5 is a graph illustrating the effect of removal of material from different locations.

DETAILED DESCRIPTION

(7) An existing laser tuning or balancing process used to match or reduce the frequency split between the cos 2.theta. modes of a vibrating ring structure comprises removing or ablating material from the neutral axis of the ring, at or near a radial anti-node of the normal mode with the lower frequency. The ring structure includes four such radial anti-nodes, at angular intervals of 90 degrees. Since the orientation and natural frequencies of the primary and secondary response modes approximate the normal modes of the ring structure, the orientation and frequency of the two normal modes can be determined by exciting the ring structure using the primary and secondary drive means respectively.

(8) A pulsed laser may be used which removes a specific, fixed amount of material for each laser shot or application thereof. Using constant laser conditions is advantageous for production, as it ensures a consistent hole profile, and hence that the quanta of material removed in each shot is stable and repeatable. By way of example, the laser may be set up in such a manner that each shot changes the frequency split by approximately 0.4 Hz.

(9) It will be appreciated that material on or near the neutral axis does not contribute to the effective stiffness of either normal mode. Removing mass at a radial anti-node of the target mode will therefore reduce the effective mass, increasing the natural frequency of the target mode without substantially affecting the other mode (which has a radial node at this location). Each quanta of material removed in this way adjusts the split between the normal modes of the ring by a specific amount, and tends to improve the alignment of the primary and secondary response modes with their associated drive and pickoff means. The quantised nature of this tuning process limits the degree to which the modes can be matched to a worst case frequency split of half of the quanta by which the frequency split is adjusted. For example, if each tuning hole reduces the frequency split by approximately 0.4 Hz, the worst case frequency split after tuning will be 0.2 Hz.

(10) Referring to FIG. 1, in practise, the method used to balance a ring structure 10 employing this technique involves exciting the ring structure 10 using primary and secondary drive means (not shown) to measure the natural frequencies and orientation of the primary and secondary response modes respectively, determining the location of the radial anti-nodes 12 of the target mode, calculating the required number of laser balance holes 14, using a laser to remove mass at (or near) the radial anti-nodes of the target mode by forming the calculated number of balancing holes 14, re-measuring the response mode frequencies and orientation to verify balancing accuracy, and repeating the process if the frequency split remains above a predetermined threshold.

(11) The laser balancing process may be performed at wafer level using fully automated equipment. By way of example, the fabrication process may produce devices which have modes which are matched to within 5 Hz, and which therefore require up to twelve holes 14, each adjusting the split by 0.4 Hz, to tune or balance the normal modes.

(12) In order to achieve consistency in the laser machining process, it is important to avoid overlap of the holes 14, and they may therefore have a predetermined minimum angular separation. By way of example, the minimum angular separation between adjacent holes 14 may be 1.

(13) Since there are only four radial anti-nodes 12 of the target mode, to tune devices with a frequency split greater than 1.6 Hz, multiple tuning holes 14 must be placed near at least one of the anti-nodes 12. At least some of the holes 14 are therefore not exactly aligned with a radial anti-node of the target mode but rather are spaced therefrom by a small angle. The tuning effect of such holes 14 will be less than the predetermined tuning quanta that results from the provision of a tuning hole 14 precisely at a radial anti-node 12. This is because the effective mass of the target mode is changed less by the removal of mass at a location with a reduced modal radial displacement magnitude, and because the effective mass of the non-target mode is reduced by holes 14 which are not in alignment with the target radial anti-node 12. Unless the tuning process takes this into account, this variance may lead to an error in tuning.

(14) FIG. 2 shows the variation in quadrature bias for a sample of vibratory ring structures 10 that have been tuned using the method described hereinbefore, over a temperature range from 40 to +85 C. It can be seen that the variation in quadrature bias over this temperature range is typically approximately 20/s. In contrast, the variation in the initial quadrature bias, after tuning, is up to 80/s, which illustrates that the quadrature bias for a typical device is dominated by the precision and accuracy (or lack thereof) of the mode tuning that sets the initial quadrature bias.

(15) The need for gyroscopes of this type with improved performance drives a corresponding requirement for improvements in the tuning process. One approach would be to use a final tuning hole of variable size, to thereby achieve a tuning resolution of less than the normal tuning quanta. This would necessitate adjusting the laser power, which is impractical for a number of reasons: existing equipment may not be able to dynamically adjust laser power; laser spot size may not be adjustable in existing equipment; the laser may require time to stabilise to a given operating condition; mass removal may not vary linearly with laser power; and small adjustments to the frequency split (e.g. <0.1 Hz) may be difficult to achieve with accuracy.

(16) A process which can achieve a high accuracy of tuning using existing equipment is highly preferable.

(17) In accordance with the invention, as shown in FIG. 3, tuning holes 14, referred to hereinafter as coarse tuning holes 14, located at or near the radial anti-nodes 12 may be used as described hereinbefore to reduce the frequency split to a relatively low level and, in addition, a pair of fine tuning holes 16 are placed at predetermined angular offsets from a radial anti-node 12 of the target mode, the angular offset being selected to minimise the frequency split of the natural modes. The pair of fine tuning holes 16 are conveniently substantially equally spaced from the associated radial anti-node 12. Where both holes 16 are associated with the same radial anti-node 12, it will be appreciated that the holes 16 are conveniently substantially symmetrically arranged about that anti-node 12. However, the holes 16 may be associated with different anti-nodes 12, if desired.

(18) As mentioned above it is known that where tuning holes are not located exactly at the radial anti-node 12 positions, the tuning effect of such holes is reduced. If a pair of holes 20a, 20b are both formed at respective anti-nodes 12, and both holes have a 0.4 Hz effect on the frequency split, as shown diagrammatically in FIG. 4a, then the net effect of the holes would be a 0.8 Hz change in the frequency split. If, on the other hand, one hole 20a is formed at the anti-node 12 and a second hole 20b is formed at a position shifted from the anti-node 12 by 45, as shown diagrammatically in FIG. 4b, the frequency split change arising from the presence of the two holes will be equal and opposite, thus the holes 20a, 20b will have no net effect upon the frequency split. It will be appreciated, therefore, that the provision of a pair of fine tuning holes 16 at appropriately selected angular spacings can be used to assist in balancing of a ring structure with a good degree of accuracy. FIG. 5 shows the shift in frequency split achieved by the provision of a pair of fine tuning holes at a range of angular spacings.

(19) Referring back to FIG. 3, therefore, it will be seen that a series of coarse tuning holes 14 are formed at or near the anti-nodes 12. The coarse tuning holes 14 are used to reduce the frequency split to a value of 0.8 Hz or less. In the example shown in FIG. 3 it is assumed that the initial frequency split of the ring structure 10 is 1.65 Hz. Three coarse tuning holes 14 are provided in this example to reduce the frequency split to approximately 0.45 Hz. It will be appreciated, however, that this is merely an example and that the number of holes 14 provided will depend upon the frequency split of the ring structure prior to commencement of the balancing process. As only three coarse tuning holes 14 are required in this example, they can each be located exactly at a respective anti-node location 12. If more than four such holes 14 were required, then as with the method described hereinbefore some of the holes 14 would have to be spaced slightly from the respective anti-node location 12.

(20) Once the frequency split has been reduced to this relatively low level by the formation of the coarse tuning holes 14, a pair of fine tuning holes 16 is formed to achieve final balancing of the ring structure 10.

(21) The change in frequency split (FF.sub.split) resulting from the formation of a pair of fine tuning holes 16 with an angular separation of .sub.2 is given by:
F.sub.split=2.Math.F.sub.hole.Math.cos(2.Math..sub.2)(1)
where F.sub.hole is the nominal change in frequency split that would be achieved by the formation of one of the holes at the anti-node 12.

(22) Referring back to FIG. 3, once the three coarse tuning holes 14 have been formed the response mode frequencies and orientations are re-measured to determine the remaining frequency split. Using equation (1), the required angular separation of the pair of fine tuning holes 16 can be determined to substantially remove the frequency split, or reduce it to an acceptable level. As mentioned above, a frequency split correction of 0.45 Hz is required to achieve balancing of the ring structure. To achieve a shift in the frequency split of 0.45 Hz, the fine tuning holes 16 need to be formed at an angular separation of approximately 28, as can be seen from FIG. 5, and so the fine tuning holes are required, symmetrically about one of the anti-nodes 12, at an offset therefrom of approximately 14. Once the required angular spacing has been determined, the pair of fine tuning holes 16 are formed at the required locations to balance the ring structure 10.

(23) In order to prevent the potential for secondary effects arising from asymmetric tuning, it is desirable that the fine tuning holes 16 are symmetric about one of the anti-nodes 12 of the target mode. However, this need not necessarily always be the case, and they could be associated with different anti-nodes 12.

(24) The angular resolution with which tuning holes are placed on the ring may be limited. For example, the equipment used to form the holes may only allow the holes to be formed at 1 angles. Where such equipment is used, then it will be appreciated that exact balancing may not always be possible. However, the degree to which the ring structure 10 can be balanced will be significantly enhanced compared to the use of just the technique described hereinbefore with reference to FIG. 1. To further enhance the accuracy to which balancing is achieved, the requirement for precise symmetry of the fine tuning holes 16 about a target mode radial anti-node 12 may be relaxed, for example to allow the fine tuning hole 16 to one side of the anti-node 12 to be placed at an angle at a 1 variance to the positioning of the fine tuning hole 16 to the opposite side of the anti-node 12, for example to allow fine tuning holes may be placed at +21 and 22 respectively (or vice versa).

(25) Although a process has been described in which the final holes are the fine tuning holes, it will be appreciated that it is the net effect of the tuning holes that is important, not the order in which they are formed, and in some embodiments the fine tuning holes may be formed before the other holes. Furthermore, depending upon the initial balance of the ring structure 10, there may be no need to form any coarse tuning holes 14, and so only the pair of fine tuning holes 16 may be present.

(26) The holes described hereinbefore are not necessarily through holes, and may be relatively shallow ablation craters.

(27) Although the method has been described with reference to cos 2 vibrational modes, it will be appreciated that the method may also be applied to other ring flexural modes such as cos 3 modes. A wide range of modifications and alterations may be made to the arrangements described hereinbefore without departing from the scope of the invention.