RING GYROSCOPE STRUCTURE AND GYROSCOPE

• US 20150211855A1
• Filed: 01/28/2015
• Published: 07/30/2015
• Est. Priority Date: 01/28/2014
• Status: Active Grant

• Current Assignee: Murata Manufacturing Co Limited
• Original Assignee: Murata Manufacturing Co Limited
• Inventors: RUOHIO, Jaakko
• Granted Patent: US 9,612,118 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B81B 2201/0242 Gyroscopes
• CPC Class Codes: B81B 3/0043 Increasing angular deflection
• CPC Class Codes: G01C 19/5684 the devices involving a micromechanical structure
• CPC Class Codes: G01C 19/5712 the devices involving a micromechanical structure
• CPC Class Codes: G01C 19/5719 using planar vibrating masses driven in a translation vibration along an axis

Abstract

A ring gyroscope structure with central spring structure that prefers prefers 2θ-modes and makes them low in frequency. The flexing resonance modes that tend to couple to external mechanical excitation are clearly higher that the 2θ-modes. The described structure is thus very robust against external mechanical shocks and vibrations

Claims

1. A planar microelectromechanical gyroscope structure comprising:

a circular structure that extends around a center point;

a central spring structure for suspending the circular structure to four central anchor points, symmetrically located around the center point;

four central circle points and four peripheral circle points between the central circle points on the circular structure, neighboring ones of said four peripheral circle points forming a pair of peripheral circle points and neighboring ones of said four central circle points forming a pair of central circle points,

wherein the central spring structure is configured to connect each of the four central anchor points to a pair of central circle points on the circular structure,

wherein a connection between the central spring structure and the circular structure is configured to transform a radial on-plane displacement of a first circle point of a pair of peripheral or central circle points to a reverse radial on-plane force on a second circle point of the pair of peripheral or central circle points,

wherein a direction of the radial on-plane displacement of the first circle point, and the direction of the radial on-plane force on the second circle point, are orthogonal.

2. The microelectromechanical gyroscope structure of claim 1,

wherein the microelectromechanical gyroscope structure is disposed in two radial directions, wherein each radial direction is aligned to a diagonal line that connects two central anchor points and the center point,

wherein the central spring structure includes four central substructures wherein a central substructure includes at least three springs that are elongate and stiff in the longitudinal direction,

wherein a first spring of the at least three springs extends in one of the two radial directions from an central anchor point to a connection point, where it connects to a second spring and a third spring of the three springs,

wherein the second spring extends between the connection point and the first central circle point, and

wherein the third spring extends between the connection point and the second central circle point.

3. The microelectromechanical gyroscope structure of claim 2, wherein an angle between a line connecting the first central circle point and the connection point and the one radial direction is equal to an angle between a line connecting the second central circle point and the connection point and the one radial direction.

4. The microelectromechanical gyroscope structure of claim 2, further comprising a peripheral spring structure that includes four peripheral anchor points symmetrically located around the center point.

5. The microelectromechanical gyroscope structure of claim 4, wherein the four peripheral anchor points and the four central anchor points are positioned such that each of the peripheral anchor points coincides with one of the diagonal lines of the microelectromechanical gyroscope structure.

6. The microelectromechanical gyroscope structure of claim 4, wherein the peripheral spring structure includes four peripheral substructures, wherein each peripheral substructure includes a fourth spring that connects a peripheral anchor point of the four peripheral anchor points and a peripheral circle point of the four peripheral circle points on the circular structure, a line connecting the peripheral anchor point and the peripheral circle point being aligned to one of the two radial directions.

7. The microelectromechanical gyroscope structure of claim 6, wherein the fourth spring is flexible to motion of the peripheral circle point in the radial direction and opposes motion of the peripheral circle point in a tangential direction, wherein the tangential direction is perpendicular to the one radial direction.

8. The microelectromechanical gyroscope structure of claim 1, wherein the radial on-plane displacements of the central circle points include linear oscillation in a radial direction of the circle of the circular structure.

9. The A microelectromechanical gyroscope structure of claim 8, further comprising a drive structure configured to induce radial on-plane displacements of the central circle points.

10. The microelectromechanical gyroscope structure of claim 9, further comprising a sense structure configured to detect radial on-plane displacements of the peripheral circle points.

11. The microelectromechanical gyroscope structure of claim 8, further comprising a drive structure configured to induce radial on-plane displacements of the peripheral circle points.

12. The microelectromechanical gyroscope structure of claim 9, further comprising a sense structure configured to detect radial on-plane displacements of the central circle points.

13. The microelectromechanical gyroscope structure of claim 9, wherein the radial on-plane displacements are induced or detected piezoelectrically or capacitively.

14. A gyroscope, including the microelectromechanical gyroscope structure of claim 1.