THREE-AXIS GYROSCOPE

• US 20130239679A1
• Filed: 03/13/2012
• Published: 09/19/2013
• Est. Priority Date: 03/13/2012
• Status: Abandoned Application

• Current Assignee: Hewlett-Packard Development Company, L.P. (HP Inc.)
• Original Assignee: Hewlett-Packard Development Company, L.P. (HP Inc.)
• Inventors: Kornilovich, Pavel
• Application Number:
  US13/418,999
• Publication Number:
  US 20130239679A1
• Time in Patent Office: Days
• US Class Current: 73/504.12
• CPC Class Codes: G01C 19/5712 the devices involving a micromechanical structure
• CPC Class Codes: G01C 19/5733 Structural details or topology

Abstract

Apparatus related to measuring angular velocities in three-space are provided. Drive masses distributed in a plane are force-oscillated in two orthogonal directions such that gyration of the collective is performed. Sense masses coupled by flexures to the drive masses are each displaceable along a respective single degree of freedom in response to angular velocities about a vector orthogonal to that degree of freedom. Electronic circuitry measures the respective sense mass displacements and provides corresponding signaling. The drive masses and sense masses can be formed such that a microelectromechanical system (MEMS) device is defined.

Claims

1. An apparatus, comprising:

a plurality of drive masses disposed in a plane, the drive masses configured to be simultaneously oscillated in two orthogonal directions in the plane; and

a plurality of sense masses, each sense mass configured to be displaced within a respective single-axis range in response to angular velocity of the apparatus about a vector orthogonal to the respective single-axis range, each drive mass supporting one or more of the sense masses.

2. The apparatus according to claim 1 further comprising electronic circuitry configured to detect displacements of the respective sense masses.

3. The apparatus according to claim 2, the electronic circuitry further configured to provide electronic signaling corresponding to angular velocities of the apparatus about three mutually-orthogonal axes.

4. The apparatus according to claim 1, the sense masses and the drive masses being respective aspects of a microelectromechanical system (MEMS) device.

5. The apparatus according to claim 1, the drive masses supported within a frame, the frame fixedly joined to the substrate, the frame and the drive masses and the sense masses formed from a single silicon wafer by way of photolithography.

6. The apparatus according to claim 1 further comprising a plurality of accelerometers respectively disposed proximate to the drive masses.

7. The apparatus according to claim 1, the drive masses being mechanically coupled to each other by way of respective extensions.

8. The apparatus according to claim 1, the drive masses and the sense masses formed from a monolithic material.

9. The apparatus according to claim 1, each sense mass being supported by either flexure coupling or torsional coupling to the corresponding drive mass.

10. The apparatus according to claim 1, the drive masses configured such that the simultaneous oscillation in the two orthogonal directions results in three-hundred sixty degree gyration within the plane.

11. A microelectromechanical system (MEMS) device, comprising:

a substrate;

a plurality of drive masses supported in overlying relationship to the substrate and distributed in a plane, the drive masses configured to be gyrated as an entity by way of forced oscillations in two orthogonal axes in the plane; and

a plurality of pairs of sense masses, each pair supported by a respective one of the drive masses, each sense mass displaceable in a single degree of freedom in response to angular velocity of the MEMS device about a vector orthogonal to the respective degree of freedom.

12. The MEMS device according to claim 11, each pair including:

a sense mass configured to be displaceable in a single degree of freedom within the plane; and

a sense mass configured to be displaceable in a single degree of freedom orthogonal to the plane.

13. The MEMS device according to claim 11, the sense masses collectively defining three mutually-orthogonal degrees of freedom so as respond to angular velocities of the MEMS device about three mutually-orthogonal vectors.

14. The MEMS device according to claim 11 further comprising electronic circuitry configured to sense respective displacements of the sense masses, the electronic circuitry further configured to provide electronic signaling in accordance with the sensing.

15. The MEMS device according to claim 11 further comprising a plurality of accelerometers respectively supported on the substrate.

16. The MEMS device according to claim 11 further comprising a frame fixed to the substrate, the drive masses suspended within the frame, the frame and the drive masses and the sense masses formed from a monolithic material.