Gyroscope and fabrication process

Patent metadata

Field	Value
Publication number	US-10532943-B2
Application number	US-201715444450-A
Country	US
Kind code	B2
Filing date	Feb 28, 2017
Priority date	Feb 29, 2016
Publication date	Jan 14, 2020
Grant date	Jan 14, 2020

Abstract

Gyroscopes are sensors that measure angular rate and angular orientation. A three-dimensional fused silica micro shell rate-integrating gyroscope is presented. One aspect of the gyroscope includes the use of optical sensors to detect motion of the resonator. The proposed gyroscope is attractive because it achieves several magnitudes higher accuracy as well as high vibration and shock insensitivity from a novel resonator design as well as other unique manufacturing processes.

First claim

What is claimed is:

1. A gyroscope, comprising:
a support substrate;
an inner shell attached to the substrate and defining an inner cavity between an interior surface of the inner shell and a top surface of the support substrate;
a hollow hemispherical resonator having an inner concave surface facing the support substrate, the resonator disposed in the inner cavity and mounted above the top surface of the support substrate, wherein the resonator has a thickness with a minimum value proximate to a rim of the resonator, where thickness of the resonator increases from the minimum value to a maximum value at the center of the resonator;
a first stem integral with the resonator and extending from a center of the inner surface of the resonator to the support substrate;
two or more driving electrodes formed on the support substrate and arranged around periphery of the resonator, wherein the two or more driving electrodes are configured to drive the resonator electrostatically; and
a plurality of optical sensors encapsulated within the support substrate, wherein each optical sensor is configured to detect motion of the resonator, wherein the optical sensors are arranged adjacent to the periphery of the resonator and positioned underneath a rim of the resonator.

2. The gyroscope of claim 1 wherein the resonator has a second integral stem extending from a center of an outer surface of the resonator and attaches to the interior surface of the inner shell.

3. The gyroscope of claim 1 , wherein the rim of the resonator has a thickness larger than the minimum value.

4. The gyroscope of claim 1 wherein the resonator has a conductive coating disposed on an exterior surface thereof and adjacent to the rim of the resonator.

5. The gyroscope of claim 4 wherein the conductive coating is patterned as a ring on the exterior surface and proximate to the rim of the resonator.

6. The gyroscope of claim 4 wherein the conductive coating is patterned as a plurality of discrete electrodes disposed around a circumference of the resonator and proximate to the rim of the resonator, where each the plurality of discrete electrodes aligns with one of the two or more driving electrodes.

7. The gyroscope of claim 1 wherein the optical sensors include vertical-cavity surface-emitting lasers.

8. A system comprising:
the gyroscope of claim 1 ;
a platform; and
an outer shell, where the platform is enclosed by the outer shell, and the platform is thermally isolated from the outer shell.

9. A resonator, comprising:
a support substrate;
an inner shell attached to the substrate and defining an inner cavity between an interior surface of the inner shell and a top surface of the support substrate;
a hollow hemispherical resonating member having an inner concave surface facing the support substrate, the resonating member disposed in the inner cavity and mounted above the top surface of the support substrate, the resonating member has a first integral stem extending from a center of the inner surface of the resonating member and attaches to support substrate, wherein the resonating member has a thickness with a minimum value proximate to a rim of the resonator, where thickness of the resonator increases from the minimum value to a maximum value at the center of the resonator;
two or more driving electrodes formed on the support substrate and arranged around periphery of the resonating member, wherein the two or more driving electrodes are configured to drive the resonating member electrostatically; and
a plurality of optical sensors encapsulated within the support substrate, wherein each optical sensor is configured to detect motion of the resonating member, wherein the optical sensors are arranged around the periphery of the resonating member and positioned underneath the rim of the resonating member.

10. The resonator of claim 9 wherein the resonating member has a second integral stem extending from a center of an outer surface of the resonating member and attaches to the interior surface of the inner shell.

11. The resonator of claim 9 , wherein the rim of the resonator has a thickness larger than the minimum value.

12. The resonator of claim 9 wherein the resonating member has a conductive coating disposed on an exterior surface thereof and adjacent to the rim of the resonating member.

13. The resonator of claim 12 wherein the conductive coating is patterned as a ring on the exterior surface and proximate to the rim of the resonator.

14. The resonator of claim 12 wherein the conductive coating is patterned as a plurality of discrete electrodes disposed around a circumference of the resonating member and proximate to the rim of the resonating member, where each of the plurality of discrete electrodes aligns with one of the two or more driving electrodes.

15. The resonator of claim 9 wherein the optical sensors include vertical-cavity surface-emitting lasers.

Assignees

• Univ Michigan Regents

Inventors

• Najafi Khalil
• Cho Jae Yoong
• DARVISHIAN Ali
• He Guohong
• Shiari Behrouz
• Nagourney Tal

Classifications

• G01C19/5691

  of essentially three-dimensional [3D] vibrators, e.g. wine glass-type vibrators · CPC title

• C03B23/0357

  by suction without blowing, e.g. with vacuum or by venturi effect · CPC title

• G01C25/00

  Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass (testing, calibrating or compensating compasses G01C17/38) · CPC title

• C03B23/0252 Primary

  by gravity only, e.g. sagging (C03B23/035 takes precedence) · CPC title

• G01D5/34

  the beams of light being detected by photocells · CPC title