3D Micro Shell Rate-Integrating Gyroscope with Optical Sensing

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Solution Overview

Problem

Current micro gyroscopes lack the necessary accuracy for navigation applications, particularly in GPS-denied environments, where position sensing errors grow exponentially with time, and require several orders of magnitude higher precision than stabilization applications.

Innovation Solution

A three-dimensional micro shell rate-integrating gyroscope is developed, featuring a support substrate, an inner shell, a resonator, driving electrodes, and integrated optical sensors, which operates by detecting changes in the resonator's motion using electrostatic driving and optical sensing, and is thermally isolated to maintain precision.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If current micro gyroscope designs are used, then manufacturing cost is reduced and device size is minimized, but measurement precision and accuracy are insufficient for navigation applications

Engineering Contradiction:
Improveangular rate detection accuracyVSAvoidgyroscope structure complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent transitions from planar 2D resonator designs to three-dimensional hemispherical shell resonators. This dimensional change enables higher measurement precision by creating resonant structures with superior mechanical Q-factors and reduced sensitivity to fabrication variations, while the hemispherical geometry provides inherent robustness against shock and vibration that would otherwise complicate the device structure

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The patent replaces traditional capacitive sensing mechanisms with optical sensing methods. By using optical interferometry to detect resonator position and motion, the system achieves higher measurement precision without requiring complex capacitive electrode arrangements, thereby reducing overall device complexity while maintaining micro-scale dimensions

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Measurement precision

If micro scale dimensions are used, then device size is minimized and cost is reduced, but accuracy is insufficient for GPS-denied navigation

Engineering Contradiction:
Improveposition sensing accuracyVSAvoidgyroscope mass
Core Design Contradiction:
Measurement precisionVSWeight of moving object

Solution Approach 1:

The patent employs three-dimensional hemispherical shell resonators instead of planar structures. This dimensional transformation allows the micro-scale device to achieve navigation-grade accuracy by creating resonant modes with higher quality factors and reduced sensitivity to manufacturing tolerances, thereby improving position sensing accuracy without increasing device mass

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The patent optimizes the resonator geometry by varying shell thickness parameters, creating regions of different thickness to enhance specific resonant modes. This parameter optimization improves the mechanical Q-factor and measurement precision of the micro-scale gyroscope, enabling navigation accuracy while maintaining minimal mass

Inventive Principle:
Principle #35Parameter changes

3Reliability

If traditional resonator designs are used, then device simplicity is maintained, but robustness against shock and vibration is insufficient

Engineering Contradiction:
Improveshock and vibration resistanceVSAvoidresonator structure complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent utilizes hemispherical shell geometry for the resonator structure. The curved spherical form provides inherent robustness against shock and vibration by distributing mechanical stresses uniformly throughout the structure, eliminating the need for additional protective elements or complex suspension mechanisms that would increase device complexity

Inventive Principle:
Principle #14Spheroidality (Curvature)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The gyroscope achieves high accuracy and stability, capable of detecting sub-picometer amplitude changes, effectively addressing the precision requirements for navigation applications while maintaining robustness against shock and vibration.

Implementation Method 1

Two or more driving electrodes are formed on the support substrate and are arranged around periphery of the resonator. The two or more driving electrodes are configured to drive the resonator electrostatically.

Methodology Applied
Scientific EffectElectrostatic force: Electrostatics

Implementation Method 2

A plurality of optical sensors are integrated into the support structure, such that each optical sensor is configured to detect motion of the resonator.

Methodology Applied
Scientific EffectOptical sensing: Light

Implementation Method 3

The platform is thermally isolated from the outer shell.

Methodology Applied
Scientific EffectThermal isolation: Thermal Insulation

Data Source

PatentUS11548805B2Gyroscope and fabrication process
Publication Date: 2023.01.10 THE RGT UNIV OF MICHIGAN
  • US11548805B2 patent drawing
  • US11548805B2 patent drawing
  • US11548805B2 patent drawing

AI summary

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.