Resonator Stress Isolation via Segmented Mass-Spring Network

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Solution Overview

Problem

Existing gyroscope resonator designs face challenges in optimizing multiple properties simultaneously due to a fixed relationship between mass and stiffness, leading to suboptimal performance in stress isolation and frequency operation, with stresses affecting bias and damping unpredictably.

Innovation Solution

The resonator is separated into thin compliant 'spring' elements and stiff 'mass' elements, with a stress isolation network of concentric symmetric regions of varying stiffness, allowing independent control of spring constant, mass, thermoelastic loss, and operating frequency, and incorporating slots to reduce stress asymmetry.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If a fully distributed mass/spring geometry is used, then the resonator structure is simple and manufacturable, but the relationship between mass and stiffness is fixed, limiting optimization freedom

Engineering Contradiction:
Improveresonator structure manufacturabilityVSAvoidoptimization freedom
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The resonator is segmented into discrete mass elements and discrete spring elements rather than using a fully distributed continuous structure. This segmentation allows independent optimization of mass distribution and stiffness distribution, providing multiple degrees of freedom for optimizing the resonator geometry while maintaining manufacturability through standard fabrication processes.

Inventive Principle:
Principle #1Segmentation

2Strength

If stresses propagate into the resonator, then the resonator is structurally connected to the mounting, but the stresses cause mode splitting and bias errors in gyroscope performance

Engineering Contradiction:
Improvestructural connectionVSAvoidgyroscope bias accuracy
Core Design Contradiction:
StrengthVSMeasurement precision

Solution Approach 1:

A stress isolation network is introduced as an intermediary structure between the mounting and the resonator active area. This network comprises concentric symmetric regions of alternating high and low stiffness that decouple external mounting stresses from the resonator, preventing stress-induced mode splitting and bias errors while maintaining structural support.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The resonator structure employs local variations in stiffness through the stress isolation network, with concentric regions of high stiffness providing structural support and low stiffness regions isolating stresses. This local differentiation allows the structure to simultaneously maintain strength and protect the resonator from stress-induced performance degradation.

Inventive Principle:
Principle #3Local quality

3Adaptability or versatility

If discrete masses on discrete springs are used, then optimization freedom increases, but the device complexity increases compared to distributed designs

Engineering Contradiction:
Improveoptimization freedomVSAvoidresonator structure complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The resonator is segmented into discrete mass elements and discrete spring elements arranged in a systematic pattern around the periphery. This segmentation provides multiple degrees of freedom for independent optimization of mass and stiffness distributions while maintaining a relatively simple overall structure that can be fabricated using standard processes, thus achieving optimization freedom without excessive complexity.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS10794700B1Stress isolation of resonating gyroscopes
Publication Date: 2020.10.06 GARMIN INTERNATIONAL INC
  • US10794700B1 patent drawing
  • US10794700B1 patent drawing
  • US10794700B1 patent drawing

AI summary

To isolate an active portion of a gyroscope resonator from mounting stresses propagating through a resonator attachment center, the resonator includes a stress isolation feature that includes alternating concentric symmetric regions of high and low stiffness. The resonator may be separated into a large number of thin, compliant spring elements and larger stiff mass elements, the aggregate areas of which optimized for an aggregate resonator spring constant (by selecting a width and a length of the spring elements), an aggregate mass (by selecting a size of the mass elements), a thermoelastic loss maximum (by selecting a width of the spring elements) and an operating frequency (by selecting a ratio of the aggregate spring to the aggregate mass).