Three-axis Rotation Rate Sensor with Dual Rotor

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Conventional three-axis rotation rate sensors are complex, sensitive to external vibrations and electrical measuring pulses, and require additional elements for Z-direction measurement, making them less robust and more susceptible to interference.

Innovation Solution

A compact three-axis rotation rate sensor design featuring dual-function rotors with deflectable seismic masses, where Coriolis forces induce radial displacement detectable via phase-opposed drive and detection movements, minimizing additional elements and coupling structures, thus reducing spurious modes and interference sensitivity.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If additional elements and coupling structures are added to enable Z-direction measurement, then three-axis measurement capability is achieved, but device complexity and susceptibility to interference increase

Engineering Contradiction:
Improvethree-axis measurement capabilityVSAvoidnumber of spring elements and coupling structures
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The rotor structure is designed to serve multiple functions: it provides X-Y plane rotation rate measurement through conventional Coriolis mass movement, and simultaneously enables Z-axis rotation rate measurement through radial elongation/compression forces. The same rotor and spring elements are used for both measurement directions, eliminating the need for separate Z-axis sensing structures.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The patent combines the Z-axis measurement functionality with the existing X-Y measurement structure by integrating radial force sensing into the rotor-spring system. The spring elements that support the rotor for X-Y measurement also detect radial elongation/compression for Z-axis measurement, merging two measurement functions into a unified structure.

Inventive Principle:
Principle #5Merging (Combining)

2Adaptability or versatility

If additional elements and coupling structures are added for Z-direction measurement, then three-axis measurement capability is achieved, but susceptibility to external vibrations and electrical measuring pulses increases

Engineering Contradiction:
Improvethree-axis measurement capabilityVSAvoidsusceptibility to external vibrations and electrical interference
Core Design Contradiction:
Adaptability or versatilityVSObject-affected harmful factors

Solution Approach 1:

The rotor structure is designed to serve multiple functions: it provides X-Y plane rotation rate measurement through conventional Coriolis mass movement, and simultaneously enables Z-axis rotation rate measurement through radial elongation/compression forces. The same rotor and spring elements are used for both measurement directions, eliminating the need for separate Z-axis sensing structures.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The patent converts the previously harmful radial forces (which were ignored or caused interference) into useful measurement signals for Z-axis detection. By equipotentializing the support structure and using the spring elements as both support and sensing mechanisms, the radial forces become the basis for Z-axis measurement rather than interference.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

3Adaptability or versatility

If soft spring elements are used in complex coupling structures, then three-axis measurement capability is achieved, but sensitivity to external vibrations increases

Engineering Contradiction:
Improvethree-axis measurement capabilityVSAvoidsensitivity to external vibrations
Core Design Contradiction:
Adaptability or versatilityVSObject-affected harmful factors

Solution Approach 1:

The patent extracts the Z-axis measurement function from the concept of adding separate soft coupling structures and instead integrates it into the existing rigid rotor and spring element system. By removing the need for additional soft coupling elements and using the existing springs for both support and Z-axis sensing, the design eliminates the vibration sensitivity associated with multiple soft elements.

Inventive Principle:
Principle #2Taking out (Extraction)

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 sensor achieves robustness against vibrations, low energy decoupling, and high sensitivity with improved surface area utilization, reducing manufacturing variations and frequency distribution, resulting in a more precise and less sensitive device.

Implementation Method 1

When an external rotation whose rotational axis is directed in parallel to the XY plane is applied to the sensor, Coriolis forces act on the rotors and tilt the rotors relative to the plane

Methodology Applied
Scientific EffectCoriolis force: Coriolis Force

Implementation Method 2

the radially extending Coriolis forces effectuate a displacement of the seismic masses in the radial direction of the rotor, which may be correspondingly detected

Methodology Applied
Scientific EffectCoriolis force: Coriolis Force

Implementation Method 3

This deflection may in turn be determined via a change in capacitance with respect to stationary detection electrodes

Methodology Applied
Scientific EffectCapacitance: Capacitance

Data Source

PatentUS11846509B2Three-axis rotation rate sensor including a substrate and a double rotor
Publication Date: 2023.12.19 ROBERT BOSCH GMBH
  • US11846509B2 patent drawing
  • US11846509B2 patent drawing
  • US11846509B2 patent drawing

AI summary

A three-axis rotation rate sensor including a substrate and a double rotor. The double rotor includes a first rotor and a second rotor which are elastically connected to one another via a first coupling element so that the two rotors are excitable to rotary oscillations in phase opposition. The first rotor includes a first seismic mass and a second seismic mass that are deflectably supported with respect to the first rotor, and the second rotor includes a third seismic mass and a fourth seismic mass that are deflectably supported with respect to the second rotor. The first mass is connected to the third mass via a first rocker element so that upon a lateral deflection of the first mass, the third mass is deflected in a direction opposite the lateral deflection of the first mass.