Circular Force Generator With Counterbalancing Rotors

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Solution Overview

Problem

Circular force generators (CFGs) face issues with rotor inertia, power consumption, and bearing drag, especially when operating at high frequencies or tracking rapidly varying frequencies, which can lead to undesirable power regeneration and rotating moments, making it challenging to effectively reduce vibrations in mechanical structures.

Innovation Solution

The design includes a first and second rotor assembly with spinning bearings and eccentric masses that are rotatable about a common shaft, with adjustable relative angular positions to control the magnitude and phase of the combined rotating force, minimizing rotor inertia and bearing drag by using precision bearings and frameless annular motors, and phase-shifting bearings to eliminate radial torque and reduce power consumption.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Force

If rotor inertia is increased to generate sufficient vibratory force, then force generation capability is improved, but power consumption during rotor acceleration and deceleration increases

Engineering Contradiction:
Improvevibratory forceVSAvoidpower consumption
Core Design Contradiction:
ForceVSUse of energy by moving object

Solution Approach 1:

The patent employs counterbalancing mechanisms where additional masses are strategically positioned to offset the inertial effects of the primary rotor masses. This allows the system to generate the required vibratory forces while the counterweights neutralize the unwanted inertial forces during acceleration and deceleration, thereby reducing power consumption.

Inventive Principle:
Principle #8Anti-weight (Counterweight)

Solution Approach 2:

The invention transitions from a single-plane rotor configuration to a multi-plane or three-dimensional arrangement of masses and counterweights. By distributing masses across multiple planes perpendicular to the rotation axis, the system achieves force generation in one dimension while counterbalancing inertial effects in other dimensions, resolving the contradiction between force generation and power consumption.

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

2Adaptability or versatility

If rotor speed is increased to track rapidly varying frequencies, then frequency tracking capability is improved, but bearing drag and power consumption increase

Engineering Contradiction:
Improvefrequency tracking capabilityVSAvoidbearing drag
Core Design Contradiction:
Adaptability or versatilityVSLoss of energy

Solution Approach 1:

The rotor system is segmented into multiple independent rotating masses, each capable of operating at optimized speeds for specific frequency ranges. This segmentation allows the system to track rapidly varying frequencies by selectively activating or adjusting individual segments rather than requiring the entire rotor to operate at high speeds, thereby reducing bearing drag and energy loss.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention implements dynamically adjustable rotor configurations where masses can be repositioned or their rotational speeds independently controlled. This dynamic adaptability enables the system to optimize bearing loads and minimize drag across different operating conditions while maintaining frequency tracking capability.

Inventive Principle:
Principle #15Dynamics

3Reliability

If CFG operates at high frequencies to reduce vibration effectively, then vibration reduction performance is improved, but bearing drag leads to increased power consumption

Engineering Contradiction:
Improvevibration reduction performanceVSAvoidpower consumption
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

The patent utilizes counterweight mechanisms specifically designed to balance the high-frequency rotational masses. These counterweights rotate in opposition to the primary masses, neutralizing the inertial forces generated during high-frequency operation. This allows the CFG to maintain effective vibration reduction performance while significantly reducing the bearing drag and associated power consumption that would otherwise result from high-speed rotation.

Inventive Principle:
Principle #8Anti-weight (Counterweight)

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

This configuration significantly reduces rotor inertia and bearing drag, achieving a safer and gentler ride by effectively damping vibrations across various applications, including vehicles and machinery, while minimizing power consumption and eliminating rotating moments.

Implementation Method 1

spinning bearing mounted about a shaft

Methodology Applied
Scientific EffectFriction: Friction

Implementation Method 2

spinning bearing mounted about a shaft

Methodology Applied
Scientific EffectBall Bearing: Ball Bearing

Implementation Method 3

first eccentric mass extending in a first axial direction away from the first position

Methodology Applied
Scientific EffectEccentric: Eccentric

Implementation Method 4

first eccentric mass and the second eccentric mass are each rotatable about the shaft to generate a combined rotating force

Methodology Applied
Scientific EffectCentrifugal Force: Centrifugal Force

Implementation Method 5

phase-shifting bearing connected to the first eccentric mass

Methodology Applied
Scientific EffectFriction: Friction

Implementation Method 6

phase-shifting bearing allow for selective adjustment of a relative angular position

Methodology Applied
Scientific EffectMechanical Advantage: Mechanical Advantage

Data Source

PatentUS11660638B2Wide bandwidth circular force generator devices, systems, and methods
Publication Date: 2023.05.30 LORD CORP
  • US11660638B2 patent drawing
  • US11660638B2 patent drawing
  • US11660638B2 patent drawing

AI summary

Circular force generator devices (100), systems, and methods for damping vibrations which include two complementary rotor assemblies (110, 120) that are rotatable together about a common shaft (102) but that have an adjustable rotational position (P1, P2) with respect to one another such that a significant reduction in rotor inertia and bearing drag relative to conventional CFG configurations is provided. The present architecture creates virtually zero rotating moment.