Torsion Vibration Damper Axial Centering Guide Bodies

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Solution Overview

Problem

Existing torsional vibration damper arrangements for vehicle drive trains face challenges in achieving a compact design with good decoupling quality between the primary and secondary sides, as they often lack effective axial security for deflection masses and guide bodies, leading to potential misalignment and reduced vibration damping efficiency.

Innovation Solution

A torsional vibration damper arrangement featuring a deflection mass carrier with two carrier disks and guide tracks that utilize roller-like guide bodies to maintain axial centering and minimize friction, ensuring the deflection masses are securely positioned and move radially to absorb vibrational energy effectively.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If guide bodies are used to enable friction-free movement of deflection masses in guide tracks, then vibration damping efficiency is improved, but axial centering and security of guide bodies relative to carrier disks is lost leading to potential misalignment

Engineering Contradiction:
Improvevibration damping efficiencyVSAvoidaxial centering and security
Core Design Contradiction:
Loss of energyVSReliability

Solution Approach 1:

The guide bodies are given a conical shape with axial extension, transforming them from purely radial rollers to three-dimensional elements that can simultaneously provide radial movement guidance and axial centering. The conical surface allows friction-free radial motion while the axial extension with centered positioning provides the missing axial stability dimension.

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

Solution Approach 2:

The guide bodies are designed to self-center axially through their conical geometry and interaction with the guide tracks. The axial centering is achieved automatically by the geometry itself without requiring additional external centering components, making the system self-sufficient for both radial and axial positioning.

Inventive Principle:
Principle #25Self-service

2Reliability

If additional components are added to secure guide bodies axially, then axial positioning is improved, but device complexity increases

Engineering Contradiction:
Improveaxial positioningVSAvoidnumber of components
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The guide bodies merge multiple functions into a single component: radial guidance, axial centering, and friction-free movement. This consolidation eliminates the need for separate centering components that would otherwise be required, reducing overall device complexity while maintaining reliability.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The guide bodies are designed as multi-functional elements that simultaneously perform radial guidance, axial centering, and support the deflection masses. This universal design approach allows one component to fulfill multiple roles that would traditionally require separate dedicated components.

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

3Loss of energy

If deflection masses are allowed to move radially for vibration damping, then vibration absorption is improved, but axial stability may be compromised

Engineering Contradiction:
Improvevibration absorptionVSAvoidaxial stability
Core Design Contradiction:
Loss of energyVSStability of the object's composition

Solution Approach 1:

The movement of deflection masses is segmented into independent radial and axial components. Radial movement is permitted for vibration damping while axial position is independently controlled and centered, allowing each degree of freedom to be optimized separately for its specific function.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The guide bodies act as intermediary elements between the deflection masses and the carrier disks. They mediate the movement by allowing radial displacement for vibration absorption while simultaneously maintaining axial centering, thus decoupling the two movement dimensions.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 design enhances decoupling quality and vibration damping efficiency by maintaining axial centering without additional components, allowing for friction-free movement and improved axial positioning of deflection masses, thus effectively reducing rotational irregularities in the drive train.

Implementation Method 1

roller-like guide bodies to maintain axial centering and minimize friction

Methodology Applied
Scientific EffectRolling: Roller

Implementation Method 2

minimize friction

Methodology Applied
Scientific EffectFriction: Friction

Implementation Method 3

at least one deflection mass carried on the deflection mass carrier from a base with a maximum distance from the axis of rotation into a deflection position with a smaller distance from the axis of rotation

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Data Source

PatentEP2636923B1Torsion vibration damper assembly and oscillation damper device, in particular in a torsion vibration damper arrangement
Publication Date: 2019.11.20 ZF FRIEDRICHSHAFEN AG
  • EP2636923B1 patent drawingFigure 1
  • EP2636923B1 patent drawingFigure 2~4
  • EP2636923B1 patent drawingFigure 5~7

AI summary

The arrangement has a primary side to be coupled to a drive element and a secondary side rotated with respect to the primary side about an axis of rotation against action of a damper element assembly. The secondary side includes circumferential support elements (102, 104) including circumferential support regions (106, 108) and an angular disk-type mass element. A connecting element (118) i.e. riveted bolt, is connected with one of the circumferential supporting elements and a deflection mass support (12) through the secondary-sided mass element.