Viscoelastic Damping Ring for Turbomachine Stator Vane Pivot

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Solution Overview

Problem

High vibration levels in high-power engines cause cracks in the triple connection radius zones of variable pitch stator vanes, leading to structural weakening and potential blade breakage.

Innovation Solution

A vibration damping ring is designed to be mounted around the pivot of the variable pitch stator vane, comprising a rigid external shroud and a flexible viscoelastic internal part, which secures to the pivot rod and absorbs vibrations, allowing for rotation while dissipating mechanical energy.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If high-power engines are used to improve power output, then power increases, but vibration levels increase causing cracks in the triple connection radius zones

Engineering Contradiction:
Improveengine powerVSAvoidvibration-induced cracks
Core Design Contradiction:
PowerVSObject-affected harmful factors

Solution Approach 1:

The patent applies viscoelastic material in the damping ring to convert harmful vibrations into beneficial energy dissipation through hysteresis damping. The viscoelastic material absorbs vibrational energy and dissipates it as heat, transforming the harmful vibration effect into a protective damping function that prevents crack formation in the triple connection radius zones

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

2Object-affected harmful factors

If a damping ring with viscoelastic material is added to reduce vibrations, then vibration damping improves, but device complexity increases

Engineering Contradiction:
Improvevibration levelsVSAvoidbearing structure complexity
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

The damping ring is nested within the existing bearing structure, with the viscoelastic material positioned between the pivot rod and the bearing outer race. This nested configuration allows the damping function to be integrated into the existing bearing assembly without requiring separate mounting operations or additional external components, thereby minimizing the increase in device complexity while achieving effective vibration reduction

Inventive Principle:
Principle #7Nested doll (Nesting)

3Ease of operation

If the pivot rod rotates freely in the bearing, then rotation smoothness improves, but vibration transmission increases causing structural cracks

Engineering Contradiction:
Improvepivot rotation smoothnessVSAvoidvibration transmission
Core Design Contradiction:
Ease of operationVSObject-affected harmful factors

Solution Approach 1:

The viscoelastic material in the damping ring acts as an intermediary element between the rotating pivot rod and the stationary bearing housing. This intermediary layer provides the necessary rotational interface while simultaneously filtering and dissipating vibrational energy, allowing smooth rotation to occur without transmitting harmful vibrations to the bearing structure and preventing crack formation

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

The damping ring effectively reduces vibrations within the vane, preventing cracks and ensuring structural integrity by absorbing and dissipating energy, thus enhancing the durability of the variable pitch stator vanes.

Implementation Method 1

an internal part solidly connected to the external part and ensuring a damping function... The material of the hollow cylindrical part is a viscoelastic material... which absorbs vibrations, allowing for rotation while dissipating mechanical energy

Methodology Applied
Scientific EffectViscoelastic damping: Viscoelasticity

Data Source

PatentUS20240151153A1Bearing for turbomachine variable pitch stator vane pivot, stator vane comprising such a bearing and turbomachine comprising such stator vanes
Publication Date: 2024.05.09 SAFRAN AIRCRAFT ENGINES SAS
  • US20240151153A1 patent drawing
  • US20240151153A1 patent drawing
  • US20240151153A1 patent drawing

AI summary

A bearing for a turbomachine variable pitch stator vane pivot mounted in a bore of a casing of the turbomachine and including a bushing integral with the bore and allowing rotation of a pivot rod within the casing, and additionally a ring mounted so as to be integral with the pivot rod inside the bushing and including an outer part providing the stiffening of the ring and an inner part integral with the outer part and providing a damping function.