Roller Bearing Inner Ring Cooling for Axial Temperature Homogeneity

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Solution Overview

Problem

Turbine engine bearings face thermal asymmetry due to high temperatures, leading to excessive internal clearances that affect engine dynamics, as current designs over-dimension clearances to accommodate the hottest axial portions, resulting in inefficiencies.

Innovation Solution

The design incorporates through-holes in the inner ring of the roller bearing to allow differential thermal cooling by oil circulation, specifically targeting the hotter axial end portion, reducing the need for oversized clearances and enhancing thermal homogeneity.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If internal clearances are over-dimensioned to accommodate the hottest axial portions, then reliability is improved, but device complexity and operational efficiency deteriorate

Engineering Contradiction:
Improvebearing reliabilityVSAvoidbearing structure complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The invention applies local quality by introducing through-holes specifically in the first axial end annular portion (the hotter portion) of the inner ring, while leaving the second axial end annular portion without through-holes. This localized modification allows differential thermal cooling where it is most needed, reducing the thermal gradient across the inner ring without requiring complex modifications to the entire bearing structure. The selective placement of cooling features in the hottest region resolves the contradiction by providing targeted reliability improvement without proportionate increases in device complexity.

Inventive Principle:
Principle #3Local quality

2Productivity

If internal clearances are reduced for better engine dynamics, then productivity is improved, but reliability deteriorates due to thermal expansion

Engineering Contradiction:
Improveengine dynamics efficiencyVSAvoidbearing reliability
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The invention applies preliminary action by implementing through-holes and oil circulation paths in advance within the inner ring structure, before thermal expansion occurs during operation. The cooling system proactively removes heat from the hottest axial portions, preventing excessive thermal expansion before it can compromise the reduced internal clearances. This preventive thermal management allows the bearing to maintain smaller, more efficient clearances while preserving reliability through advance thermal control.

Inventive Principle:
Principle #10Preliminary action

3Ease of manufacture

If uniform cooling is applied to the entire inner ring, then manufacturing simplicity is improved, but temperature distribution and operational performance worsen due to thermal asymmetry

Engineering Contradiction:
Improvecooling system manufacturingVSAvoidinner ring temperature distribution
Core Design Contradiction:
Ease of manufactureVSTemperature

Solution Approach 1:

The invention resolves this contradiction by applying local quality through asymmetric placement of through-holes in the inner ring. The through-holes are concentrated in the first axial end annular portion that is more exposed to heat, while the second axial end annular portion remains without through-holes or has fewer of them. This non-uniform distribution of cooling features matches the asymmetric thermal exposure, providing optimal temperature control without requiring complex multi-zone cooling systems. The manufacturing complexity remains low because the through-holes can be created using standard drilling or machining processes, while the temperature distribution is significantly improved by targeting the hottest regions.

Inventive Principle:
Principle #3Local quality

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 approach reduces the dimensioning of internal clearances, improving thermal homogeneity and operational efficiency of the turbine engine by targeted cooling of the hotter areas, thereby minimizing thermal gradients and enhancing overall engine performance.

Implementation Method 1

the through-holes being formed in the first axial end annular portion and distributed around the axis in order to allow for a circulation of oil coming from the oil injection device through the first axial end annular portion

Methodology Applied
Scientific EffectThermal cooling: Cooling

Implementation Method 2

circulation of oil coming from the oil injection device through the first axial end annular portion

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 3

an oil injection device configured to supply the rolling elements with oil in such a way as to ensure the lubrication of the latter

Methodology Applied
Scientific EffectLubrication: Lubrication

Data Source

PatentUS11326472B2Turbine engine comprising means for axially homogenising the temperature of an inner ring of a roller bearing
Publication Date: 2022.05.10 SAFRAN AIRCRAFT ENGINES SAS
  • US11326472B2 patent drawing
  • US11326472B2 patent drawing
  • US11326472B2 patent drawing

AI summary

A turbine engine comprises a rotor shaft and a roller bearing supporting the shaft in rotation along an axis. The bearing comprises an inner ring, an outer ring, and rolling elements engaged between the inner and outer rings. The inner ring has a first axial end annular portion that is more exposed to heat during operation than a second axial end annular portion thereof. The turbine engine further comprises an oil injection device configured to supply the rolling elements with oil for lubrication of the latter. In order to homogenise the temperature of the inner ring, the latter comprises through-holes formed in the first axial end annular portion and distributed around the axis in order to allow for a circulation of oil coming from the oil injection device through the first axial end annular portion, thereby providing additional cooling to the first end annular portion.