Oil Recovery Gutter Surface Coating for Faster Turbomachine Evacuation

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Solution Overview

Problem

Aircraft turbomachines require a high oil flow rate for operation, and existing oil recovery systems in mechanical reducers are inefficient in channeling and evacuating oil quickly enough to be cooled and reinjected into the lubrication system.

Innovation Solution

A mechanical part for an aircraft turbomachine, specifically an annular lubricating oil recovery gutter, is designed with a hydrophobic and/or lipophobic coating or surface texturing to enhance oil flow by reducing the spreading coefficient and promoting drop formation rather than film spreading.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If a conventional oil recovery gutter is used, then the structure is simple, but the oil flow rate is insufficient and evacuation is slow

Engineering Contradiction:
Improveoil flow rateVSAvoidoil evacuation time
Core Design Contradiction:
ProductivityVSLoss of time

Solution Approach 1:

The patent applies parameter changes by modifying the surface properties of the gutter through hydrophobic and/or lipophobic coating or surface texturing. This changes the interaction between the oil and the gutter surface, reducing adhesion and promoting faster oil flow and evacuation. The surface treatment alters the wetting characteristics, enabling oil to form droplets that roll off more quickly rather than spreading into films that slow down evacuation.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If the oil flow rate is increased, then lubrication efficiency improves, but the time required to cool and recycle oil increases

Engineering Contradiction:
Improvelubrication efficiencyVSAvoidoil recycling time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The surface treatment changes the physical parameters of the gutter-oil interface, creating a more efficient oil flow regime. By reducing surface adhesion through hydrophobic/lipophobic properties, the oil maintains better flow characteristics even at higher flow rates, allowing for faster evacuation and recycling without compromising lubrication efficiency.

Inventive Principle:
Principle #35Parameter changes

3Productivity

If the oil is evacuated quickly, then recycling efficiency improves, but the oil flow becomes more turbulent and difficult to control

Engineering Contradiction:
Improveoil evacuation speedVSAvoidoil flow stability
Core Design Contradiction:
ProductivityVSStability of the object's composition

Solution Approach 1:

The hydrophobic and/or lipophobic surface treatment modifies the flow regime by reducing adhesion forces between the oil and gutter surface. This allows for faster evacuation while maintaining flow stability, as the oil forms cohesive droplets that roll smoothly along the surface rather than adhering and creating irregular flow patterns. The surface treatment effectively decouples evacuation speed from flow instability.

Inventive Principle:
Principle #35Parameter changes

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 hydrophobic and/or lipophobic surface treatment facilitates faster oil flow and evacuation, reducing the impact of ventilation air and allowing for quicker recycling of oil, which in turn reduces oil consumption during turbomachine operation.

Implementation Method 1

said surface comprising a coating that is more hydrophobic and/or lipophobic than said surface or a surface texturing rendering said surface more hydrophobic and/or lipophobic

Methodology Applied
Scientific EffectHydrophobic effect: Hydrophobe

Implementation Method 2

said surface comprising a coating that is more hydrophobic and/or lipophobic than said surface or a surface texturing rendering said surface more hydrophobic and/or lipophobic

Methodology Applied
Scientific EffectLipophobic effect: Hydrophobe

Data Source

PatentUS12209652B2Mechanical part for an aircraft turbomachine and corresponding turbomachine
Publication Date: 2025.01.28 SAFRAN TRANSMISSION SYST
  • US12209652B2 patent drawing
  • US12209652B2 patent drawing
  • US12209652B2 patent drawing

AI summary

A mechanical part for an aircraft turbomachine, the mechanical part being made of metal and comprising at least one profiled surface configured to ensure an oil flow during operation. According to the invention, the surface includes a more hydrophobic and/or lipophobic coating than the surface or a surface texturing rendering the surface more hydrophobic and/or lipophobic