Aircraft Turbomachine Oil Gutter Deflector for Radial Evacuation

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Solution Overview

Problem

Existing aircraft turbomachine sun gear reducers face challenges in efficiently evacuating and recovering lubricating oil, leading to premature wear, heat exchange issues, and increased oil consumption due to inefficient oil circulation and retention.

Innovation Solution

A lubrication oil piping gutter with a deflector-shaped annular bottom wall that facilitates radial oil flow from the inside to the outside, preventing oil accumulation and enhancing evacuation, combined with lateral edges for stiffness and improved oil recovery.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a simple circular gutter is used to collect oil, then the device complexity is reduced, but oil accumulation occurs and evacuation efficiency deteriorates

Engineering Contradiction:
Improvegutter structureVSAvoidoil evacuation efficiency
Core Design Contradiction:
Device complexityVSProductivity

Solution Approach 1:

The gutter is segmented into functional zones using a deflector element that divides the oil flow path. The deflector creates distinct regions for oil collection, deflection, and evacuation, allowing each zone to perform its specific function optimally without requiring complete structural redesign

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The deflector acts as an intermediary element between the oil collection area and the evacuation opening. It mediates the oil flow by redirecting it toward the opening, ensuring efficient evacuation without requiring complex pumping or forcing mechanisms

Inventive Principle:
Principle #24Intermediary (Mediator)

2Volume of stationary object

If the gutter size is reduced to minimize tank size, then the volume of the stationary object is reduced, but oil recovery efficiency deteriorates

Engineering Contradiction:
Improvetank sizeVSAvoidoil recovery efficiency
Core Design Contradiction:
Volume of stationary objectVSProductivity

Solution Approach 1:

The deflector extracts and redirects the rotational oil film toward the evacuation opening, preventing oil from circulating uselessly around the gutter. This extraction of oil from the rotational flow ensures efficient recovery in a compact volume by directing oil flow purposefully toward the exit

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The deflector performs preliminary action by intercepting and redirecting the oil film before it can complete a full circulation around the gutter. This preliminary deflection ensures that oil is directed toward evacuation early in its rotational path, maximizing recovery efficiency in limited space

Inventive Principle:
Principle #10Preliminary action

3Ease of operation

If the gutter allows free oil circulation, then ease of operation is improved, but heat exchange and oil loss increase

Engineering Contradiction:
Improveoil circulationVSAvoidheat exchange
Core Design Contradiction:
Ease of operationVSLoss of energy

Solution Approach 1:

The deflector causes oil to skip or rush through the evacuation opening rather than allowing it to circulate slowly around the entire gutter. This rapid passage through the opening reduces the time oil spends in contact with the gutter walls, minimizing heat exchange and energy loss while maintaining operational simplicity

Inventive Principle:
Principle #21Skipping (Rushing through)

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 solution effectively enhances oil evacuation and recovery, reducing heat exchange and oil consumption, while minimizing the size of the oil tank and degassing circuit, thus addressing the inefficiencies in existing systems.

Implementation Method 1

The oil circulating in the reducer to lubricate the rolling elements and gear teeth is evacuated to the periphery by centrifugation

Methodology Applied
Scientific EffectCentrifugation: Centrifugal Force

Data Source

PatentUS11008942B2Lubricating oil piping gutter of an aircraft turbomachine
Publication Date: 2021.05.18 SAFRAN AIRCRAFT ENGINES SAS
  • US11008942B2 patent drawing
  • US11008942B2 patent drawing

AI summary

The present disclosure describes a lubrication oil piping gutter of an aircraft turbomachine. The lubrication oil piping gutter can be used for a sun gear train reducer of the turbomachine. The gutter may include two lateral annular walls connected at their outer periphery by an annular bottom wall. In some embodiments, the annular bottom wall may include at least one oil evacuation opening in which is located a deflector configured to facilitate the flow of oil radially from the inside to the outside of the gutter.