Reduction Gear Oil Distributor With Separate Supply and Recovery

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Solution Overview

Problem

Existing mechanical reduction gears in turbomachines, particularly in aircraft turbomachines, face inefficiencies in lubricating oil supply and recovery, leading to potential overheating and reduced performance due to the mixing of hot and cold oil, which can cause stirring or churning, especially in planetary type operations.

Innovation Solution

A lubricating oil distributor with independent oil circuits for supply and recovery, featuring annular chambers and strategically located inlets and outlets, prevents oil mixing by separating oil supply and recovery functions, allowing for efficient discharge of heated oil and maintaining lower operating temperatures.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a single oil circuit is used for both supply and recovery in reduction gears, then the device complexity is reduced, but the temperature control deteriorates due to mixing of hot and cold oil causing stirring or churning

Engineering Contradiction:
Improveoil circuit structureVSAvoidoperating temperature
Core Design Contradiction:
Device complexityVSTemperature

Solution Approach 1:

The patent divides the oil circuit into two independent circuits: a supply circuit and a recovery circuit. The supply circuit delivers cold oil to the reduction gear, while the recovery circuit collects hot oil from the reduction gear. This segmentation prevents mixing of hot and cold oil, eliminating stirring or churning effects and improving temperature control.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent extracts the recovery function from the supply circuit by providing a separate recovery circuit. The recovery circuit includes recovery outlets positioned to collect oil after it has performed its lubrication function, separating the oil recovery process from the oil supply process to prevent thermal mixing.

Inventive Principle:
Principle #2Taking out (Extraction)

2Temperature

If independent oil supply and recovery circuits are implemented, then temperature control is improved, but the device complexity increases

Engineering Contradiction:
Improveoperating temperatureVSAvoidoil circuit structure
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The distributor body serves multiple functions: it acts as both a supply distributor and a recovery collector. The same distributor structure provides both supply outlets for cold oil and recovery outlets for hot oil, reducing the need for separate components and minimizing overall device complexity despite the dual-circuit requirement.

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

Solution Approach 2:

The patent merges the supply and recovery circuits within a single distributor body structure. Both circuits share common components such as the distributor body, seals, and mounting arrangements, which reduces the overall complexity compared to having completely separate systems.

Inventive Principle:
Principle #5Merging (Combining)

3Device complexity

If oil recovery outlets are positioned near supply outlets, then the distributor structure is simplified, but oil mixing occurs reducing lubrication efficiency

Engineering Contradiction:
Improvedistributor structureVSAvoidlubrication efficiency
Core Design Contradiction:
Device complexityVSProductivity

Solution Approach 1:

The distributor is designed with different local characteristics for supply and recovery functions. Supply outlets are positioned in regions where cold oil should be delivered, while recovery outlets are positioned in regions where hot oil naturally accumulates after lubrication. This local differentiation prevents mixing while maintaining structural integration.

Inventive Principle:
Principle #3Local quality

Data Source

PatentUS11635028B2Supply and recovery of lubricating oil in a mechanical reduction gear of an aircraft turbomachine
Publication Date: 2023.04.25 SAFRAN TRANSMISSION SYST
  • US11635028B2 patent drawing
  • US11635028B2 patent drawing
  • US11635028B2 patent drawing

AI summary

A lubricating oil distributor for a mechanical reduction gear of a turbomachine, in particular of an aircraft, includes a body of generally annular shape around an axis X and includes first and second independent oil circuits. The first oil circuit has a first oil inlet connected by a first chamber to several oil outlets distributed on the body around the axis X. The second oil circuit has a second oil inlet connected by a second chamber to several oil outlets distributed on the body around the axis X. The first and second chambers extend circumferentially around the axis X at different diameters, wherein the first and second oil circuits are formed in the body and are respectively a recovery circuit and an oil supply circuit for toothing of the reduction gear.