Turbine Engine Lubricant Bypass Control for Cruise Efficiency

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Solution Overview

Problem

Traditional lubricant systems in turbine engines supply unnecessarily high lubricant flow rates during moderate engine operations, such as cruise periods, leading to inefficiency and increased fuel consumption.

Innovation Solution

A lubricant system with a closed-loop control mechanism that includes a lubricant reservoir, supply line, scavenge line, bypass line, temperature sensors, and a controllable bypass valve, which adjusts lubricant flow based on real-time temperature readings from upstream and downstream of the lubricated component to optimize lubricant distribution.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional lubricant systems supply high lubricant flow rates continuously, then lubrication reliability is improved, but fuel consumption increases and system efficiency deteriorates

Engineering Contradiction:
Improvelubrication reliabilityVSAvoidfuel consumption
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

The lubricant system transitions from a static continuous flow configuration to a dynamic controlled flow system. The bypass valve is actuated by a sensor-controlled mechanism that adjusts the lubricant flow rate through the bypass line based on real-time temperature differential measurements between supply and scavenge lines, enabling the system to adapt lubrication levels to actual operating conditions

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system implements a closed-loop feedback control mechanism where temperature sensors monitor the temperature differential across the lubricated component, and this information feeds back to the bypass valve actuator. When the temperature differential indicates adequate lubrication, the system reduces bypass flow; when the differential exceeds thresholds, the system increases bypass flow to maintain optimal lubrication

Inventive Principle:
Principle #23Feedback

2Reliability

If high lubricant flow rates are supplied continuously, then lubrication effectiveness is improved, but system efficiency deteriorates due to unnecessary lubricant circulation

Engineering Contradiction:
Improvelubrication effectivenessVSAvoidsystem efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The system dynamically adjusts lubricant flow distribution between the main supply line and bypass line based on real-time temperature differential measurements, transitioning from static continuous flow to adaptive variable flow that matches actual lubrication需求的

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes the flow rate parameter of lubricant through the bypass valve based on temperature differential measurements. The controller modifies the bypass valve position to adjust flow rate, thereby changing system operation from fixed high flow to variable flow optimized for current lubrication needs

Inventive Principle:
Principle #35Parameter changes

3Use of energy by moving object

If lubricant flow is reduced during cruise periods, then fuel consumption decreases, but lubrication reliability may deteriorate

Engineering Contradiction:
Improvefuel consumptionVSAvoidlubrication reliability
Core Design Contradiction:
Use of energy by moving objectVSReliability

Solution Approach 1:

The feedback control mechanism continuously monitors temperature differential across the lubricated component and automatically adjusts bypass valve position to maintain adequate lubrication. This ensures that even when overall lubricant flow is reduced during cruise, the system responds to actual lubrication needs by modulating bypass flow to prevent reliability deterioration

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The lubricant system performs self-regulation through the sensor-actuator feedback loop that automatically adjusts bypass valve positioning based on temperature differential measurements, enabling the system to self-optimize lubrication levels without external intervention while maintaining reliability

Inventive Principle:
Principle #25Self-service

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 system reduces lubricant flow by up to 60% during cruise periods, improving gearbox efficiency, reducing engine fuel consumption, and enhancing overall engine performance and safety by maintaining a constant temperature differential.

Implementation Method 1

a first sensor providing a first output indicative of a first lubricant parameter in the supply line, a second sensor providing a second output indicative of a second lubricant parameter in the scavenge line

Methodology Applied
Scientific EffectTemperature sensing:

Implementation Method 2

a controllable bypass valve fluidly coupled to and controlling the flow of lubricant through the bypass line

Methodology Applied
Scientific EffectFluid flow control:

Implementation Method 3

The lubricant can also be utilized for heat exchange with the fuel supplying the engine

Methodology Applied
Scientific EffectHeat transfer: Convection

Data Source

PatentUS12258878B2Lubricant system
Publication Date: 2025.03.25 GE AVIO SRL
  • US12258878B2 patent drawing
  • US12258878B2 patent drawing
  • US12258878B2 patent drawing

AI summary

A lubricant system for supplying lubrication to a component in a turbine engine includes a lubricant reservoir, a supply line fluidly coupling the lubricant reservoir to the component in the turbine engine, a scavenge line fluidly coupling the component to the lubricant reservoir, and a bypass line fluidly coupling the supply line to the scavenge line and bypassing the component.