Post-Shutdown Combustor Ventilation to Prevent Fuel Nozzle Coking

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Solution Overview

Problem

During gas turbine engine shutdown, residual heat causes temperature increases leading to carbon deposits (coking) in fuel nozzles and other components, which can result in engine start issues, inefficient combustion, and component distress.

Innovation Solution

A suction enabled post shutdown combustor cooling and ventilation system that draws in air from the core flow path and promotes airflow through the combustor to dump hot air to an open environment, using pumps and valves to manage airflow during shutdown conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If the engine is shutdown, then fuel consumption is reduced, but residual heat causes temperature increases leading to carbon deposits (coking) in fuel nozzles and other components

Engineering Contradiction:
Improvefuel consumptionVSAvoidcarbon deposits (coking)
Core Design Contradiction:
Loss of energyVSObject-affected harmful factors

Solution Approach 1:

The system uses the residual heat and airflow that would otherwise be wasted after engine shutdown to create a beneficial cooling effect. By activating the pump and opening the suction valve, ambient air is drawn through the fuel nozzle area, utilizing the existing thermal energy gradient to prevent coking without requiring additional fuel consumption.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

Solution Approach 2:

The pump and valve system is activated immediately upon engine shutdown to prevent coking before it can occur. The suction valve opens in advance to allow cooling airflow to reach the fuel nozzles and other vulnerable components, addressing the thermal problem before carbon deposits have time to form.

Inventive Principle:
Principle #10Preliminary action

2Temperature

If cooling systems operate continuously, then component temperatures are maintained within allowable limits, but system complexity and energy consumption increase

Engineering Contradiction:
Improvecomponent temperature controlVSAvoidcooling system complexity
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The cooling system transitions from a static, continuously operating design to a dynamic, on-demand system. The pump and suction valve are activated only when needed (during shutdown conditions), allowing the system to adapt its operation to actual thermal requirements and reduce overall complexity.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system uses the engine's own residual heat and airflow patterns to drive the cooling process after shutdown. By leveraging the natural thermal gradient and using the pump to draw ambient air through the fuel system, the design eliminates the need for external cooling infrastructure.

Inventive Principle:
Principle #25Self-service

3Object-affected harmful factors

If a suction system is activated post shutdown, then coking risk is reduced, but additional components (pump, valve) and energy consumption are required

Engineering Contradiction:
Improvecoking riskVSAvoidsystem components
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

The suction valve acts as an intermediary component that controls airflow to the fuel nozzles. By positioning the valve in the suction line, the system can precisely regulate when and how cooling air reaches vulnerable components, providing targeted protection without requiring complex cooling infrastructure throughout the entire fuel system.

Inventive Principle:
Principle #24Intermediary (Mediator)

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

Reduces the risk of coking in fuel nozzles and other components, preventing costly failures and ensuring efficient engine operation upon restart.

Implementation Method 1

a pump fluidly coupled with a suction line, wherein the suction line is fluidly coupled with suction ports proximate a fuel system component near a combustor

Methodology Applied
Scientific EffectSuction: Suction

Implementation Method 2

temperatures of gas turbine engine components are maintained within allowable limits by a plurality of cooling processes that transfer heat from the components to one or more heat sinks

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 3

residual heat in certain engine components can be transferred (i.e.; 'soakback') from the bore area, gas path, and cases and subsequently increase the temperature of other engine components beyond allowable limits

Methodology Applied
Scientific EffectHeat transfer: Heat Exchanger

Data Source

PatentEP4707560A1Suction enabled post shutdown combustor cooling and core ventilation
Publication Date: 2026.03.11 RTX CORP
  • EP4707560A1 patent drawingFigure 1
  • EP4707560A1 patent drawingFigure 2
  • EP4707560A1 patent drawingFigure 3

AI summary

A suction enabled post shutdown combustor cooling and ventilation system including a pump fluidly coupled with a suction line, wherein the suction line is fluidly coupled with suction ports proximate a compressor; a pump suction valve positioned in the suction line upstream of the pump; a pump discharge line fluidly coupled with the pump, an outlet fluidly coupled with the pump discharge line; and an engine core flow path fluidly coupled with the suction ports.