Variable Fuel Injector Manifold for Cold-Start Atomization

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Solution Overview

Problem

Current fuel injector manifolds in turbine engines provide a fixed fuel flow, which results in low delta pressure during engine startup and cold conditions, leading to difficulty in atomizing fuel and air mixture, especially with high viscosity fuels, making ignition challenging.

Innovation Solution

A variable fuel flow system with pistons and actuation mechanisms that adjust the orifice area of fuel injectors, creating a higher delta pressure for improved atomization and mixing of fuel and air, using passive or active actuation mechanisms to move pistons within the fuel manifold ring.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a fixed fuel flow system is used, then the structure is simple, but the delta pressure is low during engine startup and cold conditions, making fuel atomization difficult

Engineering Contradiction:
Improvefuel flow system structureVSAvoiddelta pressure
Core Design Contradiction:
Device complexityVSStress or pressure

Solution Approach 1:

The patent applies dynamics by replacing the fixed fuel flow system with a variable fuel flow system that can adapt to different operating conditions. The variable orifice area allows the system to dynamically adjust fuel flow characteristics, creating higher delta pressure during startup and cold conditions while maintaining simplicity through integrated piston mechanisms within the fuel manifold ring.

Inventive Principle:
Principle #15Dynamics

2Stress or pressure

If a variable fuel flow system with pistons is used, then the delta pressure is high for improved atomization, but the device complexity increases

Engineering Contradiction:
Improvedelta pressureVSAvoidfuel flow system structure
Core Design Contradiction:
Stress or pressureVSDevice complexity

Solution Approach 1:

The patent merges the piston mechanisms directly into the fuel manifold ring structure, combining multiple functions into a single integrated component. This reduces overall device complexity by eliminating separate piston housings and mounting structures, while still achieving the variable orifice area needed for high delta pressure and improved fuel atomization.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The fuel manifold ring serves multiple functions: it distributes fuel to injectors, houses piston mechanisms for flow control, and acts as a structural mounting component. This multi-functionality reduces the need for separate components, thereby reducing device complexity while maintaining the variable fuel flow capability for high delta pressure.

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

3Ease of manufacture

If a fixed orifice area is used, then the manufacturing is simple, but the fuel atomization is poor with high viscosity fuels

Engineering Contradiction:
Improveorifice manufacturingVSAvoidfuel atomization quality
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The patent implements dynamic orifice area adjustment through piston displacement, allowing the system to optimize fuel atomization for different fuel viscosities and operating conditions. During startup and cold conditions, the variable orifice creates higher delta pressure that improves atomization of high viscosity fuels, while the manufacturing remains relatively simple using standard piston and orifice fabrication methods.

Inventive Principle:
Principle #15Dynamics

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

Enhances atomization and ignition capability, improving sub-idle efficiency and reducing smoke generation, especially with cold fuels or high viscosity fuels, by maintaining high delta pressure across fuel injectors.

Implementation Method 1

creating a higher delta pressure for improved atomization and mixing of fuel and air

Methodology Applied
Scientific EffectPressure differential (delta pressure): Pressure Gradient

Implementation Method 2

improved atomization and mixing of fuel and air

Methodology Applied
Scientific EffectAtomization: Aerosol

Data Source

PatentUS20250354520A1Fuel injector manifold for a turbine engine
Publication Date: 2025.11.20 GENERAL ELECTRIC CO
  • US20250354520A1 patent drawing
  • US20250354520A1 patent drawing
  • US20250354520A1 patent drawing

AI summary

A fuel injector manifold for a turbine engine includes a fuel manifold ring, a plurality of fuel injectors, and a variable fuel flow system. The fuel manifold flowpath within the fuel manifold ring, the fuel manifold flowpath receiving fuel therein. The plurality of fuel injectors in fluid communication with the fuel manifold flowpath, each of the plurality of fuel injectors having one or more fuel injector flowpaths. The variable fuel flow system disposed within the fuel manifold flowpath, the variable fuel flow system including a closed state, a partially opened state, and a fully opened state to vary a flow of the fuel from the fuel manifold flowpath to the one or more fuel injector flowpaths of each of the plurality of fuel injectors.