Annular Fuel Injector with Segmented Multi-Fuel Paths

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Solution Overview

Problem

Existing fuel injectors for turbine engines face challenges in efficiently mixing and delivering multiple fuels or fuel additives to achieve optimal combustion conditions, leading to inefficiencies and higher emissions.

Innovation Solution

A fuel injector with an annular design that incorporates multiple fuel and air supply paths, including central and outer passages with turbulators and separate fuel and air supply channels, allowing for the intermixing of up to three different fuels or fuel additives with controlled flow rates, enhancing combustion efficiency and reducing emissions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If multiple fuel supply paths are added to enable mixing of up to three different fuels or fuel additives, then fuel flexibility and combustion efficiency are improved, but device complexity increases

Engineering Contradiction:
Improvefuel flexibilityVSAvoiddevice complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The fuel injector is divided into multiple independent fuel supply paths (first fuel supply path, second fuel supply path, third fuel supply path), each capable of delivering different fuels or fuel additives. This segmentation allows flexible fuel combination while maintaining a structured, manageable design that doesn't excessively increase complexity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The fuel injector body is designed with multiple fuel supply paths that can accommodate different types of fuels and fuel additives, making the same device capable of operating with various fuel combinations depending on operational requirements, thus achieving multi-functionality.

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

2Productivity

If separate fuel and air supply channels with turbulators are incorporated, then mixing efficiency is improved, but manufacturing complexity increases

Engineering Contradiction:
Improvemixing efficiencyVSAvoidease of manufacture
Core Design Contradiction:
ProductivityVSEase of manufacture

Solution Approach 1:

Turbulators are strategically placed at specific locations within the fuel supply paths and mixing chambers to create localized turbulence that enhances mixing efficiency. This targeted approach improves mixing where needed without requiring complex modifications throughout the entire injector structure.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The fuel supply paths and air supply channels are merged into a unified mixing chamber where multiple fuels and air converge. This integration allows efficient mixing in a single location rather than requiring separate mixing zones, simplifying the manufacturing process.

Inventive Principle:
Principle #5Merging (Combining)

3Object-generated harmful factors

If an annular design with multiple passages is used, then combustion efficiency and emissions reduction are improved, but device complexity increases

Engineering Contradiction:
ImproveemissionsVSAvoiddevice complexity
Core Design Contradiction:
Object-generated harmful factorsVSDevice complexity

Solution Approach 1:

The fuel injector adopts an annular (ring-shaped) design with multiple concentric passages arranged in different dimensions. This dimensional arrangement allows multiple fuel supplies and air channels to coexist in a compact space, improving combustion efficiency and reducing emissions while maintaining a relatively simple overall structure.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The annular design features nested concentric passages where inner passages are surrounded by outer passages. This nesting arrangement allows multiple fuel supply paths and air channels to be integrated within each other, maximizing space utilization and reducing the overall device complexity.

Inventive Principle:
Principle #7Nested doll (Nesting)

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 annular fuel injector facilitates efficient combustion, reduces emissions, and allows for flexible fuel usage based on operational conditions, improving engine performance and manufacturability.

Implementation Method 1

The outer passage includes a turbulator

Methodology Applied
Scientific EffectTurbulence: Turbulence

Data Source

PatentUS20250327570A1Fuel injector for a turbine engine
Publication Date: 2025.10.23 GENERAL ELECTRIC CO
  • US20250327570A1 patent drawing
  • US20250327570A1 patent drawing
  • US20250327570A1 patent drawing

AI summary

A gas turbine engine includes a compressor section, combustion section, and turbine section is serial flow arrangement. A fuel injector supplies a mixture of fuel and air for combustion within the combustion section. A first annular structure defines a central passage and a longitudinal axis within the fuel injector. A second annular structure is spaced from and in annular arrangement about the first annular structure to define an outer passage in annular arrangement between the first annular structure and the second annular structure.