Syngas Combustor Flashback Prevention via Fuel Blending

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Solution Overview

Problem

Conventional premixed dry-low nitrogen oxide (NOx) combustion systems for gas turbines experience flashback when combusting syngas due to its low Modified Wobbe Index (MWI) and high fuel reactivity, leading to hardware damage, and existing solutions that avoid flashback, such as diffusion combustors with nitrogen injection, increase complexity and cost.

Innovation Solution

A method and apparatus that blend syngas with natural gas to create a fuel mixture with a higher MWI and lower reactivity, reducing the likelihood of flashback by slowing the characteristic chemical time of the fuel, thereby preventing damage and simplifying the combustion system.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If conventional premixed DLN combustion systems are used to combust syngas, then the system structure is simple, but flashback occurs due to low MWI and high fuel reactivity

Engineering Contradiction:
Improvecombustion system structureVSAvoidflashback resistance
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The patent changes the chemical composition parameters of the fuel by blending syngas with natural gas. This adjusts the MWI and characteristic chemical time parameters of the fuel mixture, slowing the reaction rate and preventing flashback while maintaining system simplicity

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent creates a composite fuel mixture by combining syngas and natural gas in specific proportions. This composite fuel has intermediate properties that balance the low MWI/high reactivity of syngas with the higher MWI/lower reactivity of natural gas, eliminating flashback without requiring complex system modifications

Inventive Principle:
Principle #40Composite materials

2Reliability

If diffusion combustors with nitrogen injection are used to avoid flashback, then flashback resistance is improved, but system complexity and cost increase

Engineering Contradiction:
Improveflashback resistanceVSAvoidcombustion system structure
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent extracts the nitrogen injection system and diluent injection mechanism from the combustion system. By using fuel blending instead of diluent injection, the system eliminates the need for separate nitrogen supply lines, compression equipment, and injection devices, significantly reducing complexity

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent uses natural gas as an intermediary substance to mediate between the combustion requirements and flashback prevention needs. The natural gas acts as a buffer that slows reaction kinetics without requiring additional system components for diluent injection

Inventive Principle:
Principle #24Intermediary (Mediator)

3Object-generated harmful factors

If steam injection systems are used to control NOx formation, then NOx emissions are reduced, but system complexity and cost increase due to water quality requirements

Engineering Contradiction:
ImproveNOx emissionsVSAvoidsteam system complexity
Core Design Contradiction:
Object-generated harmful factorsVSDevice complexity

Solution Approach 1:

The patent replaces the complex steam injection system with a simpler fuel blending approach. Instead of requiring expensive steam generation equipment and water treatment systems, the solution uses readily available natural gas as a permanent component of the fuel mixture, achieving NOx control without the infrastructure of a steam system

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

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 blended fuel mixture effectively reduces flashback occurrences, maintains NOx control without additional diluents, and decreases system complexity and cost by utilizing readily available natural gas, ensuring stable combustion and extended hardware lifespan.

Implementation Method 1

mixing the first and second gaseous fuels together to form a blended gaseous fuel

Methodology Applied
Scientific EffectMixing:

Implementation Method 2

a nozzle in flow communication with the combustion zone for injecting a blended gaseous fuel into the combustion zone

Methodology Applied
Scientific EffectInjection: Injector

Implementation Method 3

Combustion systems of at least some known gas turbine engines combust synthesis gas, or syngas, to create exhaust gases that drive a gas turbine

Methodology Applied
Scientific EffectCombustion: Combustion

Data Source

PatentUS9080513B2Method and apparatus for combusting syngas within a combustor
Publication Date: 2015.07.14 GE INFRASTRUCTURE TECH LLC
  • US9080513B2 patent drawing
  • US9080513B2 patent drawing
  • US9080513B2 patent drawing

AI summary

A method for operating a combustor is provided. The method includes supplying a predetermined amount of a first gaseous fuel to the combustor, wherein the first gaseous fuel has a first Modified Wobbe Index (MWI) and a first fuel reactivity, and supplying a predetermined amount of a second gaseous fuel to the combustor, wherein the second gaseous fuel has a second MWI that is lower than the first MWI and a second fuel reactivity that is higher than the first fuel reactivity. The method also includes mixing the first and second gaseous fuels together to form a blended gaseous fuel, and injecting the blended gaseous fuel into the combustor.