Gas Turbine Injector Shielding Air Flow for NOx Reduction

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Solution Overview

Problem

Existing distributed combustion systems face challenges in reducing NOx emissions due to high flame temperatures, which can be attributed to short residence times of reactants in the combustion stage, and inefficiencies in utilizing cooling air, leading to increased NOx production and reduced engine efficiency.

Innovation Solution

The implementation of injector assemblies that generate a shielding air flow to delay ignition of reactants, allowing for increased entrainment of combustion products and efficient reuse of cooling air to form a shielding flow, thereby reducing NOx emissions and enhancing mixing performance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-generated harmful factors

If distributed combustion system is used to reduce NOx emissions, then NOx emissions are reduced, but flame temperature becomes too high

Engineering Contradiction:
ImproveNOx emissionsVSAvoidflame temperature
Core Design Contradiction:
Object-generated harmful factorsVSTemperature

Solution Approach 1:

A shielding air flow is introduced as an intermediary substance between the fuel-air reactants and the combustion zone. This shielding air acts as a mediator that delays ignition and reduces flame temperature without requiring complex active control systems

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

Cooling air, which is inherently inert and non-combustible, is redirected to form a shielding flow around the reactants. This creates a localized inert environment that suppresses premature combustion and reduces flame temperature while maintaining the distributed combustion architecture

Inventive Principle:
Principle #39Inert atmosphere (Inert environment)

2Temperature

If cooling air is used for component cooling, then component temperature is controlled, but NOx emissions increase due to inefficiency

Engineering Contradiction:
Improvecomponent temperatureVSAvoidNOx emissions
Core Design Contradiction:
TemperatureVSObject-generated harmful factors

Solution Approach 1:

The cooling air serves dual functions: it cools the combustor components (original function) and forms a shielding flow to reduce flame temperature and NOx emissions (new function). This multi-functionality eliminates waste and improves overall system efficiency

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

Solution Approach 2:

Instead of discarding the cooling air after it passes through the combustor walls, the system recovers and redirects this air to form a shielding flow around the reactants, maximizing its utility and preventing NOx formation

Inventive Principle:
Principle #34Discarding and recovering

3Object-generated harmful factors

If residence time of reactants is reduced to reduce NOx, then NOx emissions are reduced, but mixing performance deteriorates

Engineering Contradiction:
ImproveNOx emissionsVSAvoidresidence time
Core Design Contradiction:
Object-generated harmful factorsVSDuration of action of moving object

Solution Approach 1:

The shielding air flow is established in advance before the reactants are introduced into the combustion zone. This preliminary action creates a protective environment that allows extended residence time for mixing while preventing premature ignition that would lead to high NOx emissions

Inventive Principle:
Principle #10Preliminary action

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 approach effectively reduces NOx emissions by lowering flame temperatures, increases the liftoff distance of the flame, and improves engine efficiency by reusing cooling air, achieving stable operation at high turbine inlet temperatures while maintaining low NOx levels and efficient combustion.

Implementation Method 1

delay ignition of reactants, allowing for increased entrainment of combustion products

Methodology Applied
Scientific EffectEntrainment: Entrainment

Implementation Method 2

efficient reuse of cooling air to form a shielding flow

Methodology Applied
Scientific EffectConvection: Convection

Data Source

PatentEP3479025B1Injector assemblies configured to form a shielding flow of air injected into a combustion stage in a gas turbine engine
Publication Date: 2021.11.03 SIEMENS ENERGY GLOBAL GMBH & CO KG
  • EP3479025B1 patent drawingFigure 1~2
  • EP3479025B1 patent drawingFigure 3~4
  • EP3479025B1 patent drawingFigure 5

AI summary

Injector assemblies (12) and ducting arrangement including such injector assemblies are provided. The injector assembly may include a reactant-guiding structure arranged to convey a flow of reactants (19) into the combustion stage and means for injecting (24, 25, 26) a flow of air into the combustion stage. The flow of air injected into the combustion stage may be arranged to condition interaction of the flow of reactants injected into the combustion stage with a crossflow of combustion products, as the flow of reactants is admitted into the combustion stage.