Asymmetric Burner Lance Positioning for Uniform Combustion

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing burner assemblies in industrial furnaces experience non-uniform temperature profiles, leading to thermal stress and increased NOx emissions due to hot-spots, which result in inconsistent product quality, particularly in pellet induration processes.

Innovation Solution

The burner lance is repositioned to have a smaller distance to the combustion chamber centerline, with a specific velocity ratio and inclination, inducing flame deflection and recirculation, which modifies the gas flow and temperature distribution, reducing temperature gradients and NOx formation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If the burner lance is positioned at the centerline of the combustion chamber, then the combustion process is stable and easy to control, but a non-uniform temperature profile is created with hot-spots leading to thermal stress and increased NOx emissions

Engineering Contradiction:
Improvetemperature uniformityVSAvoidNOx emissions and thermal stress
Core Design Contradiction:
TemperatureVSObject-generated harmful factors

Solution Approach 1:

The burner lance is deliberately positioned asymmetrically relative to the combustion chamber centerline, specifically at a distance of 0.05D to 0.15D from the centerline. This asymmetric positioning creates a more uniform temperature distribution by preventing the formation of concentrated hot-spots that occur with centered positioning, thereby reducing thermal stress on chamber walls and decreasing NOx emissions from localized high-temperature zones

Inventive Principle:
Principle #4Asymmetry

2Object-generated harmful factors

If the burner lance is repositioned to achieve more uniform temperature distribution, then thermal stress and NOx emissions are reduced, but the combustion configuration becomes more complex

Engineering Contradiction:
Improvethermal stress and NOx emissionsVSAvoidburner configuration complexity
Core Design Contradiction:
Object-generated harmful factorsVSDevice complexity

Solution Approach 1:

The invention achieves uniform temperature distribution by changing the positional parameter of the burner lace from the centerline to a specific offset distance (0.05D to 0.15D from centerline). This simple parameter modification, rather than redesigning the entire burner system, reduces thermal stress and NOx emissions while maintaining relatively simple device configuration

Inventive Principle:
Principle #35Parameter changes

3Device complexity

If secondary oxidant is introduced via a vertical downcomer, then the combustion chamber structure is simple, but large temperature gradients are created across the furnace width

Engineering Contradiction:
Improvecombustion chamber structureVSAvoidtemperature gradient
Core Design Contradiction:
Device complexityVSTemperature

Solution Approach 1:

The burner lance is positioned asymmetrically at 0.05D to 0.15D from the centerline, which modifies the interaction between the fuel-oxidant mixture and the secondary oxidant from the vertical downcomer. This asymmetric configuration promotes better mixing and reduces the large temperature gradients that would otherwise occur across the furnace width, achieving more uniform temperature distribution while maintaining simple structural design

Inventive Principle:
Principle #4Asymmetry

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 configuration achieves a more uniform temperature profile across the furnace, reducing thermal stress and NOx emissions, and enhances pellet quality by creating a swirl effect that improves mixing and temperature homogeneity.

Implementation Method 1

combustion of gaseous or liquid fuel in a combustion chamber which can have a cylindrical shape with a sectional diameter D whereby gaseous or liquid fuel as well as primary oxidant with a mean velocity of u1 is introduced via a burner lance (including a nozzle head) into the combustion chamber

Methodology Applied
Scientific EffectCombustion: Combustion

Implementation Method 2

The burner lance is repositioned to have a smaller distance to the combustion chamber centerline, with a specific velocity ratio and inclination, inducing flame deflection and recirculation, which modifies the gas flow and temperature distribution

Methodology Applied
Scientific EffectRecirculation:

Implementation Method 3

enhances pellet quality by creating a swirl effect that improves mixing and temperature homogeneity

Methodology Applied
Scientific EffectSwirl effect: Vortex Ring

Implementation Method 4

a non-uniform temperature profile leads to thermal stress on the wall of the combustion chamber

Methodology Applied
Scientific EffectThermal stress:

Implementation Method 5

hot-spots in the flame will increase the formation of NOx

Methodology Applied
Scientific EffectNOx formation:

Data Source

PatentUS11428404B2Method and apparatus for combustion of gaseous or liquid fuel
Publication Date: 2022.08.30 METSO OUTOTEC FINLAND OY
  • US11428404B2 patent drawing
  • US11428404B2 patent drawing
  • US11428404B2 patent drawing

AI summary

A method and apparatus for combustion of fuel in a combustion chamber with a hydraulic diameter D. Fuel and a primary oxidant are introduced via a burner lance into the combustion chamber, having a certain mean velocity u1 at entry, and a secondary oxidant with a mean velocity of u2 is introduced into the combustion chamber. The burner lance has a position p that has a distance Id1I defined as the smallest distance between p and a combustion chamber centerline.