Radiant Wall Burner Tip Uniform Flow Design

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Solution Overview

Problem

Current radiant wall burner tips experience flashback due to non-uniform fuel and air mixture flow, leading to thermal damage and reduced burning capacity, as existing designs create turbulence and varying velocities that can result in reverse flow and ignition within the burner tip.

Innovation Solution

The design features a burner tip with a concave discoidal upper and lower leaf forming a constant flow area from the mixing chamber to the exit, ensuring a uniform velocity of the fuel and air mixture, optionally with a secondary fuel tip and a screen of round openings to maintain uniform flow and minimize turbulence.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Quantity of substance

If slotted discharge openings are used to increase burning capacity, then the area for fuel and air emission is increased, but the velocity of the mixture decreases and reverse flow occurs leading to flashback

Engineering Contradiction:
Improveburning capacityVSAvoidmixture velocity
Core Design Contradiction:
Quantity of substanceVSSpeed

Solution Approach 1:

The patent changes the geometric parameters of the discharge openings from narrow slots to circular openings with specific diameter ratios (0.5-2.0 times the mixing chamber diameter). This parameter change allows increasing the total discharge area for higher burning capacity while maintaining sufficient exit velocity to prevent flashback, as circular openings provide more uniform flow distribution compared to slots.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent introduces a multi-dimensional approach by using multiple circular discharge openings arranged in different planes and orientations around the mixing chamber. This spatial arrangement allows the mixture to exit in multiple directions simultaneously, increasing the effective burning area while maintaining velocity through the three-dimensional flow paths.

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

2Stability of the object's composition

If multiple discharge openings are used to distribute fuel and air radially, then uniform distribution is achieved, but turbulence is created causing non-uniform flow and varying velocities

Engineering Contradiction:
Improveflow uniformityVSAvoidturbulence
Core Design Contradiction:
Stability of the object's compositionVSObject-generated harmful factors

Solution Approach 1:

The patent applies local quality by designing each discharge opening with specific local characteristics (circular shape, specific diameter, specific orientation) that are optimized for its position. Each opening creates a localized laminar flow pattern that, when combined with other openings, produces an overall uniform flow distribution without excessive turbulence. The concave inner surface of the mixing chamber also provides local flow conditioning.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent uses curved surfaces throughout the design - the mixing chamber has a concave inner surface, and the discharge openings are circular rather than linear. These curved geometries promote smooth, laminar flow patterns and reduce flow separation and turbulence compared to sharp-edged or linear configurations. The spherical/circular geometry naturally guides flow in smooth arcs.

Inventive Principle:
Principle #14Spheroidality (Curvature)

3Reliability

If the discharge velocity is increased to prevent flashback, then flame propagation is prevented, but the burning capacity is reduced

Engineering Contradiction:
Improveflashback preventionVSAvoidburning capacity
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent segments the single discharge function into multiple separate circular openings distributed around the mixing chamber. Each opening maintains sufficient velocity for flashback prevention, while the collective output of all segments achieves the required total burning capacity. This segmentation allows velocity to be maintained in each individual stream while increasing overall throughput.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The mixing chamber design serves multiple functions simultaneously: it mixes fuel and air, conditions the flow, directs it through multiple discharge openings, and prevents flashback. The concave geometry and specific dimensional ratios allow the same structure to achieve both high velocity (for safety) and high flow capacity (for productivity) without requiring separate systems.

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

4Temperature

If thermal stress is applied to the burner tip during operation, then the burner operates at high temperature, but the tip cracks or separates from the mixer

Engineering Contradiction:
Improveoperating temperatureVSAvoidtip integrity
Core Design Contradiction:
TemperatureVSStrength

Solution Approach 1:

The patent designs the burner tip and mixing chamber with built-in thermal management features before thermal damage can occur. The specific dimensional ratios and flow patterns are designed to distribute thermal loads evenly, preventing hot spots that would cause thermal stress concentration. The geometry itself acts as a preventive measure against thermal damage.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

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 reduces the likelihood of flashback, maximizes the outward flow of fuel and air, and increases burning capacity by maintaining uniform velocity and thorough mixing, thereby preventing thermal damage and enhancing burner performance.

Implementation Method 1

an improved, aerodynamic burner tip which provides a uniform flow area from discharge from the mixing chamber up to the exit ports of the burner tip allowing for an outward flowing fuel gas and air velocity substantially uniform as the gas exits the burner tip

Methodology Applied
Scientific EffectAerodynamic flow:

Implementation Method 2

The primary fuel gas and the combustion air combine in the mixing chamber

Methodology Applied
Scientific EffectDiffusion: Diffusion

Implementation Method 3

The mixture flows in the direction from the upstream portion of the mixing chamber to the downstream portion of the mixing chamber along the axis

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 4

Radiant wall, premix fuel gas burners used in furnaces provide high heat release

Methodology Applied
Scientific EffectCombustion: Combustion

Data Source

PatentEP2909533B1Radiant wall burner apparatus with improved aerodynamic tip
Publication Date: 2020.09.02 HONEYWELL INTERNATIONAL INC
  • EP2909533B1 patent drawingFigure 1
  • EP2909533B1 patent drawingFigure 2~3
  • EP2909533B1 patent drawingFigure 4~5

AI summary

A radiant wall burner apparatus. The apparatus includes an inlet and primary fuel tip for introduction of fuel gas and air mixing in a mixing chamber. The fuel and air mixture are subject to a substantially uniform flow area from the point of discharge from a downstream portion of the mixing chamber up to the exit gap of the burner tip. The fuel gas and combustion air mixture terminate through the burner tip at a substantially uniform velocity. The radiant wall burner apparatus and burner tip allow for the substantially uniform velocity of the fuel gas and air mixture, reducing the potential for flashback of the burner tip.