Oxygen Enrichment in Premix Burners via Circumferential Injection
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Solution Overview
Problem
Conventional premix burners face challenges in safely and efficiently enriching combustion with significant oxygen due to the risk of flame flashback and overheating of burner components, limiting oxygen enrichment to low levels.
Innovation Solution
A premix burner arrangement and method that introduces oxygen circumferentially around a central air-fuel gas stream at a lower velocity ratio, inhibiting mixing and maintaining a temperature difference of at least 1000°F to prevent overheating, allowing for higher oxygen enrichment while minimizing burner component damage.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Quantity of substance
If significant additional oxygen is added directly to the premix combustion mixture, then oxygen enrichment level is improved, but flame flashback risk increases
Solution Approach 1:
The oxygen injection system is segmented into multiple circumferential nozzles arranged around the central air-fuel stream, allowing distributed oxygen addition rather than concentrated injection. This segmentation prevents localized high oxygen concentrations that could trigger flashback while achieving overall enrichment.
Solution Approach 2:
Oxygen is injected with different properties (lower velocity, lower temperature) than the central air-fuel stream. The velocity ratio is controlled to be less than 1.0, creating a velocity differential that prevents oxygen from penetrating into the combustion zone and causing flashback.
2Productivity
If oxygen is premixed with fuel at high velocity, then combustion efficiency is improved, but flame speed increases causing flashback
Solution Approach 1:
The oxygen injection is extracted from the central premix stream and placed in a separate circumferential position. This prevents oxygen from directly premixing with fuel at high velocity while still allowing combustion to occur as the oxygen diffuses into the flame zone.
Solution Approach 2:
Instead of injecting oxygen into the center where fuel flows, the patent inverts the arrangement by flowing oxygen circumferentially around the central air-fuel stream. This reversal prevents direct high-velocity mixing that would increase flame speed.
3Quantity of substance
If high velocity oxygen is injected into the burner, then oxygen enrichment is improved, but burner component overheating increases
Solution Approach 1:
The oxygen stream parameters are changed to have lower velocity and lower temperature compared to the air-fuel stream. The velocity ratio is maintained below 1.0, and the temperature differential is kept at least 1000°F, preventing the oxygen stream from contributing to burner component overheating.
4Productivity
If oxygen velocity is increased to improve mixing, then enrichment efficiency is improved, but flashback risk increases
Solution Approach 1:
Different velocity qualities are assigned to different streams: the central air-fuel stream maintains high velocity for proper atomization and mixing, while the circumferential oxygen stream uses lower velocity to prevent flashback. This differential velocity approach enables enrichment without increasing flashback risk.
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
Enables safe and efficient oxygen enrichment of premix combustion, reducing the risk of flashback and overheating, thereby achieving higher oxygen levels without damaging burner components.
Implementation Method 1
The premix burner arrangement is configured to combust or react the first stream at a temperature at least 1000° F. greater than the temperature of the second stream
Implementation Method 2
The premix burner arrangement is further configured to provide a velocity ratio of the second gas stream to the first gas stream sufficiently low to inhibit mixing of the first gas stream with the second gas stream
Data Source
AI summary
A premix burner arrangement for safely oxygen-enriching a premix air-fuel combustion system is disclosed. In the disclosed burner arrangement, a first conduit is arranged and disposed to provide a first gas stream. The first gas stream is a self-reactive or self-flammable premixture comprising air and a combustible gas. At least one second conduit is arranged and disposed to provide a second gas stream circumferentially around the first gas stream. The second gas stream includes oxygen. The premix burner arrangement is configured to combust or react the first stream at a temperature at least 1000° F. greater than the temperature of the second stream. A method and combustion system including the premix burner arrangement are also disclosed.


