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In the stage of design of the burner, factors such as fuel characteristics, furnace type, geographical environment, and user specific needs are comprehensively considered. Combustion aerodynamics and related principles are applied to design, and improvements and corrections are made through simulation results, ultimately achieving the following perfect results:
- Uniform mixing of burner fuel and air
During fuel combustion, the axial and radial air flow formed at the outlet of the burner is maximally diffused between the boundary layers through high-power strong injection. According to the user's required data, a low-level mixing model is used to achieve very uniform mixing of fuel and air.
- Advanced flame stabilization technology for burners
The burner uses a double vortex flame stabilizer designed through simulation and a variable angle backflow blade to generate strong hot gas backflow to maintain a narrow flame front chamber and achieve flame stability.
By using CFD aerodynamic simulation technology, calculate the flame length and diameter suitable for the corresponding model of furnace to ensure the correct flame shape, and adjust the gas flow rate and injection direction through separate gas and air guns to be most ideally suitable for the combustion chamber structure, so as to achieve the best combustion effect and achieve the lowest NOx emissions.
Selection data of integrated gas burner
Burner Model No.
1 2 3 4
WHAJ NGT 30-500 1/2/C
(1) Company Code
(2) Integrated series
(3) Heating capacity 104Kcal specification
(4) Single stage / Double stage/ Proportional adjustment type
