Fuel combustion system with a perforated reaction holder
A stabilizer and reaction technology, applied to gas fuel burners, burning with multiple fuels, burners, etc., can solve problems such as long residence time, uneven heating of steam pipes, etc.
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[0157] Figure 12 is a schematic diagram of an experimental setup 1200 used to determine the effect of dilution distance between a fuel nozzle and a perforated reaction stabilizer, according to one embodiment. In the experimental setup, the test ignition was carried out under the following conditions:
[0158] The fuel is methane.
[0159] Fuel pressure varies but is always around 12 psi.
[0160] The fuel nozzle (pinhole) diameter is 0.11".
[0161] The airlock in the exhaust stack was always "closed" with about 1 / 4" of clearance around the airlock. The stack size was about 12" square. The 1 / 4" gap allows the exhaust flue damper to never fully close.
[0162] The air source (inlet air) was natural draft and confined in a 3" hole positioned concentrically with the fuel nozzle tube occupying 1 / 4" around the center of the 3" hole.
[0163] 3% O in the stack 2 for NOx comparison.
[0164] The perforated reaction stabilizer had a total thickness of 4" (L dimension). The 4" ...
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