A pre-ignition pulse burner
A pulsating combustion and pre-combustion technology, used in gas fuel burners, burners, combustion methods, etc., can solve the problems of uneven temperature distribution, high nitrogen oxide emissions, insufficient combustion, etc., to overcome uneven temperature distribution. , The effect of small exhaust heat loss and sufficient combustion
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Embodiment 1
[0029] In this embodiment, it is composed of nozzle 1, pre-chamber 2 and tailpipe 3; pre-chamber 2 is a conical body, and the front end of pre-chamber 2 washes out 8 grooves 4 with b=0° (see figure 2 , 8, 9); b represents the inclination angle of the groove 4, when b=0°, the groove 4 is a straight groove; the nozzle 1 penetrates directly into the pre-chamber 2; The ends are connected, and the end of the tailpipe 3 is directly connected to the furnace.
[0030] The working principle of this embodiment is as follows (the fuel used in the implementation of this embodiment is solid or gaseous fuel):
[0031] In the initial stage, the fuel supply device passes N 2 The fuel is sprayed into the pre-chamber 2 through the nozzle 1, and at the same time, due to the turbulent diffusion of the jet, the entrained hot air enters the pre-chamber 2 through the groove 4, and the two interact in the pre-chamber 2. Mixing, because the temperature of the hot air is enough to reach the ignition...
Embodiment 2
[0033] In this embodiment, it is composed of nozzle 1, pre-chamber 2 and tailpipe 3; pre-chamber 2 is a conical body, and the front end of pre-chamber 2 washes out 8 grooves 4 with b=30° (see image 3 , 8, 10, 11), the slots 4 are evenly distributed in right-handed or left-handed directions; the nozzle 1 penetrates directly into the pre-chamber 2; the front end of the tail pipe 3 is connected into the hearth.
[0034] The working principle of this embodiment is as follows (the fuel used in the implementation of this embodiment is solid or gaseous fuel):
[0035] In the initial stage, the fuel supply device passes N 2The fuel is sprayed into the pre-chamber 2 through the nozzle 1, and at the same time, due to the turbulent diffusion of the jet, the entrained hot air enters the pre-chamber 2 through the groove 4, and the two interact in the pre-chamber 2. Mixing, because the temperature of the hot air is enough to reach the ignition point of the fuel, so that the two can be mi...
Embodiment 3
[0037] In this embodiment, it is composed of nozzle 1, pre-chamber 2 and tailpipe 3; pre-chamber 2 is a conical body, and the front end of pre-chamber 2 washes out 8 grooves 4 with b=70° (refer to b=30° ), the grooves 4 are evenly distributed right-handed or left-handed; the nozzle 1 penetrates directly into the pre-combustion chamber 2; the front end of the tail pipe 3 is connected to the rear end of the pre-chamber 2, and the end of the tail pipe 3 is directly connected to the furnace.
[0038] The working principle of this embodiment is as follows (the fuel used in the implementation of this embodiment is solid or gaseous fuel):
[0039] In the initial stage, the fuel supply device passes N 2 The fuel is sprayed into the pre-chamber 2 through the nozzle 1, and at the same time, due to the turbulent diffusion of the jet, the entrained hot air enters the pre-chamber 2 through the groove 4, and the two interact in the pre-chamber 2. Mixing, because the temperature of the hot ...
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