Technical Field
[0001] The present invention relates to technical field of gas burner, and more specifically
relates to a burner with linear arrays of fire holes.
Background Art
[0002] Nitrogen oxides (NO
x) include NO, NO
2, N
2O, N
2O
3, N
2O
4 and N
2O
5 etc. NO
x in flue gas are mainly NO and NO
2. NO is very toxic, and can be very easily combined with hemoglobin (Hb) in human
blood, causing blood hypoxia which in turns results in central nervous system paralysis.
Compared with CO, the affinity of NO with hemoglobin is about hundreds to thousands
times stronger. The pollution of NOx to the environment and its harm to the human
body are well known.
[0003] The nitrogen oxides produced in the combustion process of a gas burner are mainly
NO and NO
2, and the term nitrogen oxides NOx generally refer to these two kinds of nitrogen
oxides. Loads of experimental results show that the nitrogen oxides emitted by the
burner are mainly NO, accounting for about 95% on average, while NO
2 only accounts for about 5%. NO produced by general fuel combustion has two main sources:
the first one is the oxidation of nitrogen in combustion-supporting air during the
combustion process; and the second one is the re-oxidation of nitrides after being
thermally decomposed during the combustion process. The first one is a more dominating
source of NO among the described two sources, and the NO from this first source will
be herein referred to as "thermally reactive NO". The NO from the second source will
be referred to as "fuel NO". Apart from these two sources, there is a kind of "instantaneous
NO" which accounts for just a small amount.
[0004] In the combustion process of most burners, NOx are produced from gas during the combustion
process. Combustion methods and combustion conditions can significantly affect the
production of NOx. Therefore, the general state during combustion can be modified
to reduce the production of NOx. Specific ways of modification includes: low flame
combustion method, and increasing the combustion coefficient a1, etc.
[0005] A burner in the prior art has unreasonable structural designs for the flame ports
causing the combustion area to be too small. According to the principle of low-NOx
combustion and according to experiments, the main source of NOx in fuel gas is mainly
thermally reactive NOx. In order to reduce NOx emissions in fuel gas, the height of
the flame should be reduced as much as possible to lower the flame temperature, so
that NOx emissions during thermal reaction can be reduced.
[0006] Burner is a key component of the entire combustion equipment, bearing the responsibility
of stable combustion of the fuel and as complete as possible combustion of the fuel.
For this reason, in order to suppress the generation of NOx, to achieve low flame
combustion, and to increase the combustion coefficient a1, the structure of the burner
has to be contemplated.
Disclosure of the Invention
[0007] In view of the aforesaid disadvantages now in the prior art, the present invention
provides a burner with linear arrays of fire holes. The present invention uses a pattern
of 2:1 repeated longitudinal arrangement of flame ports along each combustion unit
and modifies the structures of the fuel gas channel and the gas regulation channel,
so as to increase the burning area of the fire holes, change the burning power at
the surfaces of the fire holes, and reduce the height of the burning flame at the
fire holes. By using the primary air inlet openings having elongated shapes and auxiliary
air inlet openings having circular shapes on the secondary air regulation panel, the
combustion coefficient a1 of the fuel is changed so that the flame is lowered and
hence reduces the emissions of NO
xduring thermal reaction. The present invention reduces the height of the burning flame
at the fire holes, reduces the temperature of the flame, and obviously reduces the
emissions of NO
xduring thermal reaction of the burner. Thus, the burner of the present invention has
the advantages of small load, reduced vibration and reduced noise during burning.
[0008] To fulfill the above objects of the present invention, the present invention provides
the following technical scheme:
A burner with linear arrays of fire holes, comprising at least one combustion unit,
a secondary air regulation panel and a fuel gas transmission unit;
the combustion unit is formed by punching and pressing panel boards; the combustion
unit is a chamber having a composite structure comprising flame ports, a gas regulation
channel and a fuel gas channel in communication with one another, wherein the flame
ports are disposed on an upper surface of the combustion unit, the gas regulation
channel is disposed below the flame ports, and the fuel gas channel is disposed below
the gas regulation channel; the fuel gas channel has a curved shape, and comprising
in sequential order a fuel gas inlet, a fuel gas mixing section and a fuel gas pressure
reduction section;
the secondary air regulation panel is formed by punching and pressing panel boards;
the secondary air regulation panel comprises a main flat surface; one side of the
main flat surface is provided with a distributor seat, and another side of the main
surface is provided with at least one combustion unit seat; primary air inlet openings
in elongated shapes and auxiliary air inlet openings in circular shapes are provided
on the main flat surface of the secondary air regulation panel;
the fuel gas transmission unit comprises a fuel gas pipe, a distributor and a plurality
of nozzles; the distributor has an elongated shape; one side of the distributor is
provided with a fuel gas pipe port, and another side of the distributor is sequentially
arranged with a plurality of nozzle seats; the fuel gas pipe is connected to the fuel
gas pipe port of the distributor; the nozzles are sequentially arranged on the nozzle
seats of the distributor respectively;
the fuel gas transmission unit is mounted on the distributor seat of the secondary
air regulation panel through the distributor; a plurality of combustion units are
provided, and a plurality of combustion unit seats are provided correspondingly; the
combustion units are sequentially arranged on the combustion unit seats of the secondary
air regulation panel respectively; also, the fuel gas inlets of the combustion units
correspond to the nozzles respectively.
[0009] The gas regulation channel of the combustion unit is a rhombus-shaped chamber formed
in the combustion unit where the rhombus-shaped chamber has a middle part wider than
two ends thereof along a longitudinal direction of the combustion unit.
[0010] The fuel gas inlet of the fuel gas channel has a reverse taper shape towards an opening
of the fuel gas inlet; the fuel gas inlet has a cross sectional shape of a circle
with two flat sides.
[0011] The fuel gas mixing section of the fuel gas channel is a tapered channel with a gradually
varying internal diameter along the tapered channel.
[0012] The fuel gas pressure reduction section of the fuel gas channel is a channel having
a channel cross section larger than a channel cross section of the fuel gas mixing
section.
[0013] The flame ports of the combustion unit are arranged longitudinally on the upper surface
of the combustion unit both in double rows and in single row, wherein the flame ports
arranged in double rows are main flame ports, and the flame ports arranged in a single
row are regulating flame ports; the main flame ports and the regulating flame ports
are arranged alternately where said double rows of main flame ports are interrupted
by one regulating flame port of said single row of regulating flame ports for every
arrangement of two main flame ports in each row.
[0014] The present invention uses a pattern of 2:1 repeated longitudinal arrangement of
flame ports along each combustion unit and modifies the structures of the fuel gas
channel and the gas regulation channel, so as to increase the burning area of the
fire holes, change the burning power at the surfaces of the fire holes, and reduce
the height of the burning flame at the fire holes. By using the primary air inlet
openings having elongated shapes and auxiliary air inlet openings having circular
shapes on the secondary air regulation panel, the combustion coefficient a1 of the
fuel is changed so that the flame is lowered and hence reduces the emissions of NO
xduring thermal reaction. The present invention reduces the height of the burning flame
at the fire holes, reduces the temperature of the flame, and obviously reduces the
emissions of NO
xduring thermal reaction of the burner. Thus, the burner of the present invention has
the advantages of small load, reduced vibration and reduced noise during burning.
Brief Description of Drawings
[0015]
FIG. 1 is a schematic structural view of the present invention.
FIG. 2 is a schematic structural view of the fuel gas transmission unit.
FIG. 3 is a schematic structural view of a combustion unit.
FIG. 4 is a schematic structural view of the combustion unit according to viewing
direction C as indicated in FIG. 3.
FIG. 5 is a schematic sectional view of FIG. 3 along line B-B.
FIG. 6 is a schematic illustration showing the present invention in operation.
Best Mode for Carrying out the Invention
[0016] With reference to FIG. 1 and FIG. 2, the present invention comprises at least one
combustion unit 1, a secondary air regulation panel 2 and a fuel gas transmission
unit 3.
[0017] With reference to FIG. 1 and FIG. 3, the combustion unit 1 is formed by punching
and pressing panel boards; the combustion unit 1 is a chamber having a composite structure
comprising flame ports 14, a gas regulation channel 15 and a fuel gas channel in communication
with one another, wherein the flame ports 14 are disposed on an upper surface of the
combustion unit 1, the gas regulation channel 15 is disposed below the flame ports
14, and the fuel gas channel is disposed below the gas regulation channel 15; the
fuel gas channel has a curved shape, and comprising in sequential order a fuel gas
inlet 11, a fuel gas mixing section 12 and a fuel gas pressure reduction section 13.
[0018] With reference to FIG. 1, the secondary air regulation panel 2 is formed by punching
and pressing panel boards; the secondary air regulation panel 2 comprises a main flat
surface; one side of the main flat surface is provided with a distributor seat, and
another side of the main surface is provided with at least one combustion unit seat;
primary air inlet openings 21 in elongated shapes and auxiliary air inlet openings
22 in circular shapes are provided on the main flat surface of the secondary air regulation
panel.
[0019] With reference to FIG. 1 and FIG. 2, the fuel gas transmission unit 3 comprises a
fuel gas pipe 31, a distributor 32 and a plurality of nozzles 33; the distributor
32 has an elongated shape; one side of the distributor 32 is provided with a fuel
gas pipe port, and another side of the distributor 32 is sequentially arranged with
a plurality of nozzle seats; the fuel gas pipe 31 is connected to the fuel gas pipe
port of the distributor 32; the nozzles 33 are sequentially arranged on the nozzle
seats of the distributor 32 respectively.
[0020] With reference to FIG. 1, FIG. 2 and FIG. 3, the fuel gas transmission unit 3 is
mounted on the distributor seat of the secondary air regulation panel 2 through the
distributor 32. A plurality of combustion units 1 are provided, and a plurality of
combustion unit seats are provided correspondingly; the combustion units 1 are sequentially
arranged on the combustion unit seats of the secondary air regulation panel 2 respectively;
also, the fuel gas inlets 11 of the combustion units 1 correspond to the nozzles 33
respectively.
[0021] With reference to FIG. 3 and FIG. 5, the gas regulation channel 15 of the combustion
unit is a rhombus-shaped chamber formed in the combustion unit where the rhombus-shaped
chamber has a middle part wider than two ends thereof along a longitudinal direction
of the combustion unit 1.
[0022] With reference to FIG. 3, the fuel gas inlet 11 of the fuel gas channel has a reverse
taper shape towards an opening of the fuel gas inlet; the fuel gas inlet 11 has a
cross sectional shape of a circle with two flat sides 111.
[0023] With reference to FIG. 3, the fuel gas mixing section 12 of the fuel gas channel
is a tapered channel with a gradually varying internal diameter along the tapered
channel.
[0024] With reference to FIG. 3, the fuel gas pressure reduction section 13 of the fuel
gas channel is a channel having a channel cross section larger than a channel cross
section of the fuel gas mixing section 12.
[0025] With reference to FIG. 3 and FIG. 4, the flame ports 14 of the combustion unit are
arranged longitudinally on the upper surface of the combustion unit 1 both in double
rows and in single row, wherein the flame ports arranged in double rows are main flame
ports 141, and the flame ports arranged in a single row are regulating flame ports
142; the main flame ports and the regulating flame ports are arranged alternately
where said double rows of main flame ports are interrupted by one regulating flame
port of said single row of regulating flame ports for every arrangement of two main
flame ports in each row.
[0026] The present invention is operated as follows:
With reference to FIG. 1, FIG. 2, FIG. 3 and FIG. 6, when fuel gas enters through
the fuel gas pipe 31 of the fuel gas transmission unit 3, the fuel gas will be distributed
to each of the nozzles 33 through the distributor 32, and then the fuel gas will then
be ejected by the nozzles 33 into the corresponding fuel gas inlets 11 of the corresponding
fuel gas channels of the combustion units 1. As the nozzles 33 eject the fuel gas,
the ejected stream of fuel gas will also drive first surrounding air into the combustion
unit as well and so the fuel gas and the first surrounding air will be mixed in the
fuel gas mixing section 12 to obtain a first mixed gas. The first mixed gas will then
pass through the fuel gas pressure reduction section 13 for pressure reduction so
as to reduce the burning power of the first mixed gas. Subsequently, the gas regulation
channel 15 (having said rhombus-shaped chamber formed in the combustion unit where
the rhombus-shaped chamber has a middle part wider than two ends thereof along a longitudinal
direction of the combustion unit) will balance and regulate the first mixed gas, while
second surrounding air flowing through the primary air inlet openings 21 and the auxiliary
air inlet openings 22 of the secondary air regulation panel 2 into the combustion
unit will be mixed again with the first mixed gas at the flame ports 14 to obtain
a second mixed gas. The second mixed gas is supplied for burning at the flame ports
14.
[0027] With reference to FIG. 1, FIG. 3 and FIG. 4, the flame ports 14 of the combustion
unit are arranged longitudinally on the upper surface of the combustion unit 1 both
in double rows and in single row, wherein the flame ports arranged in double rows
are main flame ports 141, and the flame ports arranged in a single row are regulating
flame ports 142; the main flame ports and the regulating flame ports are arranged
alternately where said double rows of main flame ports are interrupted by one regulating
flame port of said single row of regulating flame ports for every arrangement of two
main flame ports in each row, thereby achieving a pattern of 2:1 repeated longitudinal
arrangement of flame ports where arrangement of every two main flame ports in each
row will be followed by one regulating flame port of said single row of regulating
flame ports, and said one regulating flame port of said single row of regulating flame
ports will be followed by another two main flame ports arranged in each row, which
is then followed by another one regulating flame port of said single row of regulating
flame ports, and so and so forth. As such, the arrangement of flame ports 14 according
to the present invention can effectively enlarge the burning area of the fire holes.
[0028] With reference to FIG. 1, FIG. 3 and FIG. 6, the primary air inlet openings 21 and
the auxiliary air inlet openings 22 are provided on the secondary air regulation panel
2. To ensure even longitudinal distribution of the second mixed gas along each combustion
unit 1, a middle part of each combustion unit 1 has to be supplied with more second
surrounding air, and for this purpose, the primary air inlet openings 21 having elongated
shapes are provided on the secondary air regulating panel 2 corresponding to the middle
part of each combustion unit 1. The auxiliary air inlet openings 22 having circular
shapes are provided on the secondary air regulating panel 2 corresponding to two ends
of each combustion unit 1 to supply second surrounding air in an amount slightly less
than the second surrounding air supplied to the middle part of each combustion unit
1.The primary air inlet openings 21 and the auxiliary air inlet openings 22 can effectively
solve the problem of uneven longitudinal distribution of second mixed gas along the
flame ports 14 of each combustion unit 1 due to the prior art problem where lesser
second surrounding air is present at the middle part of each combustion unit 1 but
more abundant second surrounding air is present at two ends of each combustion unit
1. Accordingly, the second mixed gas can be more completely burnt, thus lowering the
height of the burning flame at the fire holes and lowering the temperature of the
flame. Also, emissions of NO
x during thermal reaction of the burner are obviously reduced.
[0029] With reference to FIG. 1 and FIG. 3, the fuel gas inlet 11 having a reverse taper
shape towards the opening thereof has a cross sectional shape of a circle with two
flat sides 111. The two flat sides 111 reduce the width of the fuel gas inlet 11 to
free some spaces which allow the plurality of combustion units 1 to be arranged more
tightly. Accordingly, the plurality of combustion units can be arranged in greater
density.
1. A burner with linear arrays of fire holes,
characterized in comprising at least one combustion unit (1), a secondary air regulation panel (2)
and a fuel gas transmission unit (3);
the combustion unit (1) is formed by punching and pressing panel boards; the combustion
unit (1) is a chamber having a composite structure comprising flame ports (14), a
gas regulation channel (15) and a fuel gas channel in communication with one another,
wherein the flame ports (14) are disposed on an upper surface of the combustion unit
(1), the gas regulation channel (15) is disposed below the flame ports (14), and the
fuel gas channel is disposed below the gas regulation channel (15); the fuel gas channel
has a curved shape, and comprising in sequential order a fuel gas inlet (11), a fuel
gas mixing section (12) and a fuel gas pressure reduction section (13);
the secondary air regulation panel (2) is formed by punching and pressing panel boards;
the secondary air regulation panel (2) comprises a main flat surface; one side of
the main flat surface is provided with a distributor seat, and another side of the
main surface is provided with at least one combustion unit seat; primary air inlet
openings (21) in elongated shapes and auxiliary air inlet openings (22) in circular
shapes are provided on the main flat surface of the secondary air regulation panel
(2);
the fuel gas transmission unit (3) comprises a fuel gas pipe (31), a distributor (32)
and a plurality of nozzles (33); the distributor (32) has an elongated shape; one
side of the distributor (32) is provided with a fuel gas pipe port, and another side
of the distributor (32) is sequentially arranged with a plurality of nozzle seats;
the fuel gas pipe (31) is connected to the fuel gas pipe port of the distributor (32);
the nozzles (33) are sequentially arranged on the nozzle seats of the distributor
(32) respectively;
the fuel gas transmission unit (3) is mounted on the distributor seat of the secondary
air regulation panel (2) through the distributor (32); a plurality of combustion units
(1) are provided, and a plurality of combustion unit seats are provided correspondingly;
the combustion units (1) are sequentially arranged on the combustion unit seats of
the secondary air regulation panel (2) respectively; also, the fuel gas inlets (11)
of the combustion units (1) correspond to the nozzles (33) respectively.
2. The burner of claim 1, wherein the gas regulation channel (15) of the combustion unit
(1) is a rhombus-shaped chamber formed in the combustion unit (1) where the rhombus-shaped
chamber has a middle part wider than two ends thereof along a longitudinal direction
of the combustion unit (1).
3. The burner of claim 1, wherein the fuel gas inlet (11) of the fuel gas channel has
a reverse taper shape towards an opening of the fuel gas inlet; the fuel gas inlet
(11) has a cross sectional shape of a circle with two flat sides (111).
4. The burner of claim 1, wherein the fuel gas mixing section (12) of the fuel gas channel
is a tapered channel with a gradually varying internal diameter along the tapered
channel.
5. The burner of claim 1, wherein the fuel gas pressure reduction section (13) of the
fuel gas channel is a channel having a channel cross section larger than a channel
cross section of the fuel gas mixing section (12).
6. The burner of claim 1, wherein the flame ports (14) of the combustion unit (1) are
arranged longitudinally on the upper surface of the combustion unit (1) both in double
rows and in single row, wherein the flame ports (14) arranged in double rows are main
flame ports (141), and the flame ports arranged in a single row are regulating flame
ports (142); the main flame ports (141) and the regulating flame ports (142) are arranged
alternately where said double rows of main flame ports are interrupted by one regulating
flame port of said single row of regulating flame ports for every arrangement of two
main flame ports in each row.