BACKGROUND OF THE INVENTION
Field of the Invention:
[0001] This invention relates to a radiant tube burner in which a nozzle of a gas burner
is coaxially placed in a combustion tube located in a radiant tube so that the burner
can be moved in the axial direction, fuel gas issuing from the gas burner undergoes
primary combustion by primary air supplied through the annular space between the gas
burner and the combustion tube and further undergoes secondary combustion by secondary
air supplied through the annular space between the combustion tube and the radiant
tube and, more particularly to a radiant tube burner used for heat treatment furnaces
or the like. The newly invented burner is capable of reducing the amount of NOx contained
in the exhaust gas discharged from the radiant tube.
Description of the Prior Art:
[0002] There has been a proposal in the design of radiant tube burners in which a damper
is provided at the inlet of the primary air admitted into the combustion tube, for
example, to restrain the generation of NOx, thereby making it possible to change the
primary and the secondary air ratio.. (See Japanese Utility Model Laid-open No. Sho
52-21036)
[0003] However, it has been found out that the amount of generated Nox cannot be sufficiently
reduced only by adjusting the primary and the secondary air ratio.
[0004] Further, there has been known another proposal in which a steam tube is provided
in the fuel gas nozzle to eject steam into the flame formed by burner combustion,
to make it possible to reduce the flame temperature to restrain the generation of
NOx (See Japanese Patent Laid-open No. Sho 52-29007).
[0005] When comparing the case of ejecting steam with that of atomizing water, the latter
is more effective in reducing the flame temperature, thus leading to higher reduction
of Nox. However, an adverse effect on the radiant tube and instability of the flame
may be expected due to the relatively large particle size of atomized water so that
the practical use has been considered to be impossible.
SUMMARY OF THE INVENTION
[0006] It is an object of the present invention to provide a radiant tube burner in which
high heat load primary combustion is caused to happen in satisfactory and stable way
by swirling the primary air and soft secondary combustion takes place in a radiant
tube, thereby making it possible to obtain low NOx.
[0007] In order to attain the first object, according to the present invention, a divergent
flame type nozle is installed movably in the axial direction, while swirling vanes
are provided on the outer periphery thereof and air dampers for adjusting the primary
and the secondary air ratio is provided on the outside of a primary air supply tube.
[0008] Another object of the present invention is to provide a radiant tube burner in which
the flame temperature is reduced by means of adding atomized water into the combustion
flame, thereby making it possible to obtain low NOx, while high heat load combustion
is going on in satisfactory and stable way owing to the two-stage combustion descirbed
above.
[0009] In order to attain the second object, a water spray nozzle is placed at the center
of the divergent flame type nozzle, said nozzle being connected to an atomized water
generator capable of supplying pressurized gas and additive water through an additive
water transfer tube installed in the gas burner.
[0010] Further, as a different advantageous means according to the present invention, the
atomized water generator is composed of a cylinder having a conical hole to be connected
to the additive water transfer tube, a recessed disk having grooves for injecting
pressurized gas and additive water thereinto and fitted to said cylinder and a housing
for accommodating said cylinder and said disk.
[0011] It is also another object of the present invention to provide a radiant tube burner
in which, in addition to the aforementioned features, the exhaust gas is used as atomizing
medium, thereby accomplishing enhanced reduction of NOx while high heat load and low
NOx combustion occurs due to the swirling of the primary air and addition of atomized
water into the combustion flame.
[0012] In order to attain the third object, the atomized water generator is connected to
the exhaust gas pipe, while other parts remain the same as described in the second
object.
[0013] Further, as another advantageous means to materialize the object of the invention,
low pressure fuel gas can be used as atomizing medium. In this case, the water atomizer
is connected to the fuel gas while other parts remain the same as described in the
second object.
[0014] In addition, as another advantageous means, an exhaust gas introducing tube and a
water out-flow nozzle are placed at the central portion of the divergent flame tube
nozzle to utilize the velocity energy of low pressure exhaust gas to atomize the water
supplied from the additive water transfer tube.
[0015] The above-mentioned objects and features of this invention will be evident from the
following description presented in reference to the drawings which indicate embodiments
of the invention.
BRIEF DESCRIPTION OF THE DRAWINGS
[0016]
Fig. 1 is a longitudinal sectional view showing an embodiment of the radiant tube
burner according to the present invention;
Figs. 2 and 3 are a front view and a sectional view showing the divergent flame type
nozzle in the burner of the present invention;
Figs. 4 and 5 are a longitudinal sectional view and a front view showing primary air
swirling vanes in the burner of the present invention;
Fig. 6 shows the amount of generated NOx versus the maximum temperature of the radiant
tube for explaining the effect of NOx reduction in the radiant tube burner according
to the present invention;
Fig. 7 is a longitudinal sectional view showing a second embodiment of the radiant
tube burner according to the present invention;
Fig. 8 is a longitudinal sectional view showing the divergent flame type nozzle used
in the burner of the present invention;
Figs. 9 and 10 are a fragmentary exploded perspective view and an assembled sectional
view showing the atomized water generator in the burner of the present invention.
Fig. 11 explains the mechanism of atomized water generation;
Fig. 12 is a longitudinal sectional view showing a third embodiment of the radiant
tube burner·according to the present invention;
Fig. 13 is a longitudinal sectional view showing the divergent flame type nozzle in
the burner of the present invention;
Fig. 14 is a view, partially cross-section, showing a major portion of a fourth embodiment
of the radiant tube burner according to the present invention using the water atomizing
system with low pressure fuel gas;
Fig. 15 is a view, partially cross-section, showing a major portion of a fifth embodiment
of the radiant tube burner according to the present invention adopting the atomized
water system by low pressure exhaust gas; and
Fig. 16 shows the amount of additive water versus the reduction rate of NOx in the
radiant tube burner according to the present invention.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0017] Referring to Fig. 1 showing the first embodiment, a gas burner 1 is coaxially placed
with a combustion tube 2. A divergent flame type nozzle 3a (see Figs. 2 and 3) is
mounted at the end of the burner 1. At the rear end of the burner 1, there is a fuel
gas connection 4. A primary air supply tube 5 joins the rear end of the combustion
tube 2 to form an integral piece extending coaxially with the burner 1. The primary
air supply tube 5 has four rectangular ports 6 evenly spaced over the entire periphery
thereof. The area of the inlet 6 can be changed by moving, with an operating rod 8
and a nut 9, a cylindrical air damper 7, into which the air supply tube 5 is loosely
fitted. Primary air swirling vanes 10 having an angle within the range from 15 to
60° are secured on a retaining tube 11 at the front end of said burner 1, as shown
in Figs. 4 and 5. The combustion tube 2 and the primary air supply tube 5 are coaxially
housed in a radiant tube 12. An air supply connection 13 is provided at the rear section
of the radiant tube 12 in which the inlet ports 6 are located. An end cover 14 closes
rear ends of the primary air supply tube 5 and radiant tube 12. The gas burner 1 is
installed across said end cover 14 to extend rearward. Reference numeral 15 designates
a pilot burner. The gas burner 1 extends movably through the end cover 14 in the axial
direction within the range of the combustion tube 2 together with the pilot burner
15. Accordingly, the divergent flame type nozzle 3a is supported in the combustion
tube 2 through the swirling vanes 10 so that the nozzle position is changeable.
[0018] The set position L of the divergent flame type nozzle 3a is changeable within the
range from 100 to 500 mm. The burner 1 is fixed by a bolt 16 attached on the end cover
14.
[0019] Next, the operating mechanism of the radiant tube burner according to the first embodiment
of the present invention will be described in the following. Referring to Fig. 1,
the gas supplied to the gas burner 1 through the connection 4 is ejected from the
divergent flame type nozzle 3a into the combustion tube 2 at the maximum ejection
angle of 60° and at the speed ranging from 10 to 100 m/sec. The jetted fuel gas mixes
with primary air C
1 which flows through the inlet 6 and is swirled by the swirling vanes 10 before being
burnt in reduced primary combustion at the high heat load within the range from 500
x 10
4 kcal/m
3-h 1,000 x 10
4 kcal/m
3-h. The primary combustion gas issues from the combustion tube 2 in the axial direction
into the radiant tube 12 at the speed within the range from 10 to 30 m/sec. Secondary
air C
2 (90 to 50%) throttled by the air damper 7 to be at a required ratio with respect
to the primary air C
1 (10 to 50%) is fed through the annular passage between the combustion tube 2 and
the radiant tube 12 while cooling said combustion tube 2 at a speed slower than that
of the primary combustion gas. The secondary air C
2 flows along the inside of the radiant tube 12 due to the kinetic energy differential
between the secondary air C
2 and the primary combustion gas, while making the secondary combustion occur in less
concentrated way to prevent localized heating at the boundary against the primary
combustion gas, thereby controlling the generation of NOx.
[0020] Test result with a 7 inch (17.5 cm) radiant tube burner according to the first embodiment
of the present invention are as follows. The heat rate was as much as 145,000 kcal/h
while generally accepted limit had been 110,000 kcal/h with prior art. NOx may be
reduced to 80 through 150 ppm by changing the position of the nozzle 3a and the primary
and the secondary air ratio. Furthermore, there was little soot and carbon monoxide
even under the stringent condition where the residual 0
2 in the exhaust gas was less than one percent. It is also possible to obtain turn-down
ratio less than 10% down to which stable combustion can be performed without blowout
even when combustion air flow capacity is held at 100% and fuel gas is throttled down
to 10%.
[0021] Regarding the tube temperature, which is an important factor in the operation of
radiant tube burners, it is possible to obtain uniform tube temperature due to the
rotation of the flame, with the temperature change in the circumferential direction
within 10°C. Further, the temperature difference in the axial direction between the
maximum and the minimum in the furnace is made within 150°C, so that extended tube
life can be expected.
[0022] Fig. 6 shows the maximum temperature of the radiant tube versus the amount of generation
of NOx to explain the effect of NOx reduction according to the present invention.
It is obvious that NOx can be reduced by approximately 30% compared with a prior art
radiant tube burner.
[0023] Next, the second embodiment according to the present invention is described in the
following with reference to Fig. 7. The numbers in Fig. 7 refer to the corresponding
parts which are the same as illustrated in Fig. 1.
[0024] Referring to Figs. 7 and 8, the gas burner 1 is placed coaxially with the combustion
tube 2. The divergent flame type nozzle 3a is mounted at the end of the burner 1.
At the rear end of the burner 1, there is the fuel gas connection 4. The primary air
supply tube 5 joins the rear end of the combustion tube 2 to form an integral piece
extending coaxially with the burner 1. The primary air supply tube 5 has four rectangular
ports 6 evenly spaced over the entire periphery thereof. The primary air swirling
vanes 10 having an angle within the range from 15 to 60° are secured on a retaining
tube (not shown) at the end of said burner 1. The combustion tube 2 and the primary
air supply tube 5 are coaxially housed in the radiant tube 12. The primary air supply
tube and the radiant tube are closed by the end cover through flanges respectively.
Further, the gas burner 1 is installed across the end cover to extend rearward.
[0025] A water spray nozzle 18 communicating to an additive water transfer tube 17 placed
in said gas burner 1 is provided at the center of the divergent flame type nozzle
3a and a multiple number of gas injection ports 14 communicating to the gas connection
4 are provided around said nozzle 18 as shown in Fig. 8. Further, an air supply connection
13 is connected to the rear section of the radiant tube 12. An atomized water generator
22 connected to the pressurized gas tube 20 and the additive water transfer tube 21
is at its rear end.
[0026] Referring to Figs. 9 and 10, the atomized water generator 22 consists of a disk 24
having a circular recess 23 and a conical hole 25 with its diameter gradually decreasing
from that corresponding to said recess. Further, a cylinder 26 having the same diameter
as that of said disk 24 is coaxially fitted to said disk to form integrally with each
other and then built in a housing 27. The disk 24 is surely pressed by a plug 28 and
the cylinder 26 is connected to the additive water transfer tube 17. When the disk
is fitted to the cylinder, an atomized water generating chamber 29 is formed. Grooves
30 and 31 for introducing the pressurized gas and the additive water and communicating
to said recess 23 in the tangential direction thereof are provided on one plain perpendicular
to the center axis at the end face of the disk 24 near the cylinder 26. These grooves
are connected to the pressurized gas supply tube 20 and the additive water supply
tube 21_respectively.
[0027] The second embodiment of the present invention is a combination of the first embodiment
and atomized water injection. For ease of understanding explanation on the air and
the gas flow will be repeated. Referring to Fig. 7, the fuel gas supplied to the gas
burner 1 through the connection 4 is ejected from the divergent flame type nozzzle
3a into the combustion tube 2. The jetted fuel gas mixes with the primary air C1 which
flows through the inlet 6 and is swirled by the primary air swirling vanes 10 before
being burnt in reduced primary combustion at the high heat load. Then, the primary
combustion gas issues from the combustion tube 2 similarly to the first embodiment
noted above.
[0028] On the other hand, the secondary air C
2 throttled by the air damper 7 as shown in Fig. 1 to be at a required ratio with respect
to the primary air C
1 is fed through the annular passage between the combustion tube 2 and the radiant
tube 12 while cooling said combustion tube 2 and then flows along the inside of the
radiant tube. Thus, the secondary combustion successively occurs to prevent localized
heating at the boundary against the primary combustion gas. The atomized water is
obtained by the atomized water generator 18 as shown in Figs. 10 and 11, being injected
from the water spray nozzle 18 located at the center of the divergent flame type nozzle
3a, thereby reducing the flame temperature to restrain the generation of NOx. In this
case, bubbles of the atomized water is sharply expanded to blow up through injection
due to the differential pressure across the bubbles and the combustion tube. Since
the thickness of the bubble is very thin, i.e., 0.1µ m or above, the pieces of the
blown-up bubbles are very fine. Therefore, the fine water particles will quickly absorb
the latent heat from the flame, thereby greatly reducing the generation of NOx due
to the lowered flame temperature.
[0029] Next, the third embodiment of the radiant tube burner according to the present invention
will be described with reference to Figs. 12 and 13. The number in Figs. 12 and 13
refer to the corresponding parts which are the same as illustrated in Figs. 7 and
8. However, it differs from the second embodiment in such a point that the exhaust
gas is ejected into the center of the fuel gas as atomizing medium while in the second
embodiment water is used as atomizing medium.
[0030] Since the mechanism of the radiant tube burner in the third embodiment of the present
invention is similar to that of the second embodiment with only such difference that
the nozzle is constituted as a divergent flame type nozzle 3b, the description thereof
will be omitted.
[0031] Next, Fig. 14 shows a modification of the third embodiment of the present invention
which is related to the atomizing system due to low pressure fuel gas. As shown in
Fig. 14, the gas burner 1 is placed coaxially with the combustion tube 2. The divergent
flame type nozzle 3b is provided at the front end of the burner 1. A water outflow
nozzle 32 is provided at the center of the nozzle 3b. In the annular space defined
by the water outflow nozzle and the exhaust gas nozzle are installed gas swirling
vanes 33 having an angle within the range from 15 to 40°.
[0032] Next, the operating mechanism of the radiant tube burner of the modification of the
third embodiment employing the atomizing system with low pressure fuel gas will be
described in the following. As shown in Fig. 14, the gas G introduced into the gas
burner 1 from the gas connection 4 is fed in the direction shown by the arrow to be
swirled at high speed by the gas swirling vanes 33, while the water W introduced into
the additive water transfer tube 17 (See Figs. 12 and 13) connected to an additive
water connection port 36 is fed in the direction shown by an arrow to issue from the
water outflow nozzle 32. In this case, the water discharged from the water outflow
nozzle is atomized by the velocity energy of the fuel gas.
[0033] Thus, since the water is atomized by the velocity energy of the fuel gas, the atomized
water and fuel gas are sufficiently mixed with each other and the effect of water
addition is greatly enhanced.
[0034] Figs. 14 and 15 show a modification of the third embodiment of the present invention
which is related to the atomizing system with low pressure exhaust gas. As shown in
the figures, an exhaust gas introducing tube 34 for atomizing the water supplied from
the water outflow nozzle 32 is placed at the center of the divergent flame type nozzle
3b. The additive water transfer tube 17 is placed at the center of the introducing
tube 34. In the annular space defined by the water outflow nozzle and the exhaust
gas nozzle are provided exhaust gas swirling vanes 35 having an angle within the range
from 15 to 40°.
[0035] The mechanism of the radiant tube burner of the modification of the third embodiment
employing the atomizing system with the low pressure exhaust gas will be described
in the following. As shown in Fig. 15, the exhaust gas G' is swirled at high speed
by the exhaust gas swirling vanes 35 to atomize the water W discharged from the water
outflow nozzle 32. The atomized water is mixed with the fuel gas G (WG) supplied from
the divergent flame type nozzle 3b by the high speed swirling flow of the exhaust
gas. Therefore, the mixing of the exhaust gas and the fuel gas and that of the fuel
gas and the atomized water occur rapidly to reduce the flame temperature by making
the flame temperature uniform due to the combustion delay of the fuel gas and absorption
of the latent heat by the atomized water, thereby greatly reducing the generation
of NOx.
[0036] The radiant tube burner including two modifications of the third embodiment noted
above has two ways of water atomizing system. One is using pressurized gas (air, vapor
and inert gas) within the range from 2 to 6 kg/cm
2 and the other is using low pressure gas (fuel gas, exhaust gas or the like) with
the range from 300 to 1,000 mm AG.
[0037] NOx reduction rate by adding water in the radiant tube burner according to the present
invention including the third and fourth embodiments is represented by the relation
between the amount of additive water and the NOx reduction rate as shown in Fig. 16.
[0038] Operational factors of the radiant tube burner according to the present invention
noted above are shown as follows:
Fuel COG : 4,500 kcal/Nm
calorific force : 145,000 kcal/h
air temperature for combustion : 400°C
Residual 02 contained in the exhaust gas : 4 %
radiant tube type : 7 inch W type
where, the amount of additive water is gradually increased to obtain higher NOx reduction
rate (%).
[0039] As is obvious from the result, NOx can be efficiently reduced by adding water in
the radiant tube burner Furthermore, since the maximum tube temperature may be lowered,
the extended tube life can be expected.>
[0040] As has been described in the foregoing, the radiant tube burner according to the
present invention will give utmost effectiveness when used for a furnace in which
direct exposure of workpieces to waste gas is not desirable. i.e., non-oxidation furnaces,
heat treatment furnaces and the like utilizing atmospheric gas and indirect heating
system in which workpieces and waste gas should not come in contact. Applicable fields
will include those industries such as metalworking industry, ceramics, glass industry,
chemical industry, paper and fiber industry and food industry or the like.
1. In a system in which a nozzle of a gas burner is coaxially placed in a combustion
tube installed in a radiant tube and fuel gas coming out of the gas burner undergoes
primary combustion by primary air supplied through the annular space between said
gas burner and said combustion tube and further undergoes secondary combustion by
secondary air supplied through the annular space between said combustion tube and
said radiant tube, a radiant tube burner comprising:
a gas burner having a divergent flame type nozzle at its end and designed to be movable
in the axial direction while placed coaxially in a combustion tube;
primary air swirling vanes located at the end of said burner, for forming a swirled
flame; and
an air damper fitted on a primary air supply tube connected to said combustion tube,
for adjusting the primary and the secondary air ratio.
2. A radiant tube burner according to claim 1, wherein the secondary air C2 (90 to 50%) is controlled by said air damper to a required ratio with respect to
the primary air C1 (10 to 50%).
3. A raidant tube burner according to claim 1, wherein said divergent flame type nozzle
has a set position L changeable within the range from 100 to 500 mm..
4. In a system in which a nozzle of a gas burner is coaxially placed in a combustion
tube installed in a radiant tube and fuel gas coming out of the gas burner undergoes
primary combustion by primary air supplied through the annular space between said
gas burner and said combustion tube and further undergoes secondary combustion by
secondary air supplied through the annular space between said combustion tube and
said radiant tube, a radiant tube burner comprising:
a gas burner having a divergent flame type nozzle at its end coaxially placed in a
combustion tube with a water spray nozzle placed at the center; and
an atomized water generator capable of supplying pressurized gas and additive water;
whereby said nozzle is connected with said atomized water generator through an additive
water transfer tube installed in said gas burner.
5. A radiant tube burner according to claim 4, wherein said atomized water generator
consists of a cylinder having a conical hole to be connected to the additive water
transfer tube, a recessed disk having grooves for injecting pressurized gas and additive
water thereinto and fitted to said cylinder and a housing for accommodating said cylinder
and said disk.
6. A radiant tube burner according to claim 4, wherein a water outflow nozzle is placed
at the center of the divergent flame type nozzle to atomize the water supplied from
the additive water transfer tube by the velocity energy of low pressure fuel gas.
7. A radiant tube burner according to claim 4, wherein an exhaust gas introducing
tube and a water outflow nozzle are placed at the center of the divergent flame type
nozzle to atomize the water supplied from the additive water transfer tube by the
velocity energy of low pressure exhaust gas.
8. A radiant tube burner accoridng to any one of claims 4 to 7, wherein the atomized
water addition is performed by using the pressurized gas (air, vapor and inert gas)
within the range from 2 to 6 kg/cm2 and the low pressure gas (fuel gas, exhaust gas or the like) within the range from
300 to 1,000 mmAg.