U.S. patent number 3,869,244 [Application Number 05/432,955] was granted by the patent office on 1975-03-04 for burner unit.
This patent grant is currently assigned to SAID Robert von Linde, by said Joachim von Linde and German Kurz. Invention is credited to German Kurz, Joachim Von Linde, Robert Von Linde.
United States Patent |
3,869,244 |
Von Linde , et al. |
March 4, 1975 |
BURNER UNIT
Abstract
A burner unit for fluid fuels and also for pulverized coal
comprising comtion chamber means, prechamber means, means to enable
combustion gases to pass from said combustion chamber means into
said prechamber means, mixing pipe means in communication with said
prechamber means and said combustion chambers means, a fuel supply
nozzle for distributing finely divided fuel towards said mixing
pipe means into the drawn-in combustion gases, and means for
supplying oxygen-containing gas, f.i. air, to the mixture of fuel
and combustion gases, wherein said means for supplying
oxygen-containing gas comprises a plurality of exit openings
arranged symmetrically about the longitudinal axis of said fuel
supply nozzle to increase the suction effect of the
oxygen-containing gas on the combustion gases drawn into said
prechamber means.
Inventors: |
Von Linde; Robert (Grafelfing,
DT), Von Linde; Joachim (Grafelfing, DT),
Kurz; German (Karlsfeld, DT) |
Assignee: |
SAID Robert von Linde, by said
Joachim von Linde and German Kurz (N/A)
|
Family
ID: |
5869772 |
Appl.
No.: |
05/432,955 |
Filed: |
January 14, 1974 |
Foreign Application Priority Data
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Jan 24, 1973 [DT] |
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2303280 |
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Current U.S.
Class: |
431/116;
431/9 |
Current CPC
Class: |
F23C
9/006 (20130101); F23C 7/06 (20130101) |
Current International
Class: |
F23C
7/00 (20060101); F23C 7/06 (20060101); F23C
9/00 (20060101); F23m 003/14 () |
Field of
Search: |
;431/115,116,9,158 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Favors; Edward G.
Attorney, Agent or Firm: Kane, Dalsimer, Kane, Sullivan and
Kurucz
Claims
What we claim is:
1. A burner unit comprising combustion chamber means, prechamber
means, means to enable combustion gases to pass from said
combustion chamber means into said prechamber means, mixing pipe
means in communication with said prechamber means and said
combustion chamber means, a fuel supply nozzle for distributing
finely divided fuel towards said mixing pipe means into said
recirculated combustion gases, and means for supplying
oxygen-containing gas to the mixture of fuel and combustion gases,
wherein said means for supplying oxygen-containing gas comprises a
plurality of exit openings arranged symmetrically about the
longitudinal axis of said fuel supply nozzle, said means for
supplying oxygen-containing gas comprises pipes extending into the
prechamber and arranged symmetrically about the fuel supply nozzle,
the interstices between adjacent pipes forming passageways for the
recirculated combustion gases into the space of the prechamber
surrounding the fuel supply nozzle.
2. A burner unit according to claim 1, wherein said pipes are
substantially parallel to the longitudinal axis of the fuel supply
nozzle.
3. A burner unit according to claim 1, wherein said pipes are
inclined towards the longitudinal axis of the fuel supply nozzle
with an angle up to 15.degree., preferably between 5.degree. and
10.degree..
4. A burner unit comprising combustion chamber means, prechamber
means, means to enable combustion gases to pass from said
combustion chamber means into said prechamber means, mixing pipe
means in communication with said prechamber means and said
combustion chamber means, a fuel supply nozzle for distributing
finely divided fuel towards said mixing pipe means into said
recirculated combustion gases, and means for supplying
oxygen-containing gas to the mixture of fuel and combustion gases,
wherein said means for supplying oxygen-containing gas comprises a
plurality of exit openings arranged symmetrically about the
longitudinal axis of said fuel supply nozzle, at least two groups
of exit openings being provided with each group being connected or
disconnected separately to or from a combustion air supply
source.
5. A burner unit comprising combustion chamber means, prechamber
means, means to enable combustion gases to pass from said
combustion chamber means into said prechamber means, mixing pipe
means in communication with said prechamber means and said
combustion chamber means, a fuel supply nozzle for distributing
finely divided fuel towards said mixing pipe means into said
recirculated combustion gases, and means for supplying
oxygen-containing gas to the mixture of fuel and combustion gases,
wherein said means for supplying oxygen-containing gas comprises a
plurality of exit openings arranged symmetrically about the
longitudinal axis of said fuel supply nozzle, the exit openings
being arranged in the inner surface of the mixing pipe and being
connected to a source of oxygen-containing gas via annular spaces
in the wall of the mixing pipe.
6. A burner unit according to claim 5, wherein two groups of exit
openings are provided with each group being individually
connectable to or disconnectable from a source of oxygen-containing
gas.
7. A burner unit according to claim 6, wherein the exit openings of
the one group have a bigger cross-section than the exit openings of
the other group with one exit opening of one group being located
between two adjacent exit openings of the other group.
Description
BACKGROUND OF THE INVENTION
This invention relates to burner units for fluid fuels such as oil,
gas or pulverized coal which are injected into hot combustion gases
drawn back from the combustion chamber into a prechamber by the
suction effect of the combustion air or other oxygen-containing gas
supplied to the unit at relatively high velocities. Such burner
unit is f.i. disclosed in U.S. Pat. No. 3,174,526. In this known
burner the combustion air is supplied through an annular gap
co-axial with the longitudinal axis of the fuel supply nozzle and
creates a suction effect in the prechamber whereby combustion gases
are drawn back from the combustion chamber. The main advantage of
such burners is the fact that the fuel is mixed with the hot
combustion gases prior to the admixture of combustion air so that
the fuel has good ignition properties when it comes in contact with
the combustion air. This improves combustion considerably. However,
the known burner suffers from some difficulties one of which is the
necessity that the combustion air supply pipe must cross the path
of the re-circulated combustion gases which affords complicated
parts subjected to high thermal stresses. Furthermore, the supply
of combustion air through one nozzle only limits the working range
of the burner because if the quantity of air is reduced in order to
reduce the rate of combustion the velocity of the air streaming
through the annular nozzle is correspondingly reduced and therefore
also the suction effect on the recirculated combustion gases. In
practice, therefore, the capacity of the burner can be varied only
between full load and one third load whereas in many applications a
variation down to one tenth load would be desirable.
These difficulties are avoided in the present invention by
supplying the oxygen-containing gas f.i. air through a plurality of
exit openings arranged symmetrically about the longitudinal axis of
the fuel supply nozzle. Compared with a single annular air supply
gap the same quantity of air passes through the plurality of exit
openings with much high velocity so that a higher reduction of the
quantity of air is possible without affecting the recirculation of
combustion gases. A very simple and effective means for reducing
the air supply is the cutting off of some of the exit openings from
the air source. The air passing through the remaining exit openings
has a velocity high enough to ensure proper recirculation of
combustion gases even at one tenth load of the burner.
Accordingly, it is an object of the present invention to provide a
burner of the type mentioned above which enables variation of the
burner capacity over a comparatively large range without adversely
affecting the combustion qualities.
The exit openings are connected via pipes or passages with
pressurized air supply means. These pipes or passages can be
parallel to the longitudinal axis of the fuel supply nozzle or they
can be inclined thereto with an angle of between 5.degree. and
10.degree., in special cases up to 15.degree.. Preferably the exit
openings for the combustion air are located downstream of the fuel
supply nozzle in order to obtain a big prechamber within which the
combustion gases can react with the fuel before the combustion air
is added.
The exit openings can be combined to individual groups with the
openings of each group being symmetrically arranged about the fuel
nozzle axis, whereby each group can be connected or disconnected to
or form the air source in order to vary the capacity of the burner.
Furthermore, the exit openings of one group may have a different
size of the exit openings of another group. If only two exit
openings are provided they are arranged diametrically opposed and
may have different sizes, the smaller opening only being supplied
with air at low load.
Normally the exit openings will be arranged outside the prechamber
and f.i. in the wall of the mixing pipe. Nozzles can be inserted in
the exit openings.
The connection and disconnection of individual exit openings or
groups of exit openings can take place outside the burner by means
of valves in the supply pipes.
Further objects, features and advantages of the present invention
will become apparent from the following description in connection
with the drawings which show, for purposes of illustration only,
some embodiments in accordance with the present invention.
DESCRIPTION OF THE DRAWINGS
FIG. 1 is a sectional elevational view of a first embodiment of a
burner unit according to the invention;
FIG. 2 is a cross-sectional view taken along line A-A of FIG.
1;
FIG. 3 is a sectional elevational view of a second embodiment of a
burner unit according to the invention with the combustion chamber
omitted; and
FIG. 4 is a sectional elevational view of a third embodiment of a
burner unit according to the invention.
DETAILED DESCRIPTION OF THE EMBODIMENT
Referring now to FIGS. 1 and 2, reference numeral 7 designates a
combustion chamber having a refractory lining 11 and an outlet
opening 12 for the burnt gases. The combustion chamber 7 is flanged
to a burner assembly generally designated 20 comprising an outer
shell 21 and an inner shell 5. Centrally within inner shell 5 is
arranged a mixing pipe 6 having a flange 22 with openings 23. A
fuel supply nozzle 1 is arranged in the inner shell 5 co-axial with
the longitudinal axis 24 of the burner unit. The space 4 between
outer shell 21 and inner shell 5 is connected by a connector 3 to a
blower (not shown) which supplies the combustion air. Pipes 2
extend from the space 4 into the prechamber 25 enclosed by inner
shell 5 and extending up to the mixing pipe 6.
In operation the combustion air is supplied through connector 3 to
space 4 and through pipes 2 into the prechamber 25. By the injector
effect of the air streaming out of pipes 2 combustion gases are
sucked back from the combustion chamber 7 through the openings 23
in flange 22, through annular chamber 8 into prechamber 25 where
they are mixed with the fuel emerging from fuel nozzle 1. The
finely divided fuel reacts with the hot combustion gases and forms
reduction products of a precombustion. These products are delivered
into the mixing pipe 6 by the air jets and are mixed with the air.
The mixture of fuel, recirculated combustion gases, reduction
products and air emerges from the exit opening 9 of the mixing pipe
6 and is ignited by the flame vortex 10. Naturally the first
ignition is effected by the usual ignition device (not shown). The
burning of the mixture takes place in the combustion chamber 7.
It is apparent that the fuel droplets or particles (in the case of
pulverized coal) cover a long distance within undiluted combustion
gases owing to the arrangement of the exit openings of the air
pipes 2 downstream of the fuel nozzle 1, so that the fuel has ample
time to react with the combustion gases.
As can be seen from FIG. 2, the recirculated combustion gases can
flow through the interstices between the pipes 2 into the space
surrounding the fuel nozzle 1. In this embodiment three groups of
air pipes are formed namely a, a'; b, b' and c, c'. Each group can
be individually connected to or disconnected from the air supply.
For full load all groups are supplied with air whereas for partial
load one or two groups are disconnected. For this purpose a rotary
valve 13 shown diagrammatically in FIG. 1 can be provided.
The embodiment of FIG. 3 differs from the embodiment of FIG. 1 only
by a shorter mixing pipe 6' and longer air supply pipes 2'. Again
the recirculated combustion gases enter partially the space around
fuel nozzle 1 through the interstices between the air pipes 2', and
partially they mix directly with the combustion air. As can be
seen, the exit openings of pipes 2' are a relatively great distance
from the fuel nozzle 1, thus enabling a long reaction of the fuel
with the recirculated combustion gases prior to the admixture of
the combustion air.
In the embodiment of FIG. 4 the combustion air is supplied to the
interior of the mixing pipe 46 through openings 42 and 42' which
are connected to annular chambers 48, 49 respectively, which are in
turn connected to air supply pipes 43, 43'. The air jets emerging
from the openings 42 and 42' into the mixing pipe 46 in direction
towards the combustion chamber 7 generate a pressure rise in the
downstream portion 46' of the mixture pipe. This pressure rise
effects a recirculation of hot combustion gases from the combustion
chamber 7 through passages 41 in the wall of the mixing pipe 46
into the prechamber 50 accommodating duel nozzle 1. The fuel which
mixes with the hot combustion gases has relatively long time to
react therewith until it reaches the air exit openings 42, 42'. In
this example the combustion chamber 7, which, owing to the good
preparation of the fuel and the intimate mixing with the combustion
air can be run with very high performance, is liquid-cooled.
The air exit openings 42 of the one group are of smaller
cross-section than the air exit openings 42' of the other group.
The openings of each group are equally spaced around the
circumference of mixing pipe 46 with one opening of one group
always between two openings of the other group. According to the
desired performance of the burner the one or the other or both
groups are supplied with combustion air. This burner is especially
suited for operation with liquid hydrocarbons which are burnt with
blue flame without generation of soot and even in substochiometric
mixture. However, also all combustible gases, particularly the
gaseous hydrocarbons, can be burnt.
The burner of the present invention is also well suited for burning
pulverized coal owing to the long reaction time available prior to
the mixing with the combustion air. Furthermore, it should be
pointed out that the burner can be operated with oxygen instead of
air. Finally it should be remarked that the combustion air flowing
through space 4 is heated and at the same time forms a heat
isolation for the prechamber and the space 8 through which the
combustion gases are recirculated.
Thus the several aforenoted objects and advantages are most
effectively attained. Although several somewhat preferred
embodiments have been disclosed and described in detail herein, it
should be understood that this invention is in no sense limited
thereby and its scope is to be determined by that of the appended
claims.
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