U.S. patent number 3,830,172 [Application Number 05/379,684] was granted by the patent office on 1974-08-20 for incinerator.
This patent grant is currently assigned to North American Mechanical Limited. Invention is credited to Arthur W. Hindenlang.
United States Patent |
3,830,172 |
Hindenlang |
August 20, 1974 |
INCINERATOR
Abstract
Comminuted waste fuel or material is injected into the
incinerator at the bottom thereof through a conduit. Centrally
arranged in this conduit, at the discharge end thereof is a second
auxiliary fuel conduit which is provided at its termination end
within the first conduit with a plurality of fuel discharge
orifices which are directed radially outwardly and upwardly towards
the discharge end of the first conduit. The incinerator also
includes provision for a separator wherein the baffles and bottom
disc are cooled by means of circulating air which is then
discharged from the disc portion of the separator in a tangential
direction complementing the direction of rotation of the cyclone
within the incinerator.
Inventors: |
Hindenlang; Arthur W. (London,
Ontario, CA) |
Assignee: |
North American Mechanical
Limited (London, Ontario, CA)
|
Family
ID: |
23498247 |
Appl.
No.: |
05/379,684 |
Filed: |
July 16, 1973 |
Current U.S.
Class: |
110/238; 110/216;
110/244 |
Current CPC
Class: |
F23G
5/32 (20130101); F23J 15/022 (20130101); F23D
17/00 (20130101) |
Current International
Class: |
F23D
17/00 (20060101); F23G 5/32 (20060101); F23J
15/02 (20060101); F23g 005/12 () |
Field of
Search: |
;110/7R,7S,8R,8C,18R,18C,22R,22A |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Sprague; Kenneth W.
Attorney, Agent or Firm: Wheeler, Morsell, House &
Fuller
Claims
What I claim as my invention is:
1. A co-axial burner for use in suspension burning incinerators of
the cyclone type to burn comminuted waste material, comprising, an
outer comminuted waste and primary air supply conduit and an inner
co-axial auxiliary fuel supply conduit, the inner wall of said
outer conduit being spaced apart from the outer wall of the
auxiliary fuel supply conduit to thereby define an annular passage
and to permit the flow of comminuted waste and primary air
therethrough, said outer conduit having an outwardly flared
discharge end and said auxiliary fuel supply conduit terminating
within said outer conduit proximate the outwardly flared discharge
end thereof, said auxiliary fuel supply conduit including at its
termination end a burner element provided with a plurality of first
fuel discharge orifices wherein said first orifices are circularly
arranged and directed radially outwardly and upwardly from said
fuel supply conduit towards the discharge end of said outer conduit
and said first orifices are in communication with said fuel supply
conduit.
2. A co-axial burner as claimed in claim 1, wherein said burner
element is provided with a plurality of second fuel discharge
orifices communicating with a secondary fuel supply conduit
internally of said auxiliary fuel supply conduit, said second fuel
dicharge orifices being positioned internally of said first fuel
discharge orifices and wherein said second orifices are circularly
arranged and directed radially outwardly and upwardly from said
secondary fuel supply conduit towards the discharge end of said
outer conduit.
3. A co-axial burner as claimed in claim 1, wherein said auxiliary
fuel supply conduit at its termination end is provided with an
upwardly and outwardly tapering annular and perforated shield.
Description
BACKGROUND OF THE INVENTION
This invention relates to improvements in incinerators and has
particular application to incinerators of the cyclone type which
are used to burn comminuted waste material.
DESCRIPTION OF THE PRIOR ART
In many conventional cyclone incinerators, the reduced garbage and
refuse is supplied to the combustion chamber via a primary air
supply conduit. Exemplary of this is the incinerator disclosed in
U.S. Pat. 3,566,809 which issued on Mar. 2, 1972 in the name of
Ecology Industries, Inc. wherein the primary air carrying the
comminuted waste fuel is injected under pressure into the bottom of
the combustion chamber through a discharge pipe. The pipe at its
discharge end is surrounded by an annular ring burner, the function
of which is to ignite the waste fuel or material issuing from the
discharge pipe. The problem inherent in this type of ignition
system resides in the fact that the flame from the annular ring
burner must penetrate into the core of the discharge stream of
primary air and comminuted waste fuel in order to effect a proper
primary combustion. Since the velocity of the primary air and waste
material is relatively high the mass flow of the auxiliary fuel
flowing through the jets or orifices in the annular ring burner
must also be relatively high. The problem here is that the primary
burner, because of its annular construction, necessarily must in
surrounding the discharge pipe, cover a large surface area and
consequently be provided with a large number of auxiliary fuel jets
or orifices which are spaced relatively close to one another for
mutual flame support. This has the effect of reducing the mass flow
of the auxiliary fuel which is available in order to properly
penetrate the primary air and waste fuel or material.
Many incinerators today are provided with what is termed a
separator which is located downstream of the discharge vent of the
combustion chamber. Basically, the separator is cage-like in
appearance and similar to that disclosed in the Ecology patent
aforesaid. The primary purpose of the separator is to further
reject uncombusted and non-combustible materials from the
combustion gases passing therethrough. This rejected material is
either recycled for combustion in the chamber or withdrawn as
reject in the ash-sump. Because of the completion of combustion and
maximizing of temperature, the cyclone effect within the chamber
decays materially at a point where its centrifugal action is most
needed. This is not readily cured by the provision of secondary air
inlet ports in the walls of the incinerator opposite the separator
since the swirling action is most required at the periphery of the
lower baffle disc where a void has been left by the natural action
of the gases in passing this obstruction during its upward flow.
Further, most separators are water cooled which, in addition to
causing serious maintenance and water treatment problems,
effectively reduces the operating temperature thereof below the
melting point of glass particulate material which otherwise would
adhere thereto and drop off in the form of slag.
SUMMARY OF THE INVENTION
I have found that the foregoing combustion disadvantages can be
overcome or minimized by providing for a co-axial burner and
primary air-waste system wherein the burner is centrally positioned
and the conduit for the primary air and waste fuel or material is
arranged thereabout. The advantage of positioning the burner
centrally and the waste fuel supply conduit thereabout is that
better ignition of the waste fuel is achieved by virtue of the fact
that the flame from the central burner can penetrate the waste
stream more efficiently. Further, because the burner is centrally
located, its fuel jets are much closer together and thus are
mutually flame supporting to a far greater degree than is the case
with ring burners. This permits the fuel jets of the central burner
to be of a greater diameter than the jets of a ring burner and
hence the novel construction permits a far greater mass flow of
auxiliary fuel through each jet of the central burner for any given
total mass flow, with a resultant improved degree of penetration of
flame through the waste fuel stream.
I have also found that providing the inner wall of the primary air
supply conduit with one or more ribs, vanes or baffles arranged in
a fashion to impart a whirling motion to the waste material passing
therethrough, such as a helix, produces a more intimate mixing of
the primary combustion air with the waste fuel. Additionally, it is
a function of these radial deflector vanes to separate
non-combustible metal and glass particulate components of the waste
by centrifugal force from the main stream of the flame issuing from
the co-axial burner. Metal particles drop out of the stream of
products of combustion into an ash sump and fine glass particles
are caused to adhere to combustion chamber walls of the incinerator
which is operating at temperatures above glass fusion temperature.
This glass coating on the combustion chamber walls continuously
flows down or drops from the walls (as molten slag) into the ash
sump. The trapping and conversion of fine glass particles to molten
slag reduces pollution by preventing escape of particulate from the
combustion chamber with the products of combustion.
While gaseous fuel is the preferred fuel, my novel co-axial burner
is also capable of including a further back-up or secondary
co-axial fuel supply conduit for an oil atomizer. This secondary
fuel supply conduit can be arranged co-axial within the auxiliary
fuel conduit and put into use when the primary auxiliary fuel
supply is exhausted or for some reason not operating. I have also
found that by positioning a conically shaped screen about the
auxiliary fuel supply conduit just below the burner, the screen
effectively shields the auxiliary fuel ignition point from the
stream of high velocity waste and primary air. The screen permits a
small fraction of air to penetrate to the root of the flame front
to assist in flame propagation through small eddy currents of air
which stabilize the auxiliary flame at its root.
I have also devised a novel air cooled separator which permits it
to function at a temperature sufficiently high to permit the
adherence thereto of glass particulate material for build-up and
drop-off as slag which is collected in the ash-sump. Further, I
have found that the cooling air can be advantageously discharged
from the bottom of the disc of the separator as what I term as
tertiary air. The tertiary air is jetted about the separator in a
direction complementary to the direction of the cyclone flow. This
tertiary air discharge enhances the rejection of passage of
particulate matter carried by the combustion gases by virtue of the
fact that a whirling air centrifugal effect is centrally created at
a point proximate the incinerators discharge vent.
BRIEF DESCRIPTION OF THE DRAWINGS
In drawings which illustrate various embodiments of my improvements
to incinerators,
FIG. 1 is a vertical section of the incinerator taken along line
I--I of FIG. 4,
FIG. 2 is a more detailed vertical section of a co-axial auxiliary
fuel conduit and outer comminuted waste and air supply conduit
which is similar to that shown in FIG. 1,
FIG. 3 is a more detailed vertical section of the separator shown
in FIG. 1, and
FIG. 4 which is illustrated on the same sheet of drawings as FIG.
2, is a plan view of the separator taken along the line IV--IV of
FIG. 1 which also shows in partial cut-away section the secondary
air inlet ports taken along lines A--A and B--B of FIG. 1.
DETAILED DESCRIPTION
Referring to FIG. 1, the incinerator 10 is generally cylindrical in
shape and has an inwardly tapering bottom portion. The incinerator
may be supported by any suitable means such as base frame 11. The
combustion chamber of the incinerator comprises primary combustion
chamber 12 and secondary combustion chamber 12a thereabove. A
centrally located discharge vent 13 is located at the top of the
incinerator. The upper portion of the incinerator is connected to
suitable chimney or flue means (not shown). Connected to the top of
the incinerator and extending downwardly into the combustion
chamber from the discharge vent 13 is separator 15.
The walls of the incinerator 10 are constructed from fire brick
inner wall 16, insulating block intermediate wall 17 and outer
metal wall and framework 18. A plenum 19 surrounds the incinerator
walls and is supplied with secondary air from an air pressure
supply source (not shown). The secondary air is fed tangentially
from plenum duct 20 through port 21 to thereby create a cyclone
effect within the plenum. Through heat exchange, the secondary air
is preheated and discharged into the combustion chamber through
secondary air inlet ports 22 as seen in FIGS. 1 and 4. Flame nozzle
23 is provided and extends through the walls of the incinerator in
the secondary combustion chamber 12a. Incoming fuel for flame
nozzle 23 is advantageously mixed with air withdrawn from the
plenum through piping 24. Inspection or observation ports 25 and 26
are also provided in the walls of the incinerator.
The lower or bottom section of the incinerator is provided with a
vertically arranged and centrally located outer comminuted waste
and primary air supply conduit 27 which is in communication with
waste and primary air feed pipe 28 connected to a waste material
source and primary air pressure supply (not shown). Co-axial with
and internally positioned in supply conduit 27 is the primary
burner and auxiliary fuel supply conduit generally indicated at 29.
A water quenching bath is maintained below the upper end of supply
conduit 27 at 30, the level of which is regulated by a conventional
water level control device generally indicated at 31. Rejected
particulate material and slag collected in the water bath or
ash-sump is withdrawn therefrom in any conventional manner (not
shown). Access door 14 is provided for periodic maintenance and
repair.
Ignition of the burner portion of the auxiliary fuel supply conduit
29 is effected by means of a retractable high energy ignitor 32.
Flame scanner 33 is positioned above the ignitor.
With reference to FIG. 2, outer supply conduit 27 is preferably
provided with ribs or baffles 34, the function of which is to
impart to the waste fuel and primary air passing through annular
passage 35 a whirling effect in order to facilitate proper
intermixing of primary air with the waste fuel and to shape the
resulting flame. As illustrated in FIG. 2, supply conduit 27 is
flared at its discharge or termination end or it can be flared in a
uniform and outwardly tapering fashion as illustrated in FIG. 1.
Auxiliary fuel supply conduit 29 which is defined by inner and
outer walls 60 and 61 terminates within the outer conduit 27 so
that the auxiliary fuel issuing from first fuel discharge orifices
36 of the burner element portion 62 of conduit 29 are directed
radially outwardly towards the discharge end of the outer supply
conduit 27 as shown through the stream of waste fuel and primary
air. A perforated screen or shield 50 is provided on the
termination end of the supply conduit in order to enhance flame
propagation of the auxiliary fuel.
While my novel waste fuel and burner arrangement need only have one
conduit for the supply of auxiliary fuel, in the embodiment
illustrated, I have made provision for an additional and co-axially
arranged secondary fuel supply conduit 37. This secondary fuel
supply conduit communicates with secondary fuel discharge orifices
38 of burner 63 which is arranged internally of discharge orifices
36 of burner 62. As illustrated, gaseous fuel is intended to be
supplied through conduit 29 and liquid fuel such as oil through
conduit 37. Since gas is the preferred fuel, in normal operation,
conduit 37 and burner 63 are removed and the upper portion of wall
61 at burner 62 is capped by any suitable means. When conversion to
oil firing is desired or necessary, the cap which is not
illustrated is removed and conduit 37 and burner 63 are installed
in the annular cavity defined by wall 36 and positioned as
illustrated. Conduit 36 at its lower end is connected by suitable
means to an oil supply (not shown).
Referring again to FIG. 1, it will be seen that ignition of the
whirling waste fuel and primary air takes place at this point of
introduction into primary combustion chamber 12. Further combustion
takes place in secondary combustion chamber 12a through the added
introduction of secondary air through ports 22 and flame injection
from nozzle 23. As the products of combustion and particulate
material carried thereby proceed upwardly, they are constrained
through the positioning of disc 39 to move outwardly towards the
walls of the incinerator.
The separator itself is formed from refractory material and
basically comprises an annular manifold 41 surrounding discharge
vent 13. The manifold is connected to disc 39 by a series of
spaced, circumferentially arranged baffles 40. A series of
interconnecting conduits 42, 43 and 44 are provided in the
manifold, baffles and disc for the passage of tertiary air
therethrough which air effectively cools the separator and then is
advantageously discharged through tertiary air discharge orifices
47 into the combustion chamber in a tangential direction compatible
with the direction of the cyclone air flow. Preferably, conduits
42, 43 and 44 are constructed from a stainless steel framework
which serves as supporting members for baffles 40 and disc 39. As
seen in FIG. 4, the baffles preferably are V-shaped in
cross-section and include outer legs 45 which extend radially
outwardly from the disc. The inner legs 46 of the baffles are
located internally of the circumference of the disc and extend in a
direction opposite to the direction of tertiary air discharge
through orifices 47. The combined tertiary air discharge and baffle
construction is such that the likelihood of particulate matter
passing through the separator and thence through discharge vent 13
is minimized.
As illustrated in FIG. 1, inspection plate 48 is attached to the
top of disc 39 and can be removed during shut down in order to
permit interior inspection and repair to the combustion
chamber.
* * * * *