[0001] The present invention relates to burners, and relates particularly but not exclusively
to oxygen-fuel burners requiring cooling during operation.
[0002] One well known kind of oxygen-fuel burner comprises a central passage for oxygen
surrounded by an inner, annular, passage for the fuel, and an outer, annular, passage
for the air. The distal end of each passage terminates at an endplate. The endplate
is formed with a first ring of orifices that co-operate with the outer annular passage,
a second ring of orifices that co-operate with the inner annular passage and a third
group of orifices that co-operate with the central passage. The central passage is
typically used for the supply of oxygen. In order to ensure that there is a good mix
of oxygen with fuel, the third group of orifices are so designed that, provided the
oxygen velocity is sufficient the oxygen exits as turbulent jets which readily mix
with the other fluids. The endplate is typically a complex and expensive part to manufacture.
Since the endplate of the burner is typically subject to hostile conditions, coming
into contact with hot and frequently corrosive atmospheres, it is desirable to make
the endplate as resistant to erosion as possible. One way of overcoming the erosion
problem is to make the endplate of a hard heat resistant metal alloy. Unfortunately,
this adds to the cost of the endplate and hence the burner. Even though a hard heat
resistant metal alloy is used, the burner may have a relatively short life if used
in particularly severe conditions.
[0003] It is an object of the present invention to provide an oxygen-fuel burner which reduces
and possibly eliminates the problems of erosion associated with the above mentioned
burner.
[0004] According to the present invention there is provided an oxygen-fuel burner comprising
a hollow body member extending along a first axis towards an endplate at a distal
end and defining a passage through which extend a plurality of oxygen and fuel ducts,
at least one of each of said ducts passing through said endplate so as to allow oxygen
and fuel to issue from the burner, and directing means for directing fuel and/or oxygen
to impinge on an inside surface of said endplate prior to issuing from said burner
thereby to cool said endplate and preheat said fuel and/or oxygen.
[0005] Advantageously, the burner includes turbulence generating means for causing said
fuel and/or oxygen to pass through the burner in a turbulent manner thereby to increase
the rate of heat transfer thereto.
[0006] In a particularly useful arrangement, the burner includes heat exchangers extending
between said oxygen and fuel ducts for transferring heat therebetween.
[0007] Conveniently, the oxygen or fuel ducts extend straight through said burner between
holes in said proximal and distal ends of said burner.
[0008] In a simple arrangement, the oxygen supply duct includes a wall portion formed by
at least a portion of the fuel supply duct.
[0009] Advantageously, the oxygen duct or the fuel duct is positioned for returning whichever
of said oxygen or fuel component is directed at the distal endplate back towards the
proximal end of said burner for eventual discharge therefrom.
[0010] Conveniently, the oxygen and fuel ducts are co-axial with each other.
[0011] Advantageously, the burner includes a plurality of said oxygen and fuel ducts circumferentially
and radially spaced around said central axis x.
[0012] In a particularly advantageous arrangement, the burner includes valve means associated
with at least one of each of said oxygen and fuel ducts and for controlling the supply
of oxygen and/or fuel for the purpose of creating fuel or oxygen rich portions of
flame downstream of said burner.
[0013] In a preferred arrangement, the oxygen duct passes straight through said burner and
said fuel duct is positioned for directing fuel to impinge on the inside surface of
said endplate prior to issuing from said burner.
[0014] The present invention will now be more particularly described by way of example only
with reference to the accompanying drawings, in which:
Figure 1 is a cross-sectional longitudinal elevation of the burner;
Figure 2 is a cross-sectional view taken in the direction of arrows A-A in Figure
1;
Figure 3 is a side elevation of the burner shown in Figures 1 and 2; and
Figure 4 illustrates an alternative flow arrangement.
[0015] Referring now to Figure 1, the burner 10 comprises a hollow body portion formed by
casing 12 which extends along a first axis x towards an endplate 14 at a distal end
12a and defines a passage 16 through which extend a plurality of oxygen and fuel ducts
18 and 20 respectively. In the particular embodiment illustrated in Figures 1 and
2 the oxygen ducts 18 are illustrated as extending straight through the burner 10
between holes 22, 24 provided at the proximal and distal ends respectively. The fuel
ducts are illustrated as being formed to direct fuel down-up-down the burner passage
16 in a manner which allows the comparatively cool fuel to impinge on the inner surface
14a of endplate 14 before being passed out of the burner. Such an arrangement has
the advantage of using a comparatively high mass flow fluid to draw heat from the
vulnerable endplate thereby cooling the endplate and heating the fuel so as to both
prolong the life of the endplate and increase the temperature if the fuel prior to
a more efficient than normal combustion step. The endplate may have any edges radiused
so as to minimise the surface area to volume ratio and hence reduce stresses and burn-back.
It will be appreciated that one could reverse the flows such that the oxygen supply
is directed so as to impinge on the endplate for the purpose of cooling it and the
fuel passes straight through the burner. However, in practice it would be most beneficial
to use the fluid having the higher mass flow as the cooling fluid and hence, in most
applications, the fuel would be used for cooling purposes. For this reason Figures
1 and 2 are illustrative of the arrangement in which fuel is used for cooling purposes,
however, both arrangements are considered to fall with the scope of the present invention.
For the purpose of brevity, the remainder of the description will refer only to the
arrangement in which fuel is used for cooling.
[0016] Referring now to both figures, it will be appreciated that fuel F enters the burner
via inlet 26 and into an upper region 26a of annular duct 28. Fuel flows both around
the duct 28a to the far side thereof and down the duct in the direction of arrows
D in Figure 1. As fuel reaches the lower region 28b of duct 28 it is forced to impinge
on the inner surface 14a of the endplate thereby to cool the endplate and heat the
fuel F. Fuel is returned to the upper region 28a via return portion 28c. As fuel passes
along portion 28c it is free to move radially inwards in the direction of arrows R
and pass over and around the outer surface 30a of oxygen ducts 18 thereby transferring
heat to said duct 18 and hence heating any oxygen passing therethrough. Returning
fuel is directed down an inner portion 28d of the fuel duct prior to issuing from
the burner adjacent oxygen outlets 32.
[0017] Whilst Figure 2 illustrates just two oxygen ducts 18 passing through the burner,
it will be appreciated that many more could be used. Indeed a plurality of such ducts
could be circumferentially and radially spaced around the burner in a manner which
will readily present itself to those skilled in the art and therefore not detailed
herein.
[0018] Further features of the burner 10 include turbulence generators and heat exchangers
shown at 36 and 38 respectively. The turbulence generators 36 act to ensure the fuel
flow is turbulent thereby facilitating a greater heat transfer rate than is available
with laminar flow. The heat exchangers are positioned in the returning fuel flow and
are linked to the oxygen duct so as to increase the effective area available for heat
transfer. If practical, the heat exchanges 38 may be provided on both sides of the
various walls defining the ducts and may also form support elements.
[0019] From Figure 3, it will be seen that valves 40, 42 may be employed to control the
flow of oxygen and/or fuel through the burner 10. Such control would be of benefit
when the burner 10 is used in applications in which it is desirable to produce zones
which are fuel and/or oxygen rich and thereby effectively alter the flame profile.
[0020] Figure 4 illustrates an arrangement in which the annular fuel supply duct 20 is replaced
with a plurality of ducts 20a. Fuel entering the ducts 20a is directed at various
points around the endplate 14, thereby acting to cool it in the manner already described,
before flowing in the direction of arrows R towards upper region 26a where it enters
the central fuel supply duct 28d as previously described. This arrangement has the
advantage of being able to direct cooling fluid at selected vulnerable endplate positions.
1. An oxygen-fuel burner (10) characterised by a hollow body member (12) extending along
a first axis (x) towards an endplate (14) at a distal end (12a) and defining a passage
(16) through which extend a plurality of oxygen and fuel ducts (18, 20), at least
one of each of said ducts (18, 20) passing through said endplate (14) so as to allow
oxygen and fuel to issue from the burner (10) and directing means for directing fuel
and/or oxygen to impinge on an inside surface of said endplate prior to issuing from
said burner thereby to cool said endplate and preheat said fuel and/or oxygen.
2. A burner (10) as claimed in Claim 1 characterised by turbulence generating means (36)
for causing said fuel and/or oxygen to pass through the burner (10) in a turbulent
manner thereby to increase the rate of heat transfer thereto.
3. A burner (10) as claimed in Claim 1 or Claim 2 characterised by heat exchanges (38)
extending between said oxygen and fuel ducts for transferring heat therebetween.
4. A burner (10) as claimed in any one of Claims 1 to 3 characterised in that said oxygen
or fuel ducts (18, 20) extend straight through said burner (10) between holes (22,
24) in said proximal and distal ends of said burner (10).
5. A burner (10) as claimed in any one of Claims 1 to 4 characterised in that said oxygen
supply duct (18) includes a wall portion formed by at least a portion of the fuel
supply duct (20).
6. A burner (10) as claimed in any one of the Claims 1 to 5 characterised in that the
oxygen duct (18) or the fuel duct (20) is positioned for returning whichever of said
oxygen or fuel component is directed at the distal endplate back towards the proximal
end of said burner for eventual discharge therefrom.
7. A burner (10) as claimed in any one of Claims 1 to 6 characterised in that said oxygen
and fuel ducts (18, 20) are co-axial with each other.
8. A burner (10) as claimed in any one of Claims 1 to 7 characterised by a plurality
of said oxygen and fuel ducts (18, 20) circumferentially and radially spaced around
said central axis x.
9. A burner (10) as claimed in any one of the preceding claims characterised by valve
means (40) associated with at least one of each of said oxygen and fuel ducts and
for controlling the supply of oxygen and/or fuel for the purpose of creating fuel
or oxygen rich portions of flame downstream of said burner.
10. A burner (10) as claimed in any one of the preceding claims characterised in that
the oxygen duct (18) passes straight through said burner (10) and said fuel duct (20)
is positioned for directing fuel to impinge on the inside surface of said endplate
(14) prior to issuing from said burner (10).