U.S. patent number 3,773,075 [Application Number 05/201,874] was granted by the patent office on 1973-11-20 for fuel burner assemblies.
This patent grant is currently assigned to Airoil Burner Company (GB) Limited. Invention is credited to David Ernest Howard, Reginald James Pearce, Michael Robert Thompson.
United States Patent |
3,773,075 |
Thompson , et al. |
November 20, 1973 |
FUEL BURNER ASSEMBLIES
Abstract
A fuel burner assembly of the venturi type having its fuel
nozzle provided with a plurality of jets and being more forwardly
disposed in relation to the venturi than is conventional in order
to reduce operating noise.
Inventors: |
Thompson; Michael Robert (West
Drayton, EN), Pearce; Reginald James (West Drayton,
EN), Howard; David Ernest (West Drayton,
EN) |
Assignee: |
Airoil Burner Company (GB)
Limited (West Drayton, Middlesex, EN)
|
Family
ID: |
10477545 |
Appl.
No.: |
05/201,874 |
Filed: |
November 24, 1971 |
Foreign Application Priority Data
|
|
|
|
|
Nov 30, 1970 [GB] |
|
|
56,788/70 |
|
Current U.S.
Class: |
137/890; 239/398;
431/114; 431/354 |
Current CPC
Class: |
F23D
14/64 (20130101); F23D 14/04 (20130101); F23D
91/02 (20150701); F23D 2206/0094 (20130101); F23D
2210/00 (20130101); F23D 2900/00011 (20130101); Y10T
137/87603 (20150401) |
Current International
Class: |
F23D
14/46 (20060101); F23D 21/00 (20060101); F23D
14/64 (20060101); F23D 14/04 (20060101); F16k
019/00 () |
Field of
Search: |
;137/604 ;48/18C
;431/114,354 ;417/179,312 ;239/398,416.4,416.5,417.3 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Nilson; Robert G.
Claims
We claim:
1. A burner assembly composed of a venturi and a fuel nozzle
arranged to discharge fuel into said venturi so that air will be
inspirated into the venturi, wherein the nozzle has a plurality of
jets through which said fuel is passed, the the distance between
the fuel-emitting end of the nozzle and the center of the venturi
throat is within the range of 0.5 to 1.5 venturi throat diameters,
and the inlet portion of the venturi facing the nozzle is formed as
a hollow member with an acoustic absorbing material within the
member.
2. An assembly according to claim 1, wherein the inner wall of the
inlet portion of the venturi is perforated.
Description
BACKGROUND TO THE INVENTION
The present invention relates in general to a fuel burner assembly
and has for its object the reduction of operating noise.
It is known to provide a burner assembly composed of a venturi and
fuel nozzle arranged to discharge fuel into said venturi so that
air will be inspirated into the venturi. The venturi may be of
various configurations, for example, the venturi may have a throat
in the form of a longitudinal section of constant minimum diameter
or else the venturi can converge to a point of minimum diameter
forming the throat.
SUMMARY OF THE INVENTION
In its broadest aspect, the invention is based upon the discovery
that by using a number of jets such as 4, 6 or more in the nozzle
and advancing the nozzle forwardly towards the venturi from the
position that it would normally adopt a significant reduction in
operating noise can be achieved.
According to the invention there is provided a burner assembly
composed of a venturi and a fuel nozzle arranged to discharge fuel
into said venturi so that air will be inspirated into the venturi,
wherein the nozzle has a plurality of jets through which said fuel
is passed and the distance between the fuel-emitting end of the
nozzle and the centre of the venturi throat is within the range 0.5
to 1.5 venturi throat diameters.
A further reduction in noise can be achieved by additionally
forming the inlet portion of the venturi facing the nozzle from a
hollow member filled with an acoustic damping material.
BRIEF DESCRIPTION OF DRAWINGS
The invention may be understood more readily from consideration of
the following description in conjunction with the accompanying
drawings, wherein:
FIG. 1 is a schematic sectional side view of part of a known fuel
burner assembly;
FIG. 2 is a part sectional side view of another known fuel burner
assembly employing an elbow venturi;
FIG. 3 is a diagrammatic and enlarged view of part of a fuel burner
assembly made in accordance with the invention and particularly
depicting the relative positions of the nozzle and venturi throat;
and
FIG. 4 is a schematic sectional side view of an alternative venturi
throat construction for use in an assembly made in accordance with
the invention.
DESCRIPTION OF PREFERRED EMBODIMENT
As shown in FIG. 1 a known burner assembly is composed of a fuel
nozzle 10 disposed in a casing 11 to which a venturi 12 is
attached. At the end of the venturi 12 remote from the casing 11
there is disposed a flame nozzle 13. In known manner the venturi 12
would be supported in the wall of a furnace so that a horizontally
disposed combustion flame is established by the nozzle 13 within
the furnace. Fuel, more usually gas is fed to the nozzle 10 and the
propulsion of the fuel from a single jet or orifice in the nozzle
10 serves to inspirate primary combustion air into the casing 11
from whence the fuel/air mixture passes through the throat 14 of
the venturi 12 for subsequent combustion.
In FIG. 2 a complete burner assembly employing an elbow venturi
instead of a straight venturi is shown and for convenience like
numerals denote like parts to FIG. 1. The operation of the assembly
of FIG. 2 is essentially as described in connection with FIG. 1 but
additionally illustrated in FIG. 2 are the walls 20 of a furnace, a
device 21 for adjusting the quantity of primary air, and a device
22 for adjusting the quantity of secondary air.
Assemblies of this general type are well known in this art. In
these prior art assemblies the end 31 of the nozzle 10 would either
be aligned with the outer surface 92 of the inlet flange 91 of the
venturi 12, as depicted by the dotted line in FIG. 1, or else this
end 31 would be disposed outwardly from the surface 92, i.e., to
the left of FIG. 1, as shown in the full lines in FIGS. 1 and 2.
Also in venturi type burners the nozzle 10 normally only has a
single central orifice or jet.
The present invention is based upon the somewhat surprising
discovery that by modifying the position of the nozzle 10 in
relation to the venturi 12 and by increasing the number of jets in
the nozzle 10 the burner will operate at a reduced noise level.
In general, it has been found that by displacing the nozzle 10
forwardly (arrow A FIG. 1) from the position which it normally
adopts, and by employing a plurality of jets in the nozzle 10
instead of a single jet an improvement in the noise characteristics
of the burner assembly of around 10 to 20 dBA can be achieved.
FIG. 3 depicts, in schematic form, a typical arrangement made in
accordance with the invention. In this case, in contrast to FIGS. 1
and 2, there are a number of jets 30 in the nozzle 10 and the
distance `x` between the end 31 of the nozzle 10 and a reference
point 50 in the venturi 12, conveniently taken as the centre of the
parallel throat section 14 of the venturi 12 is within the range
0.5 to 1.5 venturi throat diameters `d.` The dimension `d` can be
taken as the smallest internal diameter of the venturi 12. The
nozzle 10 has a plurality of jets 30 preferably exceeding four. The
collective area of such holes is equivalent to the area of a single
conventional jet and is chosen to match the particular fuel flow
rate in question.
The operating noise of the assembly can be further reduced by
modifying the inlet part 40 of the venturi 12 as shown in FIG. 4.
The inlet part 40 of the venturi 12 is formed from a hollow member
with a perforated inner wall 41 and an outer wall 42. A fibre-glass
material 43 or similar acoustic absorbing material is sandwiched
between the walls 41, 42.
* * * * *