U.S. patent number 3,819,318 [Application Number 05/354,132] was granted by the patent office on 1974-06-25 for pulsating combustors.
This patent grant is currently assigned to Babcock & Wilcox Limited. Invention is credited to Ronald Denzil Pearson.
United States Patent |
3,819,318 |
Pearson |
June 25, 1974 |
PULSATING COMBUSTORS
Abstract
A pulse combustion installation including a combustion chamber
closed at one end and provided with a neck at the other end with an
outlet duct extending therefrom. An inlet duct extending
convergently to the neck and being co-axial and partly coextensive
with the outlet duct at the neck. The inlet and outlet ducts and
combustion chamber being of such length as to produce resonant
conditions upon combustion of fluent fuel within the combustion
chamber.
Inventors: |
Pearson; Ronald Denzil
(Bathford, EN) |
Assignee: |
Babcock & Wilcox Limited
(London, EN)
|
Family
ID: |
23392000 |
Appl.
No.: |
05/354,132 |
Filed: |
April 24, 1973 |
Current U.S.
Class: |
431/1 |
Current CPC
Class: |
F23C
15/00 (20130101); F02G 3/00 (20130101) |
Current International
Class: |
F02G
3/00 (20060101); F23C 15/00 (20060101); F23c
003/02 () |
Field of
Search: |
;431/1 ;110/14
;60/39.77 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Favors; Edward G.
Attorney, Agent or Firm: Kemon, Palmer & Estabrook
Claims
What we claim is:
1. A pulse combustion installation including a tubular combustion
chamber closed at one end and formed with a neck at the other end,
a combustion gases outlet duct extending divergently from the neck
and co-axially therewith, a combustion air inlet duct extending
convergently to the neck co-axially and partly co-extensively with
the outlet duct at the neck, a transition region between the neck
and an entry portion of the inlet duct having an aerodynamically
unimpeded form relative to air flow toward the neck, means at the
neck substantially sharp edged in a direction toward the combustion
chamber interior arranged to cause a substantial contraction in the
cross-sectional area of gas flow stream out of the combustion
chamber compared with the cross-sectional area of gas flow stream
into the combustion chamber and an entry portion of the outlet duct
arranged to direct combustion gases discharged from the combustion
chamber to the outlet duct, the lengths of the inlet and outlet
duct and the combustion chamber being such as to produce resonant
conditions upon combustion of fluent fuel within the combustion
chamber.
2. A pulse combustion installation as claimed in claim 1, wherein
the junction of a wall of the combustion air inlet duct and a wall
of the tubular combustion chamber forms a flat sharp-edged orifice
at the neck.
3. A pulse combustion installation as claimed in claim 1, wherein
at the junction of a wall of the combustion air inlet duct and a
wall of the tubular combustion chamber the wall of the tubular
combustion chamber is directed toward the combustion chamber
interior such that a sharpedged re-entrant orifice is formed.
4. A pulse combustion installation as claimed in claim 2, wherein
the ratio of the cross-sectional area of the outlet duct at the
entry thereto perpendicular to gas flow in the duct to the
cross-sectional area of the sharp-edged flat or re-entrant orifice
is between 0.8 and 1.5.
5. A pulse combustion installation as claimed in claim 2 wherein
the ratio of the cross-sectional area of the sharp-edged flat or
re-entrant orifice to the crosssectional area of the outlet duct at
the entry thereto perpendicular to gas flow in the duct is
approximately 1.0 to 1.1 respectively.
6. A pulse combustion installation as claimed in any one of claim
2, wherein the ratio of the cross-sectional area of the sharp-edged
orifice to the cross-sectional area of the inlet duct at the neck
perpendicular to air flow in the duct is between 1.0 and 5.0.
7. A pulse combustion installation as claimed in claim 1 wherein
the angle between a discharge portion of the inlet duct immediately
adjacent the neck and the central axis of the outlet duct is
between 45.degree. and 60.degree..
8. A pulse combustion installation as claimed in claim 1, wherein
the angle between a discharge portion of the inlet duct immediately
adjacent the neck and the central axis of the outlet duct is
approximately 52.degree..
9. A pulse combustion installation as claimed in claim 1, wherein
the ratio of the length of a cylindrical duct acoustically
equivalent to the outlet duct to the length of a cylindrical duct
acoustically equivalent to the inlet duct is approximately 2.4.
10. A pulse combustion installation as claimed in claim 1, wherein
the ratio of the combustion chamber diameter of axial length is
between 1.0 and 2.0 and preferably 1.4.
11. A pulse combustion installation as claimed in claim 1, wherein
a helmholtz resonator means aligned with the entry portion of the
inlet duct is arranged to attenuate noise and recover part of the
resonant energy by being tuned to the fundamental frequency of
resonance.
12. A pulse combustion installation as claimed in claim 1, wherein
the inlet duct extends around and coaxially of the outlet duct.
13. A pulse combustion installation as claimed in claim 12, wherein
an axial passage is formed by radially extending webs intermediate
the adjacent walls of the inlet and outlet ducts for the forced
flow of air during establishment of combustion and resonant
conditions.
14. A pulse combustion installation as claimed in claim 1, wherein
the inlet duct is branched into passageways swept through
180.degree. to extend adjacent to the combustion chamber and
parallel to the axis thereof such that air flow at the entry is in
the same direction as the direction of flow of combustion gases in
the outlet duct.
15. A pulse combustion installation as claimed in claim 14 wherein
the inlet duct is branched into diametrically opposed pairs of
passageways of generally rectangular cross-section remote from the
entries thereto.
16. A pulse combustion installation as claimed in claim 15 wherein
each passageway of one pair of passageways extends over about
120.degree.-150.degree. of arc and each passageway of the other
pair of passageways extends over about 60.degree. to 30.degree. of
arc and is arranged to receive a forced flow of air during the
establishment of combustion and resonant conditions.
17. A pulse combustion installation as claimed in claim 15, wherein
entries to one pair of passageways are of re-entrant form and the
entries to the other pair of passageways are of bell-mouthed
form.
18. A pulse combustion installation as claimed in claim 1, wherein
a pressure jet atomising burner nozzle is positioned in the
combustion chamber for the supply of fuel thereto.
19. A pulse combustion installation as claimed in claim 1, wherein
the outlet duct is positioned within a combustion flue tube of a
water heating unit, and the combustion gases are arranged to flow
in heat exchange relationship with a body of water within the
unit.
20. A pulse combustion installation as claimed in claim 19, wherein
the combustion flue tube is provided with a closed end to form a
resonant cavity to attenuate noise and assist recovery of resonant
energy.
Description
This invention relates to a pulse combustion installation and, more
particularly, to a pulse combustion installation dispensing with
mechanical valves in the combustion air supply and relying on
resonant conditions to induce the flow of combustion gases through
the installations.
According to the present invention there is provided a pulse
combustion installation including a tubular combustion chamber
closed at one end and formed with a neck at the other end, a
combustion gases outlet duct extending divergently from the neck
and co-axially therewith, a combustion air inlet duct extending
convergently to the neck co-axially and partly co-extensively with
the outlet duct at the neck, a transition region between the neck
and an entry portion of the inlet duct having an aerodynamically
unimpeded form relative to air flow toward the neck, means at the
neck substantially sharp edged in a direction toward the combustion
chamber interior arranged to cause a substantial contraction in the
cross-sectional area of gas flow stream out of the combustion
chamber compared with the cross-sectional area of gas flow stream
into the combustion chamber and an entry portion of the outlet duct
arranged to direct combustion gases discharged from the combustion
chamber to the outlet duct, the lengths of the inlet and outlet
duct and the combustion chamber being such as to produce resonant
conditions upon combustion of fluent fuel within the combustion
chamber.
The invention will now be described, by way of example, with
reference to the accompanying, partly diagrammatic drawings, in
which:
FIG. 1 is a longitudinal cross-section of a pulse combustor;
FIG. 2 is a cross-section of the pulse combustor taken at the line
II--II of FIG. 1;
FIG. 3 is a longitudinal cross-section of an alternative form of
pulse combustor; and
FIG. 4 is a cross-section of the alternative form of combustor
taken at the line IV--IV of FIG. 3.
Referring to FIGS. 1 and 2 of the drawings, a cylindrical
combustion chamber 2 is formed with a reentrant neck 4 having an
outer wall 6 of frusto-conical form of an inlet duct 8 diverging
smoothly therefrom. A wall 10 of an outlet duct 12 -- which forms
in conjunction with an inner wall 14 of the inlet duct a water
jacket 16 -- extends co-axially within and beyond the inlet duct
walls 6 and 14 of the neck to form a cylindrical inlet gap 22. The
intake end 24 of the inlet duct outer wall 6 is formed with an
outwardly directed lip 26 which co-acts with a blanked-off
frusto-conical sleeve 28 aligned with the inlet duct 8 to form an
aerodynamic valve enhancing the inflow and inhibiting the outflow
of air to and from the inlet duct. Alternatively, an inwardly
directed lip may be provided to the same purpose.
Two pairs of axial baffles 30 are positioned between the inner and
outer walls 6 and 14 of the inlet duct from adjacent the lip 26 to
adjacent the cylindrical inlet gap 22 to form ducts 31 of
cross-sectional area together approximating to 1/5 of the total
cross-sectional flow area and the discharge outlet from a forced
draft fan 32 is connected to supply air to the ducts for starting
purposes.
A pressure jet atomising burner nozzle 34 giving an 80.degree.
spray cone is positioned within the combustion chamber 2 adjacent
the front end wall 36 thereof, the associated burner barrel 38
extending through the wall together with ignition and
instrumentation probes 40 and 42.
A valve 44 is provided in the fuel circuit to admit fuel
temporarily during start-up. Since the time-average pressure in the
combustion chamber 2 rises upon successful ignition a pressure
tapping is provided by the instrumentation probe 42 and connected
to a pressure sensing device actuating a valve 46 in the fuel
supply to provide a fuel flow upon ignition. A main shut-off valve
(not shown) is also provided. The valve 44 is subsequently closed.
The fuel system herein described causes fuel to be shut off if for
any reason there is a cessation of combustion.
The outlet duct discharges to a water heating unit (not shown)
which may take various forms for example a unit with smoke tubes
extending helically around the outlet duct axis within a water
space of annular cross-section between a cylindrical flue and a
cylindrical vessel, or one with annular cross-section smoke ducts
alternating with water ways within a cylindrical vessel.
In operation, to initiate start-up, air is supplied from a forced
draft fan 32 along the ducts 31 in the inlet duct 8 and circulates
in the combustion chamber 2. Fuel is supplied at a low rate to the
chamber and ignited to heat the walls of the chamber until the
temperature within the chamber is such that a steady resonant
condition arises. Upon this condition arising, the rate of fuel
supply is increased to the required operating flow and the forced
draught fan 32 de-energised and the combustion process becomes
self-sustaining.
The blanked-off frusto-conical sleeve 28 serves as a reflector to
attenuate sound at the inlet duct, whilst sound at the outlet is
attenuated by virtue of provision of a reflector in conjunction
with the outlet from the outlet duct and the extended length of the
flue gas path within the water heating unit.
Since the successful operation of the combustion process depends
upon the sustained resonant vibrations, the fuel supply to the
burner head may be, with advantage, pulsated in phase with the
vibrations either mechanically or by a physical connection between
the combustion chamber and the fuel supply line at a pressure only
slightly in excess of supply pressure.
From theoretical considerations in conjunction with experimental
results it would appear that for an arrangement in which the
combustion chamber is formed with a flat sharp-edged orifice (as
shown in FIG. 1) or a re-entrant orifice 54 subtending about
15.degree. to the central axis (as shown in FIG. 3) the following
proportions should be utilised.
1. Ratio of the cross-sectional area of the outlet duct 12 at the
entry thereto, perpendicular to gas flow in the duct, to the
cross-sectional area of the orifice 48, should be between 0.8 and
1.5 preferably approximately 1.0 for a sharp-edged orifice and
approximately 1.1 for a re-entrant orifice.
2. Ratio of the cross-sectional area of the inlet duct 8 at the
inlet end 24 perpendicular to air flow in the duct, to the
cross-sectional area of the orifice 48, should be between 1.0 and
5, preferably approximately 2.4.
3. Angle between discharge portion of the inlet duct 8 adjacent the
neck 4 and the central axis of the outlet duct 12 should be between
45.degree. and 60.degree., preferably approximately 52.degree..
4. Ratio of the equivalent length of outlet duct 12 to the
equivalent length of the inlet duct 8 should be approximately 2.4,
these lengths being the lengths of cylindrical ducts of equal inlet
area acoustically equivalent to the actual ducts.
5. Ratio of combustion chamber diameter to length between 1 and 2,
preferably approximately 1.4.
In the alternative arrangement shown in FIGS. 3 and 4 a cylindrical
combustion chamber 52 is formed with a re-entrant neck 54 having an
adjacent end portion 56 of frusto-conical form of a wall 58 of an
inlet duct 60 diverging smoothly therefrom. A wall 62 of
frusto-conical form of an outlet duct 64 extends from an inner wall
66 of the inlet duct 60 co-axially of the combustion chamber 52, an
end portion adjacent the neck 54 co-acting with an edge portion of
the neck to form a cylindrical inlet gap 68. Adjacent the
cylindrical inlet gap 68, the inlet duct 60 divides into two pairs
of passageways 70, 72 each of generally rectangular cross-section,
one pair 70, disposed symmetrically to either side of the
horizontal plane, each extending over approximately 150.degree. to
120.degree. of arc of the cylindrical inlet gap and the other pair
72, disposed symmetrically to either side of the vertical plane,
each extending over approximately 30.degree. to 60.degree. of arc.
Each of the passageways 70, 72 is smoothly swept through
180.degree. to extend forwardly parallel to the combustion chamber
axis and diverges to a circular cross-section intake portion 74,
76. The intake portions 74 of the horizontal pair 70 are formed
with bell-mouth inlets 78 whilst the intake portions of the
vertical pair 72 are formed with re-entrant inlets 80. The inlets
are positioned within a windbox 82 adjacent the front of the
combustion chamber and each has a helmholtz resonator 84, 86
aligned therewith tuned to the fundamental frequency of resonance
for noise attenuation and recovery of part of the resonant energy.
The resonators aligned with the respective pairs of passageways may
be interconnected to enhance performance thereof. An impeller fan
88 is positioned in the windbox to deliver air through ducts to the
inlets of the vertical pair of passageways for start-up purposes.
Air is supplied to the windbox through a rearwardly extending
intake 90 of venturi form having a bell-mouthed inlet.
A pressure jet atomising burner nozzle 92 giving an 80.degree.
spray cone is positioned within the combustion chamber adjacent the
front end wall thereof, the associated burner barrel 94 extending
through the windbox together with instrumentation and ignition
probes 96, 98.
A valve 100 is connected in the burner oil fuel supply line 102 and
is actuated initially by a starting device (not shown) which opens
it and then by a signal, which maintains it open, derived from a
pressure tapping in the combustion chamber. A main shut-off valve
(not shown) is also provided.
As in the arrangement described previously, the outlet duct 64
discharges to a water heating unit of the form described. However,
since the passageways 70, 72 of the inlet duct are swept through
180.degree. to a windbox at the front of the combustion chamber,
more satisfactory attenuation of noise may be achieved by providing
a reflector space within the flue tube. The re-entrant inlets 80 to
the vertical pair of passageways 72 restrict flow of combustion
gases to those passageways, so that on the intake portion of the
sequence, unburnt air is immediately drawn into the combustion
chamber.
In operation, to initiate start-up, air is supplied from the fan
impeller along the vertical passageways of the inlet duct and
circulates in the combustion chamber. Fuel is supplied at a low
rate to the chamber and ignited to heat the walls of the chamber
until the temperature within the chamber is such that a steady
resonant condition arises. Upon this condition arising, the rate of
fuel supply is increased to the required operating flow and the fan
impeller de-energised and combustion process becomes
self-sustaining.
* * * * *