US3897198A

US3897198A - Gaseous fuel burners

Info

Publication number: US3897198A
Application number: US350780A
Authority: US
Inventors: Alfred Longworth
Original assignee: Radiation Ltd
Current assignee: Radiation Ltd
Priority date: 1972-04-17
Filing date: 1973-04-13
Publication date: 1975-07-29
Anticipated expiration: 1992-07-29
Also published as: NL168605C; NL7305234A; FR2199853A5; JPS4920727A; JPS5332540B2; NL168605B; IT980235B; ES413765A1; DE2318658C2; DE2318658A1

Abstract

A gaseous fuel mixture burner has a gaseous fuel diffuser mounted in the outlet of the burner. The diffuser provides a multiplicity of ports at which the fuel mixture burns once ignited. Through the diffuser extends a path through which a cooling fluid is circulated. Used in conjunction with the burner to provide the gaseous fuel mixture is a mixer device into which gas is injected so as to provide a gaseous vortex formation within the mixer, air being drawn into the device and mixed with the gas by the low pressure region created within the vortex.

Description

United States Patent [191 Longworth [4 1 July 29,1975

[ 1 GASEOUS FUEL BURNERS [75] Inventor: Alfred Lngworth,Wembley,

- England [73] Assignee: Radiation Limited, London,

England [22] Filed: Apr. 13, 1973 [21] Appl. No.: 350,780

[56] References Cited UNITED STATES PATENTS 1,357,493 11/1920 Foster 122/367 R United Kingdom 122/367 United Kingdom 122/367 Primary Examirter.lohn J. Camby Assistant Exam'in'erl-lenry C. Yuen Attorney, Agent, or Firm-Brisebois & Kruger [57] g ABSTRACT A gaseous fuel mixture burner has a gaseous fuel diffuser mounted in the outlet of the burner. The diffuser provides a multiplicity of ports at which the fuel mix: ture burns once ignited. Through the diffuser extends a path through which a cooling fluid is circulated. Used in conjunction with the burner to provide the gaseous fuel mixture is a mixer device into which gas is injected so as to provide a gaseous vortex formation within the mixer, air being drawn into the device and 3,368,547 2/1968 Hale 126/350 R mixed with the gas by the low pressure region created 3,385,356 5/l968 Dalin 122/367 R within the vortex. 3,685,740 8/1972 Shepherd 239/1323 FOREIGN PATENTS OR APPLICATIONS 9 Claims, Drawing Figures 634,011 8/1936 Germany 126/350 R --,JL -:J 2 7 PATENTED JUL 2 9 I975 SHEET GASEOUS FUEL BURNERS This invention relates to gaseous fuel burners that is to say burners in which the fuel is burnt in gaseous form although the fuel may be stored in liquid or gaseous form. The invention also has particular but not exclusive reference to gaseous fuel burners for gas-fired water heaters which term is intended to include the socalled instantaneous water heaters and the heating units, usually referred to as boilers, incorporated in gasfired central heating systems.

One of the factors affecting the overall height of gasfired water heaters is the flame height of the flames of the burner used in the appliance. A reduction in flame height usually involves an increase in the number of burner flames in order to maintain the thermal output of the burner and this leads to an increase in the plan area of the burner. If an attempt is made to reduce the plan area by reducing the spacing between individual flames aeration problems arise and there is also a tendency for the burner body to overheat and this leads to the development of high back pressure, high burn down and the increased possibility of light back. The aeration problem can be dealt with by increasing the supply of primary air but the other problems remain and become acute as the plan area of the burner is reduced.

It is an object of the present invention to provide a gaseous fuel burner in which the remaining problems discussed above are less acute.

According to the present invention, a gaseous fuel burner comprises a duct for carrying a combustible gaseous fuel mixture to a burner outlet comprising a diffuser head for diffusing the mixture, the head having a path therethrough for the circulation of a cooling fluid.

The diffuser head is adapted to provide the large number of flame ports necessary to secure a desired flame height at a specified thermal rating. The diffuser head may comprise an assembly of finned pipes, the spaces between the fins and the pipes constituting the flame ports. Alternatively, the diffuser head may comprise a porous metallic structure through which conduits pass to convey the cooling fluid. The structure has a plurality of apertures that constitute the flame ports. The diffuser head may be a double-walled structure having a multiplicity of transverse fuel passageways, coolant being circulated between the double walls.

Preferably, there is located in the duct a mixer device comprising a hollow open-ended vessel having a longitudinal axis and an arrangement including one or more orifices for a combustible gas, the or each orifice being positioned so as to permit entry of the gas into the vessel between the open ends thereof, and in which the arrangement is such as to impart a helical motion to the gas about the longitudinal axis with a component of motion directed towards the burner outlet, the helical motion creating a vortex within the vessel with a low pressure zone in the vicinity of the axis, the zone enabling the entry of air into the vessel for intimate mixing with the combustible gas.

The mixer device may include an arrangement comprising a number of fuel supply pipes each of which passes into the vessel through the wall thereof, each pipe having at least one of the orifices formed in it.

Another form of mixer device includes two parts that have mating surfaces, the orifices being formed between the surfaces. ln such a construction there may be included a further, resilient part that is mounted between the two parts in such manner that rate of flow of fuel through the orifices is determined by the degree of compression of the further part, and in which the two parts are adjustable in position relatively to one another in order to vary the degree of compression of the further part.

The internal contour of the vessel may be of venturi form, the longitudinal axis of the vessel corresponding with that of the venturi. The orifices may be positioned at the throat of the venturi.

The gaseous fuel burner may include a burner head with an inlet adapted to receive the output of the mixer device and so arranged relatively thereto in such manner that further air is entrained in the output of the mixer device as that output enters the burner head inlet.

The burner may have several such inlets each fed from a separate mixer device.

Alternatively, the duct may be fitted to a mixer in which combustible gas is mixed with air supplied by a blower, fan or other powered device, or a mixer in which the flow of air is induced by means of an exhaust fan or similar mechanism.

It will be appreciated that the diffuser head constitutes a heat exchanger, heat being extracted from the diffuser head by the fluid, for example water, circulated therethrough.

The circulatory path may be joined to a further heat exchanger located above the burner.

In one particular embodiment, the burner may form part of a heat exchanger assembly for a gas-fired water heater, the assembly including the further heat exchanger which is located in close proximity to, and above, the diffuser head so as to define therewith, at least partially, a gaseous fuel mixture combustion zone.

In the case of the water heater, the diffuser head is water cooled and the circulatory path forms part of the water heating circuit of the water heater.

The invention also provides a mixer device comprising an open-ended cylindrical mixing chamber and means at or adjacent one end of the chamber for inspirating one of the fluids into the chamber, the means comprising a supply header for the other fluid, the header being of generally annular form and having a surface coaxial with the longitudinal axis of the chamber and facing the other end of the mixing chamber, and a series of orifices in the surface and in communication with the interior of the header, the orifices being so arranged that, in use, fluid entering the chamber from the orifices has imparted to it a helical motion about the longitudinal axis and directed towards the other end of the chamber, the arrangement being such that, in use, the one fluid is drawn into the chamber through and externally of the supply header.

The mixer device just defined is not restricted to use with gaseous fuel burners and may be used for mixing fluids other than gaseous fuel and air.

The supply header may be positioned coaxially within the mixing chamber, the arrangement being such that there is formed an annular passageway between the header and the chamber for the entry into the latter of fluid drawn externally of the header. Alternatively, the supply header may be received in the one end of the mixing chamber, the curved wall of the latter being gapped or formed with holes at locations close to the orifices to permit the entry into the latter of fluid drawn externally of the header.

The supply header may comprise inner and outer tubular members nested together to form the header. At one end the members have surfaces which coact to provide the orifices in the end surface. Either inner or outer member may have a shoulder grooved on its outer or inner face respectively and which co-operates with a plain face on the other member to form the orifices.

By way of example only, gaseous fuel burners embodying the invention, mixer devices for use therewith, and a heat exchanger assembly incorporating the burner and suitable for a gas-fired water heater will now be described in greater detail with reference to the accompanying drawings of which:

FIG. 1 is a section through a burner and mixer assemy,

FIG. 2 shows the heat exchanger assembly and burner assembly in diagrammatic form only and partly in section,

FIG. 3 is a section on the line IIIIII of FIG. 2,

FIG. 4 is a horizontal transverse section through a different form of mixer device,

FIG. 5 shows in diagrammatic form only part of another gaseous fuel burner embodying the invention,

FIG. 6 is a plan view of another form of mixer device,

FIG. 7 is a section on the line VII-VII of FIG. 6,

FIG. 8 is a plan view of a component of the embodiment shown in FIG. 6,

FIG. 9 is a section on the line IX-IX of FIG. 8,

FIG. 10 is a plan view of yet another form of mixer device,

FIG. 11 is a section on the line XI-XI of FIG. 10,

FIG. 12 is a plan view of an alternative form of one of the components of the mixer device,

FIG. 13 is a section on the line XIII--XIII of FIG. 12, and

FIGS. 14 and 15 are side elevations of further gaseous fuel burners embodying the invention and incorporating mixer devices.

The burner and mixer assembly shown in FIG. 1 has a gas/air mixer 1 comprising an outlet member 2 and an inlet member 3. The bore of the member 2 has a diverging exit portion 4 and a cylindrical portion 5. The portion 5 is located within a cylindrical mounting element 6 having a circular opening 7 in its curved wall and is screw-threaded internally at 8 to receive the inlet member 3 which is appropriately screw-threaded. The inlet member 3 has a bore 9 which is flared downwardly and outwardly as shown.

The cylindrical bore portion 5 has a bevelled edge 10 and the inlet member has a mating bevelled edge 11. The bevelled edge 11 has grooves 12 in it. Each groove has one wall which lies along a line which is tangential to the portion 5 while the other wall lies at an angle of about 15 to the tangential wall. In addition, the bevelled surface 10 is upwardly inclined at an angle of about 50 to the horizontal.

The cylindrical bore portion 5 is recessed to receive a ring 13 with sharply bevelled ends and slightly oversize lengthwise so that when the inlet member 3 is screwed into the outlet member 2 slight deformation of the ring 13 takes place and fluid tight joints are obtained between the ring 13 and the inlet and

outlet members

3,2. the grooves 12 are sufficiently deep to ensure that the deformation of the ring does not result in objectionable blockage of the grooves 12.

Secured in the opening 7 is a supply pipe 14 whose function will be described later.

The outlet member 2 is telescopically engaged with the cylindrical extension 15 of a diffuser cone 16 which forms the burner mouth and which is contoured at 17 to receive a diffuser head 18 through which passes a passageway 19 with an inlet 20 and an outlet 21 and which is part of a circulatory path for a cooling fluid.

The diffuser head may be a porous plug which has a multiplicity of passageways each providing a flame orifree in the outer surface of the diffuser head.

In use, the supply pipe 14 is joined to a source of combustible gas whilst the inlet member 3 is open to the atmosphere. Gas entering pipe 14 passes through the circular opening 7 and flows through grooves 12 which impart to the streams flowing through them a helical motion which produces within the bore of the outlet member 2 a vortex having an upward component of motion towards the diffuser head 18. The creation of the vortex produces a low pressure region in the vicinity of the axis of the vortex and this induces a flow of air into the mixer device via the open end of the inlet member 3. The air becomes entrained with the streams of gas entering via grooves 12 and becomes thoroughly mixed therewith. A degree of turbulence is also created inside the bore which contributes to effective mixing.

The mixed gas-air fuel enters the cone l6 and spreads out to follow the contour of the latter and after passage through the diffuser head 18 is ignited to burn on the surface thereof in a multiplicity of flames of very low profile.

The dimension of the mixer device 1 and the gas pressure are such that the volumes of air and gas are at least in the appropriate stoichiometric ratio so that sufficient air is available for effective combustion.

The cooling of the diffuser head eliminates the transfer of heat from the burner flames to the cone l6 and any adjacent structure as well as to gaseous fuel moving upwards towards the diffuser and the temperature of the fuel is limited to a value at which light back does not occur. In addition, back pressure is reduced and burn down is eliminated. Reduction of back pressure allows adequate aeration of the gas to be maintained.

It will be appreciated that air necessary for effective combustion is all supplied as primary air and no secondary aeration of the flames is necessary. This implies that the flame height can be minimised and there is no flame mantle. Small flame height enhances cross lighting during ignition and also reduces ignition noises.

FIG. 2 shows a burner embodying the invention incorporated in a heat exchanger assembly for a gas-fired water heater.

The assembly includes a gas burner having a mixer device 22 of the construction described above which is joined by a mouthpiece 22a, to a diffuser cone 23 which forms the burner outlet and is contoured as at 24 to receive a diffuser which, in this embodiment, is in the form of a series of finned pipes 25 which lie in parallel, side-by-side relationship in a common plane as is apparent from FIGS. 2 and 3. The pipes have fins which do not extend very far from the pipe surface. In this way, the pipes are close together, and the maximum fin temperature is never greatly in excess of the temperature of the cooling fluid-water which flows through the pipes when the burner is operating. The ends of the pipes terminate in

headers

26, 27 there being an outlet 28 from header 27 and a connector 29 which joins header 26 to one end of a finned pipe 30. The pipe 30 is one of a second series of parallel, side-by-side pipes which together form the heat exchanger 31 of the assembly. The second series of pipes lies above and in close proximity to the pipes in the burner mouth being separated from the latter pipes by a space 32 which constitutes a combustion zone. The second series of pipes has a water inlet 33.

Located above the heat exchanger 31 is an exhaust cone 34 through which combustion products pass to atmosphere.

The construction so far described operates in the following manner. Combustible gas is fed into the mixer device 22 via entry pipe 35 in the manner explained above end the resulting air/gas mixture passes through the diffuser head via the flame ports formed between the fins and pipes of the diffuser head and burns in the combustion zone 32 with extremely short flames. The finned pipes such as pipe 25 extract heat partly by radiation and partly by conduction from the closely adjacent flames which, in effect, seat on the fins of the pipes.

The heat exchanger 31 extracts heat from the products of combustion which flow through the spaces between the finned pipes and is also heated by radiation from the closely adjacent flames.

The area of cooling surface provided in the heat exchanger 31 and in the diffuser head is such that condensation of combustion products and the resultant deleterious corrosion is avoided.

The heat exchanger assembly allows a greater proportion of radiant heat to be absorbed than in conventional water heaters and this reduces the air temperature in the vicinity of the combustion zone and the temperature of structures adjacent that zone and thus reradiation from such structures is very small. These factors all contribute to an easing of the problem of thermally insulating the casing for the heater and other components and there is greater freedom in positioning the heater controls.

It will be appreciated that the assembly shown in FIG. 2 has a small top-to-bottom dimension as compared with the equivalent assembly in a conventional water heater. The absence of a combustion chamber as such contributes greatly in this respect.

The components described above are put together to form a rigid assembly and this ensures alignment of the heat exchanger pipes with those of the diffuser and with the gaseous fuel supply conduit.

It is not essential that the mixer device be of generally cylindrical form as is the case with the mixer 1 described above. The cross-section of the mixer transverse to its length may be of elliptical or other form provided this does not militate against the setting up of the vortex referred to above.

In an alternative form of mixer suitable for use in a gaseous fuel burner, the gas is introduced at a point or points lying within the mixer. For example, a gas supply conduit having a plurality of orifices at its end is introduced into the inlet member 3 of the mixer device 1 described above and gas is introduced via the conduit and orifices instead of via the grooves 12. The orifices may be formed in one end wall of the conduit or in a head attached to the conduit. Each orifice emits a stream of gas and .because of the orientation of the orifices the streams are tangential to a circle drawn about the longitudinal axis of the mixer and are inclined towards the upper end thereof to produce the vortex configuration referred to above. The orifices are so located within the mixer that gas spillage from the lower end of the mixer does not occur. The actual position the orifices occupy along the axis of the mixer is effected by the vortex angle, the internal cross-sectional area of the mixer and the velocity at which the gas enters the mixer.

FIG. 4 shows alternative arrangements by means of which the gas may be introduced.

In FIG. 4, the mixer comprises a cylindrical tube 36 and, in one of the embodiments shown, a series of pipes 37 extend radially into the tube 36. Each pipe 37 has a closed end 38 and, adjacent that closed end, an orifree 39 orientated to direct gas into the tube 36 tangentially to a circle 40 lying inside the tube 36, and with an inclination towards the upper end of the tube through which the air/gas mixture exits to the burner. The pipes 37 need not occupy the diametricallyopposed systems shown in FIG. 3, although, in general, equal spacing of the pipes is advantageous. A smaller or greater number of pipes 37 can be used and they may have orifices tangential to circles of different radii and the orifices may occupy differential positions along the axis of the mixer.

FIG. 4 shows. in chain dotted lines, another position which the pipes might occupy. In this case only one pipe is shown and it projects through the wall of the tube 36 along a chord thereof and into the tube for a short distance. At its end, the pipe 41 has an orifice 42 in its end wall, the orifice being orientated to lie tangentially to the circle 40 or to some other circle lying inside the tube 36, the orifice also having the necessary inclination towards the relevant end of the tube 36. Several such pipes 41 will normally be used and they may direct fluid tangentially to circles of differing radii. Alternatively, the pipes 41 may themselves be inclined towards the axis of the tube 36. It will be understood that the pipes 41 need not project through the wall of the tube 36 and "into the interior thereof but could terminate at the wall, the orifices lying, in effect, in the in- I side face of the wall. However, by spacing the orifices improved mixing of gas and air is possible.

It will be appreciated that a combination of pipes 37 and 41 may be used and may occupy different positions along the axis of the tube.

It is not necessary that burner head and mixer device be in telescoped close-fitting engagement as in the embodiment described above with reference to FIG. 1. An

end-to-end fitting could be used or indeed, the burner and the mixer device may be spaced apart to permit entry of further primary air. Such an arrangement is shown in FIG. 5 in which only part of the burner is shown and the mixer device is shown as a block 42. The burner 43 has the general form described above with reference to FIG. 1, but the diffuser cone 44 is openended as shown with a flared or belled mouth 45 in which is located the upper end of the mixer device 42. The mixer device 42 operates in the manner of the mixer device described above, and the gas/air mixture leaving the device entrains further air as indicated by the arrows 46.

Other forms of mixer device will now be described with reference to FIGS. 6-13.

The embodiment shown in FIGS. 6-9 comprises an outer open-ended sleeve 51 within which is coaxially positioned an assembly 52 comprising inner and

outer members

53, 54 nested to form an internal annular space 55 access to which is provided by a radial extension 56 of the outer member 54. Secured, for example by screwing, to the extension 56 is a connector 57 which passes through an aperture in the wall of the sleeve 51 so enabling the assembly 52 to be attached to and located within the sleeve 51, the assembly being spaced from the sleeve by an annular gap 58.

The outer member 54 has a flange 59 at one end, the inner face 60 of the flange being formed to provide a series of grooves 61 that are inclined with respect to the axis of the member 54 by an angle lying within the range 3560 and preferably about 45. The other end of member 54 is contoured to fit closely the slightlybelled end of the inner member 53. The other end of the member 53 is sized to fit tightly against the face 60 of the flange 59. As can be seen from FIG. 7, the axial lengths of the

members

53 and 54 are equal so that with the members in the positions shown in FIG. 7, a series of orifices is formed in the end surface of the assembly 52 uppermost in FIG. 7.

The device shown in FIGS. 69 can be used to mix air and gas and the connector 57 is joined to a source of gas. In use, gas emerges from the orifices as a series of jets which, because of the inclination of the grooves 61, establish a vortex within the sleeve 51. The axis of the vortex coincides substantially with that of the assembly 52 and the region of low pressure within the vortex around that axis causes air to be drawn in through the inner member 53. The slightly converging internal configuration of the member 53 produces an increase in the velocity of the air so drawn in and this helps to maintain the generally upward movement of the air-gas flow.

In addition, air is drawn in through the annular passageway 58 and thus the jets of gas are in intimate contact with a central core of air entering via the inner member 53 and an outer sheath of air entering via the passageway 58. In this way a large volume of air is drawn into the upper part of the sleeve 51 and mixed effectively with the streams of gas.

In the embodiment shown in FIGS. and 11, there is included a sleeve 62 having a bore with a portion 63 of constant internal diameter and a second portion 64 whose bore diverges with increasing distance from portion 63. The lower (as seen in FIG. 11) end of the sleeve is stepped to receive one end of an assembly, similar to assembly 52 described above except that the outer member 54 is stepped at 65 to mate with the correspondingly contoured end of the sleeve 62.

The lower end of the sleeve 62 is also castellated, the gaps of the castellations being indicated at 66. Alternatively, the sleeve may be formed with a series of apertures or windows disposed circumferentially adjacent its lower end.

When the components are assembled as shown in FIG. 11, the gaps 66 of the castellations or the windows are so located that they lie adjacent the orifices formed in the end wall of the assembly 2 uppermost in FIG. 11.

The embodiment shown in FIGS. 10 and 11 operates in a manner generally similar to the embodiment of FIGS. 69. Extension 56 is joined to a source of gas, and gas emerges from the orifices as a series of jets to establish a vortex within the sleeve 62. Air is drawn in through the inner member 53 by the low pressure zone within the vortex to provide the inner core of air described above and also through the gaps 66 to provide an outer sheath of air.

It is not essential that the grooves 61 be formed in the outer member 54. The grooves could, alternatively, be formed in the inner member 53 and FIGS. 12 and 13 show such an alternative form of inner member.

As is shown in FIGS. 12 and 13, the upper (as seen in the Figures) end of inner member 67 has an outwardly extending shoulder 68 grooved at intervals round its periphery as indicated at 69. The grooves are inclined at an angle lying within the range 3560 preferably about 45 to the axis of the member 53. The outer member co-operating with an inner member of the form shown in FIGS. 12 and I3 incorporates a flange similar to flange 59 described above but which has a plain inner face that is not grooved as is the face 60 of the flange 59.

An assembly with an inner member of the form shown in FIGS. 12 and 13 can be used in the embodiments of FIGS. 69 and FIGS. 10 and 11 instead of the assembly 52.

The inner and outer members of the assemblies described above may be, for example, die cast in aluminium, the grooves being subsequently accurately sized by a suitable machining operation. Alternatively, after the members are put together the grooves can be sized by a swaging, the size being measured by passing air through the assembly. For example, a ball-ended tool is forced into the bore of the inner member 2 compressing the entrance thereof to an extent necessary to ensure the correct groove depth as determined by the air flow measurement.

Whilst the mixing devices described above with respect to FIGS. 6-13 can be used to mix fluids, the devices are primarily intended to form mixing devices for incorporation in gaseous fuel burners, the fluids then being gas and air as described above. The device may be fitted to a burner head which seats directly on the upper (as seen in the drawings) end of the

sleeves

51 or 62 or alternatively the burner head may have an entrance adapted to receive the mixed gas-air output of the mixer device and to permit the ingress of an additional supply of air drawn from the atmosphere. Ingress may be permitted via a series of holes in the entrance adjacent the mixer device output, or by spacing the entrance from the mixer device. A construction of the latter form is shown diagrammatically in FIG. 14.

The head of the burner shown in FIGS. 14 and 15 is of the construction described above with reference to FIG. 1, that is, it includes a diffuser positioned in the mouth of the burner head, the diffuser having a path therethrough for the circulation of a cooling fluid.

FIG. 14 shows an arrangement in which burner head 70 has a belled entrance 71. Located centrally with respect to the entrance 71 is a mixing device 72 which may be of any of the forms described above. Positioned in the mouth of the burner head 70 is a diffuser comprising a plurality of finned water pipes indicated in FIG. 14 by the block 73. The device 72 operates in the manner described above, the mixture of gas and air issuing from the upper (as seen in FIG. 14) end of the device passing into the entrance 71, entraining as it does so a further supply of air as indicated by the arrows in FIG. 14.

For burners of greater thermal output, it may be necessary to employ two or more mixer devices and FIG.

shows a burner employing two mixer devices 74, 75 supplying a common burner head 75.

What l claim is:

l. A gaseous fuel burner assembly comprising in combination:

a gaseous fuel mixture supply duct,

a gaseous fuel burner having an axis of symmetry, a downstream end in the form of a burner mouth transverse to said axis of symmetry, and an upstream end connected to said gaseous fuel mixture supply duct, and

gaseous fuel diffuser means comprising a body comprising an assembly of spaced, finned pipes extending across the mouth of said burner transversely of said axis of symmetry with the spaces between said fins constituting passageways for uncombusted fuel, said passageways constituting the sole gaseous fuel outlet for said burner, said passageways having inlet ends positioned to receive an uncombusted fuel mixture from said supply duct and outlet ends exposed to the ambient air which constitute substantially the sole flame ports at which combustion takes place, and said pipes constituting coolant passage means in heat exchange relationship with substantially all of said fuel passageways upstream of said flame ports.

2. A gaseous fuel burner assembly as claimed in claim 1 which further comprises an air/gaseous fuel mixer device having an inlet for air, an inlet for gaseous fuel, and an outlet for an air/gaseous fuel mixture communicating with said duct.

3. A gaseous fuel assembly as claimed in claim 2 comprising a further air inlet positioned to admit air into said duct adjacent said mixer device outlet.

4. A gaseous fuel burner assembly as claimed in claim 2 in which said mixer device outlet is separated from the upstream end of said duct by an air gap open to atmosphere.

5. A gaseous fuel burner as claimed in claim 1 and further including an air/gaseous fuel mixer device comprising an open-ended vessel having a longitudinal axis and an air inlet at one end and an outlet at the other end communicating with said duct,

a plurality of fuel inlets for conveying gaseous fuel into said vessel, each such fuel inlet being positioned to cause entry of said gaseous fuel into said vessel between the open ends of the latter in such manner as to impart to said gaseous fuel a helical motion about said longitudinal axis with a component of motion directed towards the outlet of said vessel, whereby air is drawn into said vessel through the inlet thereof.

6. A gaseous fuel burner assembly as claimed in claim 5 in which the mixer device includes two parts that have mating surfaces, the orifices being formed between the surfaces.

7. A gaseous fuel burner assembly as claimed in claim 6 in which there is included a further resilient part that is mounted between the two parts and defines at least part of the walls of said fuel inlets so that the crosssectional area of the fuel inlets is determined by the degree of compression of the further part, and in which the two parts are adjustable in position relatively to one another in order to vary the degree of compression of the further part.

8. A gaseous fuel burner as claimed in claim 5 in which the internal contour of the vessel is of venturi form, the longitudinal axis of the vessel being coincident with the axis of the venturi.

9. A gaseous fuel burner as claimed in claim 8 in which the fuel inlets are located at the throat of the venturi.

UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION PATENT NO. 3, 97,198

DATED July 29, 1975 INVENTOR(S) Alfred Longworth it is certified that error appears in the ab0veidentified patent and that said Letters Patent are hereby corrected as shown below:

Great Britain 13583/73 March 21, 1973 Signed and Sealed this thirteenth Day of April1976 [SEAL] A ties t.

RUTH C. MfiSON C. MARSHALL DANN Artz'slrng ()jjzcer ('unrmr'ssiuner nflan'l'rls and Trademarks

Claims

1. A gaseous fuel burner assembly comprising in combination: a gaseous fuel mixture supply duct, a gaseous fuel burner having an axis of symmetry, a downstream end in the form of a burner mouth transverse to said axis of symmetry, and an upstream end connected to said gaseous fuel mixture supply duct, and gaseous fuel diffuser means comprising a body comprising an assembly of spaced, finned pipes extending across the mouth of said burner transversely of said axis of symmetry with the spaces between said fins constituting passageways for uncombusted fuel, said passageways constituting the sole gaseous fuel outlet for said burner, said passageways having inlet ends positioned to receive an uncombusted fuel mixture from said supply duct and outlet ends exposed to the ambient air which constitute substantially the sole flame ports at which combustion takes place, and said pipes constituting coolant passage means in heat exchange relationship with substantially all of said fuel passageways upstream of said flame ports.

5. A gaseous fuel burner as claimed in claim 1 and further including an air/gaseous fuel mixer device comprising an open-ended vessel having a longitudinal axis and an air inlet at one end and an outlet at the other end communicating with said duct, a plurality of fuel inlets for conveying gaseous fuel into said vessel, each such fuel inlet being positioned to cause entry of said gaseous fuel into said vessel between the open ends of the latter in such manner as to impart to said gaseous fuel a helical motion about said longitudinal axis with a component of motion directed towards the outlet of said vessel, whereby air is drawn into said vessel through the inlet thereof.

7. A gaseous fuel burner assembly as claimed in claim 6 in which there is included a further resilient part that is mounted between the two parts and defines at least part of the walls of said fuel inlets so that the cross-sectional area of the fuel inlets is determined by the degree of compression of the further part, and in which the two parts are adjustable in position relatively to one another in order to vary the degree of compression of the further part.