WO2017077005A1 - Améliorations dans ou en rapport avec un module de brûleur et brûleur à gaz intégré - Google Patents

Améliorations dans ou en rapport avec un module de brûleur et brûleur à gaz intégré Download PDF

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Publication number
WO2017077005A1
WO2017077005A1 PCT/EP2016/076611 EP2016076611W WO2017077005A1 WO 2017077005 A1 WO2017077005 A1 WO 2017077005A1 EP 2016076611 W EP2016076611 W EP 2016076611W WO 2017077005 A1 WO2017077005 A1 WO 2017077005A1
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WO
WIPO (PCT)
Prior art keywords
burner
perforated screen
air
module
integrated
Prior art date
Application number
PCT/EP2016/076611
Other languages
English (en)
Inventor
Anthony Owens
Brian Walsh
Stefaan Verbruggen
Original Assignee
Eco-Burner Products Ltd.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Eco-Burner Products Ltd. filed Critical Eco-Burner Products Ltd.
Priority to EP16801717.6A priority Critical patent/EP3371513A1/fr
Priority to US15/773,521 priority patent/US20180320895A1/en
Publication of WO2017077005A1 publication Critical patent/WO2017077005A1/fr

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/12—Radiant burners
    • F23D14/14—Radiant burners using screens or perforated plates
    • F23D14/145—Radiant burners using screens or perforated plates combustion being stabilised at a screen or a perforated plate
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • F23D14/04—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/12—Radiant burners
    • F23D14/18—Radiant burners using catalysis for flameless combustion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/26—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid with provision for a retention flame
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2203/00—Gaseous fuel burners
    • F23D2203/005—Radiant burner heads
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2212/00—Burner material specifications
    • F23D2212/005—Radiant gas burners made of specific materials, e.g. rare earths

Definitions

  • the present invention relates to an improved integrated gas burner and to cooking and heating devices including the improved integrated gas burner. Background
  • An integrated gas burner comprises a gas train and a burner module.
  • the gas train has a connection to a gas supply, an ejector for forming an air/fuel mixture and a diffusor or plenum for expanding the air/fuel flow which is in fluid communication with the burner module.
  • the burner module comprises a burner face having one or more surfaces which have been coated with a catalyst.
  • Small-power portable LPG-fuelled appliances include portable soldering irons, hair curling tongs and camping stoves. Flameless radiant-mode gas-fired burners offer safety and emissions advantages over blue-flame burners and facilitate wind-resistant operation, so are sometimes specified for small-power appliances where indoor operation is envisaged. As flameless burners must be fully-aerated, they must be supplied with air/fuel mixture at or above the stoichiometric ratio required for combustion. In small-power portable gas-fuelled appliances fuelled by butane or propane-based blends (LPG fuel), one or more large area-ratio passive ejectors (gas-driven jet pump) are generally used to entrain, compress and mix the required fraction of combustion air with the fuel gas.
  • LPG fuel butane or propane-based blends
  • Flameless burner heads may variously be of substantially flat, cylindrical or conical shape, are generally sized to deliver a heat flux of less than 400kW/sq. m, and may bear a catalytic coating to promote surface combustion rather than gas-phase combustion in a flame.
  • an appliance typically has an ejector for forming an air/fuel mixture.
  • a packaging problem arises in expanding the high velocity air/fuel flow discharging from the ejector to fill the entrance aperture of the radiant burner face head, whose area is typically two orders of magnitude greater than that of the mixing tube of the ejector, while delivering a uniform velocity profile.
  • a noise problem also can exist in certain gas-fuelled portable appliances.
  • the expansion of the pressurised fuel jet through the mixing ejector and air entrainment is a turbulent and therefore noisy process. Without some intervening muffling, jet noise can radiate from the burner aperture. Muffling is not straightforward however, as simple resistive attenuators are undesirable due to energy losses.
  • a further problem concerns the need to comply with emissions regulations concerning uncombusted gas and carbon monoxide emissions. Carbon monoxide emissions occur due to incomplete combustion.
  • a burner module for use in combusting an air/fluid fuel flow
  • the burner module comprises a burner face comprising catalytic material for combusting the air/fluid fuel flow and a perforated screen having a plurality of micro-perforations wherein the perforated screen is positioned upline to the burner face to increase combustion.
  • the term fluid used in the context of the present invention encompasses gas.
  • the invention provides a compact burner module adapted to perform a large flow expansion between a gas jet inlet and a burner aperture outlet, in a minimum of axial length, in a compact volume, with minimal use of expensive catalytic surface area, while also providing excellent handling qualities in use.
  • a burner module for use in combusting an air/fluid fuel flow
  • the burner module comprises a burner face comprising catalytic material for combusting the air/fluid fuel flow and a perforated screen having a plurality of micro-perforations and the perforated screen is positioned upline to the burner face to increase combustion, wherein the perforated screen is formed from a material having a thermal conductivity adapted to reduce thermal bridging from the burner face and reflect incident heat radiation in a direction substantially perpendicular to the burner face.
  • the perforated screen can be made from a thin material, such as a metallic foil or coated with a metallic foil.
  • an integrated gas burner for connection to a pressurised fluid fuel flow
  • the integrated gas burner comprises a burner module and a gas train
  • the burner module comprises a burner face comprising catalytic material for combusting the air/fluid fuel flow and a perforated screen having a plurality of micro-perforations wherein the perforated screen is positioned upline to the burner face to increase combustion
  • the gas train comprises:
  • an appliance comprising an integrated burner according to the invention.
  • the present invention provides an integrated burner having an improved rate of combustion, effective flow metering, mixing and expansion of air and fuel flows while avoiding the noise, overheating tendencies and flow instability of known methods of flow expansion in a gas train.
  • a reduction in the amount of emissions is envisaged, specifically a reduction in the amount of uncombusted gas and carbon monoxide produced by the burner module or integrated burner in use compared to a known burner used in comparable conditions.
  • the perforated screen minimises ingress of liquid or other foreign matter into the gas train. This enables a compact, low cost close-coupled radiant integrated burner and gas train module to be engineered, with good durability and stability.
  • the perforated screen may be positioned adjacent to the burner face, for example a few gas jet diameters upline of the burner face.
  • the burner face has an aperture which is its upline facing surface which admits the air/fluid fuel mixture.
  • the perforated screen may be a homogenisation perforated screen which has perforations arranged to improve the uniformity of combustion across the aperture of the burner face.
  • the integrated burner or burner module according to the invention may comprise two perforated screens upline of the burner face wherein the perforated screens comprise a throttling perforated screen and a homogenisation perforated screen wherein the homogenisation perforated screen is positioned upline and adjacent to the burner face and the throttling perforated screen is positioned upline of the homogenisation perforated screen; and wherein the perforations on the throttling perforated screen are arranged to provide a predetermined degree of aeration of the air/fuel mixture.
  • the perforations on the throttling perforated screen are arranged to provide a predetermined degree of aeration of the air/fuel mixture.
  • the perforations on the throttling perforated screen may be arranged to provide a flattened velocity profile of the air/fluid fuel flow perpendicular to the throttling perforated screen to provide uniform combustion.
  • the integrated burner may be a radiant integrated burner comprising two perforated screens wherein the throttling perforated screen provides a fully-aerated air/fuel mixture.
  • the degree of aeration of the air/fuel mixture provided by the throttling perforated screen may be 12-20 parts of air entrained with each part of fuel gas (by weight).
  • the perforated screen may be shaped to provide one or more supports for the burner face.
  • the one or more perforated screen supports may have a pointed shape to minimise thermal bridging.
  • the perforated screen may have one or more ribs to provide axial stiffness. [0019]
  • the plurality of perforations of the perforated screen may be shaped to increase spill resistance and noise attenuation.
  • the burner module and the integrated burner according to the invention are noticeably quieter in use than comparable known burner modules and integrated burners.
  • noise attenuation can be achieved using Helmholz resonators for noise abatement (e.g. some types of auto exhaust mufflers).
  • Helmholz resonators for noise abatement e.g. some types of auto exhaust mufflers.
  • a succession of high impedance and low inpedence flow channels to a turbulent (noisy) fluid flow Hence two screens and three plenums provide some noise attenuation.
  • Fuel pressure-driven catalytic radiant integrated burners for LPG service generally require a gas train with a physically long flow length to efficiently mix and expand separate flows of air and vaporous fuel to a larger area homogenous flow of uniform velocity. This flow length scales approximately with the square root of burner power.
  • the present invention overcomes this problem with gas flow train length.
  • the present invention overcomes this problem.
  • the advantages of the present invention include: a. Use of one or more perforated screens having plurality of micro-perforations to: i. turbulate the boundary layer of fuel and oxygen species adsorbed onto the catalytic surfaces, thus significantly boosting the surface combustion efficiency without need of additional stages of mesh in the burner face to 'scavenge' and combust the products of incomplete combustion; ii.
  • the perforations of the perforated screen may be chemically etched perforations. In some embodiments, the perforations may have a cusp. In some embodiments, the perforated screen may be formed from a metal such as aluminium or steel. In some embodiments, the perforated screen may have perforations which have uniform density and diameter across the perforated area such that the perforated screen is a homogenisation perforated screen such that it may bring about intense mixing of chemical species in the boundary layer adhering to a catalytic burner face. In some embodiments, the perforated screen may have a thickness which is from 0.1 mm to 1 mm, for example 0.35mm.
  • the diameter of the perforations of the perforated screen may be from 0.1 to 0.5 mm, for example 0.25mm.
  • the perforated screen may have a square, rectangular, curved or three dimensional shape (such as a cylindrical, spherical or cuboid shape).
  • the perforated screen may be reflective.
  • the perforated screen may be formed from a thin foil having a low thermal conductivity to reduce thermal bridging from the burner face.
  • the thin foil may be a metallic foil.
  • the perforated screen may be a throttling screen and may have a plurality of perforations in a plurality of perforated areas
  • the density (number of perforations per unit area) and/or diameter of the perforations may be the same or different in each of the plurality of perforated areas and may vary across each perforated area such that the rate of flow across the plurality of perforated areas is regulated.
  • each perforated area may have the same or a different shape such as a triangular, square, rectangular, radial, annular, polygonal, curved, sector and/or irregular shape as may be required in order to homogenise the gas flow.
  • the perforated screen may be formed from a corrosion-resistant malleable, dimensionally-stable metal sheet material, may be capable of sustaining service temperatures in the range 300-600°C for the intended life of the integrated burner and/or may be capable of being polished to efficiently reflect infrared radiation, for example radiation in the wavelength range of from 0.5 to 7.5 ⁇ .
  • the perforated screen may be formed from cold-reduced austenitic or martensitic stainless steel strip or FeCrAL alloy or similar alloy. It can be difficult to avoid radiation of heat from the burner face back into the plenum, causing parts to overheat especially when the burner face is presented to external surfaces which reflect incident radiation efficiently.
  • the embodiment having a perforated screen which is capable of reflecting infrared radiation overcomes these problems. This is because the infrared reflecting perforated screen may re-radiate radiant energy from the back surfaces of the burner face back out of the burner module, helping to moderate burner self-heating.
  • the perforated screen may be manufactured by hot needle rolling, laser-cutting, waterjet-cutting, CNC machining and chemical milling. In some embodiments, the perforated screen may be electropolished to remove burrs. In some embodiments, the perforations of the perforated screen may have a cusp to provide a sharp-edged orifice to fluid flow, producing a consistent jet diameter with minimal frictional energy losses.
  • the perforated screen may be shaped to provide a support for the burner face. Advantages of the perforated screen support include that it provides means of stabilising large spans of a light-gauge radiant flat mesh burner face against slumping or handling damage by supporting the burner face from the rear. In some embodiments, the perforated screen support may have a conical shape in order to minimise any thermal bridging effect.
  • the perforated screen may be formed from a smooth material, having high reflective efficiency to IR and/or having relatively low heat conductivity such that much of the air/fuel fluid flow can be baffled from rearward infrared radiation from the burner face, limiting burner temperature rise, risk of light-back, and boosting radiant efficiency.
  • the mean reflectivity of the perforated screen material to normally-incident radiation in the range 0.5 - 7.5 ⁇ may exceed 80%.
  • the thermal conductivity of the screen material may be less than 20 W/m.K.
  • the gas train of the integrated burner may comprise a diffusor and/or a plenum.
  • the plenum may have a cross-sectional area which increases in the direction of the fluid flow.
  • the diffusor may have a cross-sectional area which increases in the direction of fluid flow.
  • the gas train of the integrated burner according to the invention may comprise an axial ejector.
  • an axial ejector may comprise a co-axial gas injector nozzle and one or more radial air inlets.
  • the ejector may have a cross-sectional area which decreases in the direction of fluid flow.
  • the gas train may comprise a radial diffusor downline of the ejector.
  • the burner may comprise one or more disc shaped perforated screens.
  • the gas train provides fluid communication from a gas fuel source and an air inlet to the burner module.
  • the integrated burner comprises a fuel source, for example a gas fuel source.
  • the gas train may comprise a folded air/fuel fluid flow such that the integrated burner is a compact integrated burner.
  • the gas train may comprise a co-annular folded air/fuel fluid flow.
  • a compact integrated burner may comprise an ejector, an annular diffusor, an annular homogeniser, optionally an annular plenum and/or a cylindrical or annular burner face.
  • a compact integrated burner may comprise one or more radially-arranged ejectors feeding a common compact plenum. Use of a folded air/fuel fluid flow path through the compact integrated burner allows the axial length of the gas train to be collapsed and simultaneously to provide a plenum of meaningful volume.
  • the annular diffusor may be shaped to provide a degree of swirl where it discharges into the annular plenum, potentially improving mixing further.
  • the burner module may comprise a crimp ring for attaching a perforated screen to the burner face.
  • the crimp ring may comprise a clip for attaching the burner module to a gas train.
  • the crimp ring may be shaped to provide a radial space to allow the burner module to thermally expand in use.
  • the crimp ring may prevent slip of the air/fuel mixture past the burner module.
  • the burner module may comprise one or more axial spacers for providing axial separation between a perforation screen and the burner face or between perforation screens.
  • the axial separator for placement between a perforated screen and the burner face may be selected to have an axial length which is sufficiently short to reduce the risk of light back and overheating of the perforated screen whilst sufficiently long such that flow from the perforated screen turbulates the burner face.
  • a skilled person would understand how to select a suitable axial length for such an axial separator.
  • the crimp ring accordingly allows an effective catalytic burner face to be engineered.
  • the crimp ring enables the radiant burner face to be supplied with a flow of mixed air/gas mixture across its entrance aperture.
  • the radial space of the crimp ring may allow the burner face to be thermally decoupled from its mounting to avoid cold spots and allows the burner face to thermally expand and contract freely to avoid deformation and/or low-cycle fatigue effects.
  • the gas train may comprise an adaptor for connection to a pressurised fluid fuel source.
  • the burner face may comprise a metal mesh, a porous ceramic monolith and/or an open-cell metal foam treated with a combustion catalyst.
  • a suitable combustion catalyst includes platinum (Pt), palladium (Pd), rhodium ( h) and/or a rare earth compound.
  • the burner face may have a sufficient area to fully combust the required fuel to generate the target power output.
  • the burner face may have a greater catalytic area than may be required to assure complete combustion of fuel to allow for imperfections such as incomplete air/gas mixing, non-uniform mixture velocity across the burner face, or excessive conduction of heat away from the burner face to its mounting.
  • the gas train may comprise an axial gas inlet. In some embodiments, the gas train may comprise one or more radially-arranged ejectors. [0036]
  • the compact gas train and radiant burner technology described here can be used in many portable and permanent combustion applications, including heating and combustible gas purification and flaring applications.
  • an appliance according to the invention may be a food warming device such as a chafing dish heater, a space heater or a stove.
  • a chafing dish heater may comprise two nesting metal vessels and one or more integrated burners according to the invention. In some embodiments, each nesting metal vessel may have a substantially flat under-surface.
  • a lower dish contains a shallow layer of water, used as a heat distribution and coupling agent and an upper dish contains solid or liquid foodstuffs to be kept warm or cooked, and placed beneath the nested dishes are one or more integrated burners according to the invention with a pressurised fuel supply.
  • the integrated burner is radiant, the appliance can be operated if necessary with minimal clearance between the burner face and the underside of the nested dishes, as, being a fully-aerated flameless technology there are negligible flame-quenching effects and carbon monoxide emission levels will comply with regulatory norms under all conditions of service.
  • a space heater may comprise a reflective surface, an integrated burner according to the invention and a pressurised fuel source.
  • a space heater may additionally comprise a support, an electrical igniter and/or a handle for positioning of the reflective surface and/or integrated burner.
  • a stove may comprise an integrated burner, a pressurised fuel supply, a pot support, a pot and a burner shield. The pot may be shaped such that the other components can fit inside it for storage.
  • the relevance of this invention is that use of the features and method described eases those difficulties [0039]
  • the objective of this method is to provide clean-burning, quiet, long-lived ejector-mixers and radiant integrated burners, which may optionally be close-coupled as a module, for appliances powered by fuel vapour pressure, with minimal bulk and cost.
  • the burner face may have a spherical, flat, cylindrical, or conical shape, particularly a flat or cylindrical shape.
  • V b A b * L Tax (1)
  • L T is the path length of gas flow through the integrated burner. This is given by equation (2):
  • L T L e + L d + L p + L b (2)
  • L e represents the length of the ejector
  • L d represents the length of the diffusor
  • L p represents the length of the plenum (where present)
  • U represents the length of the burner module
  • L Tax is the axial component of the vector sum given by equation 3: [0042]
  • the integrated burner has an arrangement where V b is minimised for a given heat input rate. Arrangements where V b is minimised also tend to minimise cost. Because A b is substantially determined by required heat input rate, this implies minimisation of L Tax .
  • An expansion ratio Rf may be defined between the cross sectional area of the mixing tube of the ejector (1) and the area of the exit aperture of the burner (4):
  • Rf typically is in the range 50 - 150 for radiant burners in fully-aerated ejector-driven appliances.
  • a difficulty arises in mixing an appropriate fraction of entrained air thoroughly with the driving gas jet, then expanding the mixture flow to enter the burner entrance aperture with uniform velocity and air/gas concentration, while simultaneously minimising L T . This is because ejectors, faired diffusers and plenum chambers need to have substantial length to operate efficiently.
  • Gas-driven ejectors for entraining and mixing sufficient air to combust the fuel gas typically require mixing tube lengths in the range 3.5-5.5 times the tube diameter.
  • Faired (conical diverging) diffusers are typically designed with an included angle between opposing walls of around 5.5 degrees, while good recovery of pressure from the high velocity mixture discharging from the ejector requires a ratio of diffuser discharge area to inlet area of better than 2:1.
  • Plenum chambers must be sufficiently large to allow flow separation or other instabilities at diffuser discharge to dissipate and mixture velocity to become homogenous. Residence time of mixture in a plenum sometimes is necessary for sufficient molecular diffusion and micro-mixing to occur between phases to ensure adequate air/gas homogenisation. Given all these considerations, L T for a typical appliance tends to be large.
  • FIGURE 1A shows a schematic plan view of a first embodiment of a perforated screen according to the invention
  • FIGURE IB shows a schematic plan view of a second embodiment of a perforated screen according to the invention
  • FIGURE 1C shows a schematic plan view of a third embodiment of a perforated screen according to the invention
  • FIGURE 2 shows a schematic partial cross-sectional view of a perforation of a perforated screen according to the first, second or third embodiment of a perforated screen according to the invention
  • FIGURE 3A shows a schematic cross sectional view of a first embodiment of an integrated burner according to the present invention
  • FIGURE 3B shows a schematic cross sectional view of a burner module according to the invention as part of the integrated burner of the first embodiment of the invention
  • FIGURE 4A shows a computational fluid dynamics visualisation of gas density in moles per cubic metre of the first embodiment of an integrated burner according to the invention in use
  • FIGURE 4B shows a computational fluid dynamics visualisation of gas flow in metres per second of the first embodiment of an integrated burner according to the invention in use;
  • FIGURE 4C shows a computational fluid dynamics visualisation of gas temperature in degrees Centigrade in the first embodiment of an integrated burner according to the invention in use; and
  • FIGURE 4D shows a computational fluid dynamics visualisation showing dump diffuser diffusion effect;
  • FIGURE 5 shows a schematic cross sectional view of a second embodiment of an integrated burner according to the present invention
  • FIGURE 6 shows a schematic cross sectional view of a third embodiment of an integrated burner according to the present invention.
  • FIGURE 7A shows a computational fluid dynamics visualisation of gas concentration in moles per cubic metre through the third embodiment of an integrated burner according to the invention in use where a mixing shock is discernible close to the downline end of the radial transition duct after which air and fuel are no longer separate phases but are well mixed; and
  • FIGURE 7B shows a computational fluid dynamics visualisation of fluid velocity in metres per second of air and vaporous fuel streamlines of the third embodiment of an integrated burner according to the invention in use, indicating smooth air entrainment and compression through the ejector without flow separation followed by discharge into the annular plenum;
  • FIGURE 8 shows a schematic cross sectional view of a fourth embodiment of an integrated burner according to the present invention, including two mixing ejectors arranged in parallel with common fuel and air inputs and a common discharge plenum;
  • FIGURE 9 shows a schematic plan and partial cross-sectional view of the fourth embodiment of an integrated burner according to the present invention, but including three mixing ejectors arranged in parallel with common supply and delivery provisions;
  • FIGURE 10 shows a graph depicting three alternate graded porosity distributions of the third embodiment of the perforated screen which may be used in the first, second or fourth embodiment of an integrated burner according to the invention
  • FIGURE 11 shows a schematic cross-sectional view of a first embodiment of an appliance according to the invention in the form of a chafing dish heater comprising a first embodiment of an integrated burner according to the invention
  • FIGURE 12 shows a schematic cross-sectional view of a second embodiment of an appliance according to the invention in the form of a patio heater according to the invention comprising a first embodiment of an integrated burner according to the invention;
  • FIGURE 13 shows a schematic partial cross-sectional and partial side view of a second embodiment of an appliance according to the invention in the form of a camping stove according to the invention comprising a first embodiment of an integrated burner according to the invention.
  • a first embodiment of a perforated screen according to the invention is generally indicated at 40 on Figure 1A of the accompanying drawings.
  • Perforated screen 40 is in the form of a metal disc 41 and has a plurality of perforations 48 in a perforated area marked 42, six radial ribs 45 to stiffen the perforated screen 40 and six circular shaped supports 44 for supporting a burner face (not shown).
  • the perforated screen 40 is typically arranged in a gas train immediately upline of a burner module. The density and diameter of the perforations is homogenous across perforated area 42.
  • Perforated screen 40 is a homogenisation perforated screen as its purpose includes homogenising air/gas flow and turbulating or energising any layer of stagnant gases which is coating a surface of the burner module. It has been found that by energising such a boundary layer adhering to surfaces of the burner module, the reactivity of the catalysts coating those surfaces is significantly increased.
  • Perforated screen 30A is in the form of a metal disc and has a plurality of perforations 38 in a plurality of perforated areas which are marked 32A,32B,32C,32D,34A,34B,34C,34D and four transverse ribs 35 to stiffen the perforated screen 30.
  • the density of the perforations is different in each of the plurality of perforated areas 32A,32B,32C,32D,34A,34B,34C,34D and may vary across each perforated area 32A,32B,32C,32D,34A,34B,34C,34D.
  • perforated screen 30A is a throttling perforated screen 30A.
  • the perforated areas 32A,32B,32C,32D,34A,34B,34C,34D may take an alternative shape such as a triangular, square, annular, polygonal, curved, sector and/or irregular shape as may be required in order to tune aeration of the air/fuel mixture and adjust the velocity profile of the flow across the aperture of the screen.
  • Perforated screen 30B is in the form of a metal disc 31B and has a plurality of perforations 38 in a plurality of perforated areas or zones which are marked 36A,36B,36C,36D,36E,36F,36G,36H.
  • the density of the perforations is different in each of the plurality of perforated areas 36A,36B,36C,36D,36E,36F,36G,36H.
  • Perforated areas 36A,36B,36C,36D,36E,36F,36G,36H cover an outer area of the metal disc 31A and have an annular shape.
  • perforated screen 30B is a throttling perforated screen 30B.
  • the perforated areas 36A,36B,36C,36D,36E,36F,36G,36H may take an alternative shape such as a triangular, square, polygonal, curved, sector and/or irregular shape as may be required in order to homogenise the gas flow.
  • the diameter of the perforations may vary across the plurality of perforated areas 36A,36B,36C,36D,36E,36F,36G,36H.
  • the density and/or the diameter of the perforations may vary across each perforated area 36A,36B,36C,36D,36E,36F,36G,36H.
  • Cusp 39,49 is believed to improve the performance of the perforated screen 30A,30B,40 as it allows perforation 38,48 to perform as a nozzle.
  • Metal disc has a thickness 33,43 which is about 0.25mm.
  • the perforations 38,48 have a diameter of about 0.35mm.
  • the thickness 43 may be from 0.1 mm to 1 mm.
  • the diameter of perforations 38,48 may be greater than thickness 43 for ease of manufacture.
  • the diameter of the perforations 48 may be from 0.1 to 0.5 mm.
  • perforated screen 40 may have a different shape such as a square, rectangular, curved or three dimensional shape (such as a cylindrical, spherical or cuboid shape).
  • the perforated screens 30,40 have a hydraulic diameter which for each perforated screen 30,40 is the sum of the diameters of all of their perforations 38,48.
  • the hydraulic diameter determines the back pressure of the throttling screen 30 and thereby the degree of aeration of an air/fluid fuel flow from the gas train may be selected by setting the hydraulic diameter by the appropriate choice of the number of the perforations 38,48 and their diameters.
  • Suitable perforated screens 30A,30B,40 are preferably made from a corrosion-resistant malleable, dimensionally-stable metal sheet material, capable of sustaining service temperatures in the range 300-600°C for the intended life of the burner 100,200,300,400, and capable of being polished to efficiently reflect radiation in the wavelength range 0.5 - 7.5 ⁇ .
  • Cold-reduced austenitic or martensitic stainless steel strip or FeCr alloy are suitable materials.
  • the size of the required perforations depends in part upon the geometry of the burner 100,200,300,400, for example on the clearance between the perforated screen 30A,30B,40 and the upstream surfaces of a burner face 150,250,350,450.
  • a perforated screen 30A,30B,40 having perforations 38,48 having a smaller diameter has improved noise attenuation and spill resistance as ingress by solid or liquid matter into the gas train or burner module is reduced.
  • the density of perforations 38,48 can either be fixed or can be varied across the surface of the screen to flatten the velocity profile of mixture entering the burner face 150,250,350,450.
  • Figure 1C shows an example of a perforated screen 30B for a flat circular burner. The surface has been divided into annular zones 36A,36B,36C,36D,36E,36F,36G,36H which all bear the same size of hole, but the hole density can easily be varied by increasing or decreasing the hole count monotonically in each dv
  • Figure 10 depicts three alternate graded porosity distributions for the screen of Figure 1C obtained in this way. Overall porosity is given by the ratio of total hole area to the burner entrance aperture, and can conveniently be used to adjust the mixture strength of the burner 100,200,300,400.
  • the perforated screens 30A,30B,40 may be manufactured by a number of methods, of which the more convenient include hot needle roller, laser-cutting, waterjet-cutting, CNC machining and chemical milling. For the first four methods, improved tolerances and reduced costs result where sheet material is laminated together during machining and clamped between thicker plates. On completion, screens may be electropolished to remove burrs.
  • the preferred method of manufacture is chemical milling of the sheet material from both sides, with accurate mutual registration of a lithographic mask on each side. According to this process, the minimum hole size that is possible with high yield is given by the material thickness used.
  • the resulting profile of the etched perforation 38,48 will not have parallel walls but will have a reduced diameter cusp 39,49 approximately halfway down the bore. This can be advantageous in that it behaves as a sharp-edged orifice to fluid flow, producing consistent jet diameter with minimal frictional energy losses.
  • Chemical milling can be conveniently coupled with electropolishing to remove sharp edges and improve the reflectivity of the burner-facing surface.
  • FIG. 1 A first embodiment of an integrated burner according to the invention is indicated generally at 100 on Figures 3A and 3B of the accompanying drawings.
  • Integrated burner 100 comprises a gas jet-driven air-aspirating ejector 110, a radial diffusor of elliptical wall profile 120, a disc shaped throttling screen 130 and a burner module indicated generally at 159 which comprises a homogenisation screen 140, a crimp ring 155 and a burner face 150.
  • Ejector 110 has a co-axial primary nozzle 112, two radial air inlets 114 and an ejector secondary nozzle 116. The primary nozzle and two radial air inlets 114 provide inlets for the ejector secondary nozzle 116.
  • Secondary nozzle 116 of ejector 110 discharges to a mixing tube 118 which discharges to a radial diffusor 120.
  • Diffusor 120 has a cross-sectional area which broadens from narrow tube 118 to be substantially the same as that A B of the burner face 150.
  • Diffusor 120 houses the throttling screen 130 and the burner module 159.
  • Diffusor 120 has a lower lip 124 for supporting the throttling screen 130, an axial spacer 126 for supporting the burner module 159 and an upper lip 122 for securing the burner module 159.
  • Burner module 159 comprises the burner face 150, the homogenisation screen 140 and the crimp ring 155.
  • Crimp ring 155 secures the homogenisation screen 140 to the burner face 150.
  • Crimp ring 155 has a lower clip 158 for engagement with the homogenisation screen 140 and an upper clip 156 for securing burner face 150.
  • Crimp ring 155 minimises the risk of air/fuel mixture bypassing the burner face 150.
  • the throttling screen 130 is supported by lower lip 124 of the diffusor 120.
  • Axial spacer 126 is placed on top of throttling screen 130 to space it from the homogenisation screen 140 of the burner module 159.
  • Burner module 159 is placed on axial spacer 126 and is secured by upper lip 122 of the diffusor 120.
  • the burner module 159 may comprise the homogenisation screen 140.
  • the crimp ring 155 may comprise a clip for engaging with the diffusor 120.
  • Throttling screen 130 may be a perforated screen 30A according to the second embodiment of the invention as shown in Figure IB, having perforations 138.
  • Homogenisation screen 140 may be a perforated screen 40 according to the first embodiment of the invention shown in Figure 1A, having perforations 148.
  • Homogenisation screen 140 is shaped to form three supports 144 for burner face 150 to prevent burner face 150 from sagging, to improve durability of the burner face 150 and to allow a wider burner aperture (A B ).
  • Support 144 has a pointed shaped to minimise thermal bridging between the homogenisation screen 140 and the burner face 150.
  • Throttling screen 130 and homogenisation screen 140 are separated from each other by an annular spacer 153.
  • Burner face 150 is formed from a metal mesh which is at least partially coated with a catalytic material to ensure substantially flameless combustion of a gas/air mixture.
  • Upper clip 156 of the crimp ring 155 is shaped such that a radial space 152 is provided to allow for thermal expansion of the burner face 150 in use.
  • Primary nozzle 112 has an adaptor (not shown) for connection to a pressurised fluid fuel source.
  • Ejector 110 has an axial length which is indicated at L E .
  • Diffusor 120 has an axial length which is indicated as the sum of L D and L P .
  • Burner face 150 has an axial length L B .
  • the integrated burner 100 has an overall axial length L Tax which is indicated as being the vector sum of L E , L D , L P and L B .
  • ⁇ (L d + L p ) is minimised by use of the radial diffuser 120 and substantial elimination of a plenum upline of the burner face 150.
  • the upline screen 130 acts as a semi-permeable boundary for the radial diffuser 120, ensuring high velocity mixture discharging the ejector 110 negotiates the axial to radial direction change with acceptable energy losses and without severe flow separation, while also enabling the flow to distribute across its aperture, permeate, and progress towards the burner face 150.
  • the axial to radial direction change is required because the aperture of the burner face 150 is greater than that of the mixing tube 118.
  • the downline screen 140 behind the burner face 150 acts to further homogenise the velocity distribution of the mixture flow and to reflect radiation emitted by the burner face 150 back out of the burner face 150.
  • Flow passage through each screen 130,140 is accompanied by considerable microturbulence due to jet action through the perforations 138,148. In this way, the flow length of a conventional plenum can be greatly shortened, while the use of a radial diffuser 120 with semi-porous boundary wall formed by screens 130,140 enables flow expansion in a very short axial length.
  • the gas train can be baffled from infrared radiation radiated from the rear of the burner face, limiting burner temperature rise, hence reducing risk of light-back and boosting radiant efficiency.
  • a further benefit of the use of thin perforated screens 130,140 in the burner 100 according to the first embodiment of the invention is relevant to cooking applications, where burners 100 are generally inverted and stationed below cooking vessels.
  • the small diameter of the perforations 138,148 - typically of the same order as the thickness of the screen material - affords some protection to the gas train from liquid and particulate ingress via the burner face 150.
  • a yet further benefit of the use of at least one thin perforated screen 130,140 stationed a few microjet diameters upstream of the rear of the burner face 150, is the ability to boost mass transport rate of reactant molecules to a catalytically-coated burner face 150 through the effects of jet impingement.
  • FIG. 4A depicts a propane/butane gas jet at 280 kiloPascals gauge (dark grey at bottom LHS) mixing with ambient air (dark grey at left). Blended air/gas passes from the radial diffuser 120 through two perforated screens 130,140 and through the flat catalytic burner face 150 and is discharged to atmosphere. Combined screens and burner resistance of 50 Pascals was assumed. As the flow progresses down the mixing tube 118 and jet breakup occurs, momentum is transferred to the entrained air.
  • Figure 4B Shortly after the entry to the axial-radial transition at the inlet to the radial diffuser 120, the streamlines and velocities in Figure 4B clearly indicate a powerful toroidal vortex, which in Figure 4A appears to homogenise a partially-mixed air/gas flow discharging from the ejector. Also clearly visible in Figure 4B is the homogenising effect of the screens 130,140 on velocity profile across the burner face 150. Also visible is the jetting effect of the perforations 148 in the screen 140 closest the burner face 150 onto the catalytic surfaces.
  • Figure 4C indicates the effectiveness of the perforated screens 130,140 in baffling much of the rearward-emitted radiation from the burner face 150 from affecting upstream mixture temperature, reducing risk of lightback.
  • Figure 4D indicates the effectiveness of dump diffuser diffusion effect 119.
  • Integrated burner 200 comprises a gas jet-driven air-aspirating ejector 210, an annular diffusor 220, an annular plenum 225, a cylindrical homogenisation screen 240 and an outer cylindrical burner face 250.
  • Ejector 210 has a co-axial primary nozzle 212, two radial air inlets 214 and an ejector secondary nozzle 216.
  • the primary nozzle 212 and air inlets 214 provide inlets for the ejector secondary nozzle 216.
  • Secondary nozzle 216 discharges to a mixing tube 218 which discharges into annular diffusor 220.
  • Annular duct 219 turns fluid flow radially and then axially to enter annular diffusor 220. Fluid flow from the annular diffusor 220 is turned radially by one or more radial outlets 221 to enter plenum 225 and is directed towards the burner face 250 via cylindrical homogenisation screen 240.
  • Homogenisation screen 240 may be a perforated screen 40 according to the first embodiment of the invention shown in Figure 1A except that it has a cylindrical shape.
  • Burner face 250 may be formed from a metal mesh which is at least partially coated with a catalytic material to ensure substantially flameless combustion of a gas/air mixture.
  • Primary nozzle 212 has an adaptor (not shown) for connection to a pressurised fluid fuel source.
  • the integrated burner 200 accordingly has a co-annular arrangement of ejector 210, diffuser 220 and plenum 225 which folds these three elements very efficiently via two flow reversals provided by radial tube 219 and radial outlet 221 from the diffusor 220. This minimises ⁇ (L e + ⁇ d ) an d consequently L Tax .
  • the folded gas train is used to feed a radially- firing cylindrical burner face 250. Flow from a conventional central jet ejector 210 is turned first radially then axially into an annular diffuser 220, before finally being turned radially again and discharged into an annular plenum 225. Flow entry into the plenum 225 can have tangential swirl imparted.
  • a single cylindrical perforated screen 240 is added in close proximity to the inlet surfaces of the burner face 250 to turbulate the catalytic surfaces (not shown) of the burner face 250 and acts as a radiation baffle.
  • the co-annular ejector-diffuser 210,220 arrangement provides excellent mixing of air/gas as is clear from the CFD simulations of Figures 7A and 7B and a good degree of flow expansion.
  • a second perforated screen for improving flow uniformity and mixing quality may be unnecessary.
  • Integrated burner 300 comprises a gas jet-driven air-aspirating ejector 310, an annular diffusor 320, an annular plenum 325, an annular homogenisation screen 340 and an annular burner face 350.
  • Ejector 310 has a primary nozzle 312 for gas injection, two radial air inlets 314 and an ejector secondary nozzle 316.
  • Primary nozzle 312 and air inlets 314 are provide inlets for ejector secondary nozzle 316.
  • Secondary nozzle 316 of ejector 310 discharges into mixing tube 318 which discharges into diffusor 320.
  • Annular duct 319 turns fluid flow radially and then axially to enter annular diffusor 320. Fluid flow from the annular diffusor 320 is turned radially by one or more radial outlets 321 to enter plenum 325 and is directed towards the burner face 350 via annular metering screen 330 and annular homogenisation screen 340. Homogenisation screen 340 may be a perforated screen 40 according to the first embodiment of the invention shown in Figure 1A except that it has an annular shape.
  • the integrated burner 300 according to a third embodiment of the invention provides a substantially flat burner face variant of the integrated burner 200 according to the second embodiment of the invention depicted in Figure 5.
  • Burner face 350 is formed from a metal mesh which is at least partially coated with a catalytic material to ensure substantially flameless combustion of a gas/air mixture.
  • Primary nozzle 312 has an adaptor (not shown) for connection to a pressurised fluid fuel source.
  • FIG. 7A depicts gas concentration in moles per cubic metre of a propane/butane gas jet at 280 kiloPascals gauge (dark grey at top LHS) mixing with ambient air (dark grey at left). Blended air/gas discharges from the annular flat surface at the right hand end of the plenum 325 to an assumed perforated screen and burner face resistance of 50 Pascals. As the flow progresses down the ejector's mixing tube 318 and jet breakup occurs, momentum is transferred to the entrained air.
  • Figure 7B depicts flow velocity in metres per second and streamlines.
  • the effectiveness of the lengthy annular diffuser in decelerating the flow velocity is apparent, as is the good control of flow separation throughout the gas train which is often difficult to achieve in annular ducts.
  • the mass ratio of entrained air to gas for this CFD case was 20.7:1, equivalent to approximately 25% excess air for a typical LPG-type fuel. This simulation indicates the outstandingly good combination of mixing effectiveness, high air entrainment and very compact dimensions possible using gas trains folded in this way.
  • Integrated burner 400 comprises an axial gas inlet 405, three radially-arranged gas/air ejectors 410A,410B,410B, three axial diffusors 420A,420B,420C, an annular plenum 425, an annular homogenisation screen 440 and an annular burner face 450.
  • the ejectors 410A,410B,410C each have a primary nozzle 412A,412B,412C for gas injection, an axial air inlet 414A,414B,414C and a secondary nozzle 416A,416B,416C.
  • Primary nozzle 412A,412B,412C for gas injection and axial air inlet 414A,414B,414C provide inlets for the secondary nozzle 416A,416B,416C.
  • Secondary nozzles 416A,416B,416C of ejectors 410 lead to radially-arranged mixing tubes 418A,418B,418C which discharge into diffusing bends 420A,420B,420C.
  • Fluid flow discharging axially from the diffusing bend 420A,420B,420C exits into plenum 425 and is directed towards annular burner face 450 via homogenisation screen 440.
  • Homogenisation screen 440 may be a perforated screen 40 according to the first embodiment of the invention shown in Figure 1A except that it has an annular shape.
  • Burner face 450 may be formed from a metal mesh which is at least partially coated with a catalytic material to ensure substantially flameless combustion of a gas/air mixture.
  • Primary nozzles 412A,412B,412C have an adaptor (not shown) for connection to a pressurised fluid fuel source.
  • the fourth embodiment of the integrated burner according to the invention shown in figures 9 and 10 illustrates the concept of segmentation of a single large ejector into multiple radially or axially-arranged smaller identical ejectors fed by a common gas supply, with single shared plenum and burner face.
  • ⁇ (L e + L d ) is minimised.
  • a diffusing duct 420A,420B,420C incorporating a 90 degree bend is provided at the discharge end of each ejector 410A,410B,410C.
  • This gas train arrangement can be packaged efficiently with radial-firing or axial-firing burner faces 450, using at least one perforated screen 440 to homogenise flow distribution into the burner face 450 and to turbulate catalytic surfaces.
  • the burner face 150,250,350,450 may be a catalytic radiant burner head.
  • the burner face 150,250,350,450 may comprise a porous ceramic monolith or open-cell metal foam treated with a combustion catalyst such as platinum (Pt), palladium (Pd), rhodium ( h) and/or a rare earth compound.
  • Burner face 150,250,350,450 has a sufficient area to fully combust the required fuel to generate the target power output.
  • greater catalytic area may be required to assure complete combustion of fuel in the face of imperfections such as incomplete air/gas mixing, non-uniform mixture velocity across the burner face 150,250,350,450, or excessive conduction of heat away from the burner face 150,250,350,450 to its mounting means.
  • Radiant burner faces require mounting methods that minimise heat losses at the support points, minimise the degree of 'slip' or bypassing of mixture around the burner perimeter, while enabling substantial thermal expansion and contraction of the burner face without restraint.
  • High temperature gasketing materials of needled quartz fibre are suitable.
  • FIG. 11 depicts a first embodiment of an appliance according to the invention which is indicated generally at 60.
  • Appliance 60 is in the form of a well-known food warming or cooking device.
  • a chafing dish 63,64 is provided, consisting of two nesting metal vessels 63,64, with substantially flat under-surfaces.
  • the lower vessel 63 contains a shallow layer of water 62, used as a heat distribution and coupling agent.
  • the upper dish contains solid or liquid foodstuffs 65 to be kept warm or cooked.
  • the appliance 60 Placed beneath the nested dishes are one or more integrated burners 100 each connected to a LPG- fuel container 107. As the integrated burner is radiant, the appliance 60 can be operated if necessary with minimal clearance between the burner face and the underside of the nested dishes, as, being a fully-aerated flameless technology there are negligible flame-quenching effects and carbon monoxide emission levels will comply with regulatory norms under all conditions of service.
  • FIG. 12 schematically depicts a second embodiment of an appliance according to the invention which is indicated generally at 70.
  • Appliance 70 is in the form of space heating device for indoor or outdoor use, employing a radiant integrated burner 100 adapted to have a spherical burner face 150.
  • the spherical burner face 150 is placed a short distance inside the focal point of a substantially parabolic reflector 72.
  • Heat from the integrated burner 100 is reflected off parabolic reflector 72 as illustrated by beams 77.
  • the integrated burner is both supported and fuelled via a tubular support 74 mounted coaxially with the reflector 72.
  • a compact gas supply 107 is located behind, and is baffled by, the reflector 72 from direct radiation.
  • Convenient burner power control can be provided via a projecting handle 76 which is rotatable about the reflector axis and incorporating a button control (not shown) to operate an electrical igniter (not shown).
  • the handle 76 may additionally be used to adjust the pose of the reflector 72 in tip and tilt.
  • the intra-focal distance of the centre of curvature of the burner face 150 may be adjusted via the projecting handle 76 or by other means, enabling beam divergence to be adjusted.
  • the reflector 72 and integrated burner 100 may be pole or wall-mounted and positioned for indoor or outdoor comfort heating, accelerated drying or curing of coatings or composites and other purposes.
  • a flameless radiant integrated burner has a better-defined object shape than a blue-flame burner, while a truncated spherical profile is optimal for projecting a uniform heat flux on the image plane. Radiant burners, being fully-aerated, are not susceptible to soot accumulation on the reflective optics over time.
  • the low mass of the compact folded gas train embodiments disclosed here enable the suspended mass to be minimised to the benefit of safety and stability, while the mass of embodied materials and therefore the cost of the integrated burner is very low.
  • FIG. 13 depicts in half-section a third embodiment of an appliance according to the invention which is indicated generally at 80.
  • Appliance 80 is in the form of a portable single-burner LPG-fuelled stove for camping and the like.
  • Stove 80 comprises a pot 82, a pot support 86, a burner shield 84, an integrated burner 300 according to the third embodiment of the invention and fuel supply 307.
  • the pot support 86, pot support 86, burner shield 84, integrated burner 300 and fuel supply 307 nest into the pot 82 for compact storage.
  • the burner face 350 of outer diameter approximately 90mm, combusts approximately 2kW of gas, measured by heat input rate, equivalent to a heat flux of 320 kW/sq.m approximately.
  • Burner face temperature is approximately 820 - 900°C depending on the reflectivity of the under surface of the pot 82.
  • a stepped substantially-conical radiation reflector with air induction and exhaust holes doubles as a pot support 86 and as windproofing screen 84. Exhaust gases are discharged through perforations around the perimeter of the radiation reflector (not shown) while infrared radiation is concentrated within the cavity formed between perforated screen, underside of the pan, and the stepped radiation reflector.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)

Abstract

L'invention concerne un module de brûleur destiné à être utilisé pour la combustion d'un flux d'air/combustible fluide, le module de brûleur comprenant une face de brûleur (150) comprenant un matériau catalytique pour la combustion du flux d'air/combustible fluide et un tamis perforé (140) présentant une pluralité de microperforations (148), le tamis perforé (140) étant positionné en amont de la face de brûleur (150) pour augmenter la combustion ; un brûleur à gaz intégré pour un raccordement à un flux de carburant fluide sous pression, le brûleur à gaz intégré comprenant un module de brûleur et un circuit de gaz, le module de brûleur comprenant une face de brûleur (150) comprenant un matériau catalytique pour la combustion du flux d'air/combustible fluide et un tamis perforé (140) présentant une pluralité de microperforations (148), le tamis perforé étant positionné en amont de la face de brûleur pour augmenter la combustion ; et le circuit de gaz comprend : a) un éjecteur (110) pour entraîner de l'air avec le flux de combustible fluide ; et b) un diffuseur (120) pour transformer l'énergie cinétique du flux d'air/combustible fluide en pression et pour exécuter une expansion de flux.
PCT/EP2016/076611 2015-11-03 2016-11-03 Améliorations dans ou en rapport avec un module de brûleur et brûleur à gaz intégré WO2017077005A1 (fr)

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EP16801717.6A EP3371513A1 (fr) 2015-11-03 2016-11-03 Améliorations dans ou en rapport avec un module de brûleur et brûleur à gaz intégré
US15/773,521 US20180320895A1 (en) 2015-11-03 2016-11-03 Improvements in or relating to a burner module and an integrated gas burner

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GBGB1519449.1A GB201519449D0 (en) 2015-11-03 2015-11-03 Improvements in or relating to organic material
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EP3371513A1 (fr) 2018-09-12
US20180320895A1 (en) 2018-11-08
GB201519449D0 (en) 2015-12-16

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