EP0419459A1 - Gas distributing and infra-red radiating block assembly - Google Patents
Gas distributing and infra-red radiating block assemblyInfo
- Publication number
- EP0419459A1 EP0419459A1 EP88906429A EP88906429A EP0419459A1 EP 0419459 A1 EP0419459 A1 EP 0419459A1 EP 88906429 A EP88906429 A EP 88906429A EP 88906429 A EP88906429 A EP 88906429A EP 0419459 A1 EP0419459 A1 EP 0419459A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- block
- mixture
- radiation
- gas
- spaces
- Prior art date
- Legal status (The legal status 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 status listed.)
- Withdrawn
Links
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
- F23D14/16—Radiant burners using permeable blocks
Definitions
- This invention relates to gas-fired infrared burners and in particular to how the gas is distributed to the combustion zone and allowed to burn so as to efficiently emit radiation energy.
- the gas is distributed to the combustion zone through specially designed orifices or parts which are formed within a unitary block or plate of ceramic material.
- this does single block/plate of material serves to transport and distribute the gas to the burning zone, but also that the top layer of that same material serves as the combustion zone, which on being heated to incandescence also serves to produce the infrared radiation or radiant heat flux.
- the unitary material of prior art burner blocks serves at least four functions: namely transportation, distribution, combustion and radiation.
- the invention is directed towards a method for providing a burner assembly for gas-fired infrared burners, which comprises:
- the invention is directed to an appaaratus which provides a burner assembly for gas-fired infrared burners, which comprises:
- the invention involves a method for producing infrared radiation, which comprises the steps of: (a) forcing a pressurized mixture of combustion gas and air through a multitude of small first spaces connected together in a first block of material, at a velocity which is greater than the velocity of the flame propagation in the mixture, into a second block of material, which, while containing a multitude of spaces connected together which are larger than those of the first spaces, is combined with said first block to form a composite burner block assembly;
- the invention involves a method for producing infrared radiation, which comprises the steps of:
- the invention involves a method for producing infrared radiation, which comprises the steps of:
- the above-mentioned first block of material which is also referred to hereafter as the "distribution block” should have low coefficients of both thermal expansion and thermal conductivity, as well as high temperature resistance.
- Various ceramic materials can meet such needs, for example, bonded aluminium oxide fibers, lithium aluminum silicate, and materials sold under various trade names.
- the above-mentioned second block of material which is referred to hereafter as the “radiation block” should, in addition to having high temperature resistance and a low coefficient of thermal expansion, have a high emissivity and/or the ability to receive a surface oxide deposit or coating which exhibits a high infrared emissivity in the wavelength region of 1.5 to 2.0 microns. Silicon carbide is one such material, and there are various metal oxides coatings, which will meet such needs.
- the radiation block should have a high coefficient of thermal conductivity.
- first and second blocks are “combined" to form a burner assembly, this may be accomplished in a number of ways, e.g. they may be laminated or held together by a chemical bonding/sealing means, or held together mechanically.
- the overall thickness of the assembly is typically less than 2.5 cm and the second block is thinner than the first block.
- a surface screen may be used to increase the overall radiation of the assembly.
- a high temperature metal screen is used which has a relatively high heat capacity and takes time to "cool down"; it also has a relatively low radiant surface area. It is therefore a further object of this invention to provide a reverberation/enhancement screen/layer of material, which will have a very low heat capacity and a high radiant surface area of high emissivity.
- the present invention is also directed to a method for providing a reverberation layer for gas-fired infrared burners, which comprises:
- the above burner block may consist of separate layers of material having different properties as already described above.
- this fifth function of reverberation when provided in the form of a porous reticulated structure, may be combined with or bonded to the main burner assembly as a special layer of material to form an overall composite assembly of three layers of material.
- the first layer would continue to perform the functions of transporting and distributing the gas mixture (and flame arresting), and the second layer would generate by combustion the primary infra-red radiation and finally the third layer would enhance this.
- Figure 1 illustrates, in cross-section, a type of infrared burner unit in which the present invention, involving a composite burner plate/block assembly, may be used;
- Figure 2 illustrates a portion of a cross-sectional view of an embodiment of such a composite block, involving separate blocks for distribution and for radiation;
- Figure 3 illustrates a similar cross-section of another embodiment involving separate distribution and radiation blocks, combined in one assembly
- Figure 4 illustrates still another embodiment of such a composite assembly
- Figure 5 is a graph showing the relationship between the radiant output and the temperature of the emitter
- Figure 6 illustrates a cross-section of another embodiment involving separate distribution (transportation), primary radiation (combustion) and reverberation (enchancement) layers of material, combined all in one assembly.
- reference numeral 2 illustrates a type of infrared burner unit in which the present invention, involving a composite burner plate/block assembly 3, may be used.
- Burner block assembly 3 has a first block of material or distribution block 4, to transport and distribute a mixture of combustion gas and air to a second block of material or radiation blook 5, which is different from the material in distribution blook 4.
- Radiation block 5 will complete the transportation and distribution of the mixture and provide a combustion zone, wherein the gas can burn and heat the top surface of the second blook of material 5 to incandescence (generally in the range of 1100 - 1400°C) such that it will produce very efficient infrared radiation.
- the mixture is initially ignited adjacent the upper surface of block 5, e.g.
- Means are provided to combine the first and second blocks of material, i.e. distribution block 4 and radiation block 5, to form the burner block assembly 3.
- Such means to hold blocks 4 and 5 together may include chemical bonding, such as molecular bonding, sealing, gluing, etc. and/or mechanical bonding, such as molecular attraction, clamping, etc. Since chemical bonding will depend on the type of block material used, for purposes of illustration only, a more general type of mechanical bonding will be used, i.e. clip-like clamps 11.
- Block assembly 3 forms a gas-air outlet surface or side of an enclosed plenum chamber 8.
- the mixture of gas and air enters chamber 6 through tube 7 from a source 8.
- source 8 preferably supplies pressurized gas and air sufficient to provide the required mass flow rate, in certain cases, a conventional venturi aspirator may be used.
- the air and combustion gas mixture supplied from source 8 will support complete combustion without the need of any auxiliary air.
- a special metal screen or mesh 8 is provided at a short distance from the top of radiation block 5. Screen 8 is heated to incandescence by the combustion of the gas-air mixture, thereby producing radiant heat in addition to that being produced by radiation block 5.
- the inlet side to distribution block 4 is provided with a thin metal screen or membrane 10, containing a large number of small holes or orifices, the size of which is small enough to serve as a flame arrester during low gas-air flow rates.
- a thin metal screen or membrane 10 containing a large number of small holes or orifices, the size of which is small enough to serve as a flame arrester during low gas-air flow rates.
- the screens 8 and 10 may, if desired, be omitted.
- each block assembly will depend on the use to which the assembly is put; consequently, details involving cross-sectional views only are shown. As mentioned above, the overall thickness of the assembly is generally not greater than 2.5 cm. and the radiation blook is generally thinner than the distribution block.
- reference numeral reference 13 indicates such a portion, consisting of a portion of a first blook of material or distribution block 14, comprising a multitude of small first spaces (not shown) connected together, and a second block of material or radiation block 15, comprising a multitude a second small spaces connected together, which spaces are larger than those of the first spaces in distribution blook 14.
- the size of the first spaces are such that, on forcing a pressurized mixture of combustion gas and air through the small first spaces in the first or distribution block of material 14, the velocity of flow will be grater than the velocity of the flame propagation in the mixture.
- the sizes of the second spaces in the second or radiation block of material 15 are such as to allow the mixture to expand and form a turbulent mixture and to ignite and burn, thereby heating the top surface of the radiation block 15 to a very high incandescence temperature and causing it to produce very efficient infrared radiation.
- the material in each block may have a reticulated structure, involving a precise and uniformly distributed cellular pore structure, which may be expressed in terms of porosity, radiation block 15 having a greater porosity than the distribution block 14.
- the thermal conductivity and expansion of the distribution block 14 should be low, e.g. the thermal conductivity should be low enough so as to present a oool surface to the gas plenum, i.e. approx.
- porous ceramic materials provide such properties. While the thermal expansion of radiation block 15 should also be low, its thermal conductivity, temperature resistance, and emissivity should be as high as possible, silicon carbinde being one such material, or alternatively, it must be able to accept a surface coating of a high emissivity material, e.g. metal oxide coatings, such as those of cobalt, nickel, chromium, and thorium, as well as metal silicates and sillces carbide. Some of these materials may also be impregnated into the top layer. Optional screens 8 and 10 mentioned in connection with Figure 1 may be provided here to advantage: this could extend the choice of porous materials.
- the radiation block could be very much thinner than the distribution block, e.g. 206 mm compared to 10-20 mm for the distribution block, which should be thick enough to provide back pressure for the gas-air mixture to allow uniform combustion across a large number of burner surfaces connected to the same manifold.
- the pore size of block 14 should also be small enough so as to prevent flashback.
- reference numeral 23 indicates a portion of a cross-sectional view of a block assembly, consisting of a first block of material or distribution block 24, comprising a multitude of small distinct channels 26, each channel being perpendicular to the radiation surface consisting of a first section 27 and a second section 28, the first section having a cross-sectional area smaller than that of a second section 28, such that when a pressurized mixture of combustion gas and air is forced through section 27, the velocity of the mixture through the first section 27 is greater than the velocity of the flame propagation in the mixture.
- the cross-sectional area of the second section 28 is a varying one commencing with that of the first section and then expanding in bowl- shaped fashion until section 28 makes contact with a second block of material or radiation block 25, consisting of a multitude of spaces connected together, into which the mixture is forced to flow.
- the sizes of the spaces in the second or radiation block 25 are such as to allow the mixture to expand and form a turbulent mixture and to ignite and burn, thereby heating the top surface of the radiation block 25 to a very high incandescence temperature and causing it to produce very efficient infrared radiation.
- the materials and design of the channels for distribution block 24 are well known in the prior art.
- the thermal conductivity and expansion of distribution block 24 should be low, as provided by various ceramic materials, such as aluminum oxide fibers; lithium alumi nium silicate; and those sold under various trade names , e . g . "Cordiorite” " , “Mullite “ “ , etc .
- the des i gn of the channels is disclosed in e.g. U.S. Patent Nos, 3,885,907 and 3,635,644.
- Details for radiation block 25 are the same as those for radiation block 15 discussed in connection with Figure 2.
- radiation block 25 can serve to retard "lift-off" of the flame and thereby allow for a wider range of gas-air flow rates/energy inputs. Whether or not combustion takes place in the expanded section of the distribution block 24 will depend on the flow rate, the thickness and porosity of radiation block 25, as well as the design of that particular section.
- reference numeral 33 indicates a portion of a cross-sectional view of the block assembly, consisting a multitude of first small distinct channels 36 in the distribution block 34,
- Each channel 36 is perpendicular to the radiation surface and has a cross- sectional area such that when a pressurized mixture of combustion gas and air is forced through distribution block 34, the velocity of the mixture through channels 36 is greater than the velocity of the flame propagation in the mixture, each channel 36 being extended until it meets with at least one second, small channel 37 in a second block of material or radiation block 35, con taining a multitude of second channels 37, which are in direct alignment with the first small channels 36.
- the cross-sectional area of second channels 37 is a varying one commencing with that of the first channels, and then expanding in bowl-shaped fashion until the second channel 37 makes contact with the top surface of the radiation block 36.
- the size and shape of channels 37 in the radiation block 35 are such as to allow the mixture to expand and form a turbulent mixture and to ignite and burn, thereby heating the top surface of the radiation block 35 to a very high incandescence temperature, causing it to produce very efficient infrared radiation.
- the materials and design of the channels for distribution block 34 would be the same as for the first meeting of the channels described in distribution block 24 in connection with Figure 3.
- the design of the channels for the radiation block 35 is the same as that of those shown in Figure 3.
- the design of the channels for the radiation block 35 is the same as for the second section of the channels in the distribution block 24 and described in connection with Figure 3, i.e. as disclosed in the aforesaid United States patents.
- the materials for radiation block 35 should be carefully chosen, and as mentioned above, in addition to having high temperature resistance and a low coefficient of thermal expansion, they should have a high emissivity and/or the ability to receive a surface oxide deposit or coating which exhibits a high infrared emissivity in the wavelength region of 1,5 to 2.0 microns, e.g. silicon carbide or various metal oxides coatings, as mentioned above in connection with Figure 2.
- the radiation block should have a high coefficient of thermal conductivity.
- the thicknesses of the distribution and radiation blocks will depend on the type of material and prior art design for the channels that might be selected.
- Figures 3 and 4 show a gradual expansion of the sections or channels, i.e. sections 28 in Figure 3 and channel 37 in Figure 4, the expansion could also be fairly abrupt at first so as to form a bowl with nearly perpendicular sides, rather than a gradual cone-shaped bowl.
- the use of the above optional screen should be given consideration, as it will increase the radiation efficiency of the overall assembly. This arises from the following: while the total emissivity is a function of the temperature and radiating surface area, the radiation surface will reach a point of diminishing returns with higher energy inputs; however, a proper screen mounted above the radiating surface will increaase the radiation output, because the screen captures the flue gases and converts this exhaust energy to radiant energy, and also by trapping this cushion of gases, it provides an extension of the effective radiant surface by reverberation, and the same time prevents ambient air from reaching the emitting surface.
- a screen may be made from a high temperature metal or from a reticulated open ceramic structure, as already mentioned above.
- the three critical parameters for an infrared emitter are: surface area, temperature and emissivity.
- the emissivity varies with temperature and the nature of the material, so by choosing a material which inherently already has a high emissivity, the fact that it has a recticular/porous structure will further increase its emissivity.
- Various materials are disclosed above, with porous silicon carbide being an excellent example.
- the radiant flux/energy will increase in proportion to the total surface area of the radiating body which is seen by the absorbing body.
- the surfaces of the porous body 15 in Figure 2, body 25 in Figure 3, and body 45 in Figure 6 are each substantially greater than that of the upper surface 25 in Figure 4 (surface 35 being a typical surface for a conventional emitter).
- surface 35 being a typical surface for a conventional emitter.
- the emitter of curve (b) has more surface area and a higher emissivity, its radiant output at temperature T 0 will be greater than that of the conventional emitters of curve (a) at the same temperature T 0 .
- the curve does not level off as quickly, but continues to rise, making posible a further increase in the output by an increase in temperature of the emitter (through higher gas flows).
- This invention therefore, allows one to take advantage of the benefits of the higher temperatures.
- its emissivity is in the range of 0.6-0.95.
- This assembly consists of a first block of material or distribution block 44, comprising a multitude of small first spaces (not shown) connected together, a second block of material or radiation block 45, comprising a multitude of second small spaces connected together, which spaces are larger than those of the first spaces in the distribution block 44, and a third block/layer or reverberation block 46, comprising a multitude of third small spaces connected together, which spaces are still larger than those of the second block. Details of the first and second blocks are given in reference to that illustrated in Figure 2 above.
- the first or distribution block may have a porosity in the range of 60-85 ppi and be made from LAS (lithium alumina silicate) or "Mullite"
- the second or primary radiation (combustion) block may have a porosity in the range of 25-50 ppi and be made from LAS or silicon carbide (coated or impregnated with a higher emissivity material)
- the third or reverberation (enhancement) layer may have a porosity in the range of 5-10 ppi and be made from silicon carbide. Thickness of the layers will depend on various factors, but typical ranges are: first block, 10-20mm; second block 2-6mm; and third block 2-6mm.
- Another important feature of the present invention lies in the fact that conventional burners use metal parts in various areas, as well as for the reverberation screen, and in addition use dense ceramic for the burner itself; the relatively high heat capacity of these materials has the result that when the burner is turned off, the "cool-down period" is relatively long, e.g. 180-360 seconds. While the use of metal parts to hold the assembly of the present invention together is not forbidden, in its preferred form, the various layer/blocks are bonded together chemically, thereby eliminating the high heat oapacity of these metal parts. As mentioned above, the very low heat capacity of the various porous layers makes the overall heat capacity of the assembly extremely low, with the result that the "cool-down period" can be less than 5-10 secs.
- the highly porous materials can also have a very low heat, conductivity, so by choosing such a material for the distibution block, all surfaces, other than those involved in oombustion and reverberation, remain relatively cool to the touch, compared to prior art assembly surfaces, which are so hot that they can ignite flammable material.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
Abstract
L'ensemble brûleur radiant décrit, qui est destiné à un brûleur infrarouge au gaz, comprend un premier bloc (24) de matériau perméable servant au transport et à la distribution d'un mélange d'air et de gaz de combustion. Un second bloc de matériau (25) ayant des propriétés différentes du matériau du premier bloc achève le transport et la distribution du mélange et forme une zone de combustion dans laquelle le mélange brûle et chauffe la surface externe du second bloc jusqu'à la porter à l'incandescence en vue de permettre un rayonnement infrarouge efficace. Les espaces à travers lesquels le gaz s'écoule dans le second bloc (25) sont plus grands que les espaces à travers lesquels le gaz s'écoule dans le premier bloc (24), de sorte que le mélange se dilate pour former un mélange turbulent dans le second bloc. Des espaces d'écoulement de gaz de grandeurs variables peuvent être prévus dans chaque bloc de matériau. Des matériaux céramiques sont utilisés pour résister aux températures élevées.The described radiant burner assembly, which is intended for an infrared gas burner, comprises a first block (24) of permeable material used for transporting and distributing a mixture of air and combustion gases. A second block of material (25) having properties different from the material of the first block completes the transport and distribution of the mixture and forms a combustion zone in which the mixture burns and heats the external surface of the second block until it brings it to incandescence in order to allow efficient infrared radiation. The spaces through which the gas flows in the second block (25) are larger than the spaces through which the gas flows in the first block (24), so that the mixture expands to form a mixture turbulent in the second block. Gas flow spaces of varying sizes can be provided in each block of material. Ceramic materials are used to resist high temperatures.
Description
Claims
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US1988/002085 WO1989012784A1 (en) | 1988-06-17 | 1988-06-17 | Gas distributing and infra-red radiating block assembly |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0419459A1 true EP0419459A1 (en) | 1991-04-03 |
EP0419459A4 EP0419459A4 (en) | 1992-03-25 |
Family
ID=22208747
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19880906429 Withdrawn EP0419459A4 (en) | 1988-06-17 | 1988-06-17 | Gas distributing and infra-red radiating block assembly |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0419459A4 (en) |
JP (1) | JPH04500997A (en) |
CA (1) | CA1336258C (en) |
WO (1) | WO1989012784A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5224856A (en) * | 1990-01-31 | 1993-07-06 | Nippon Kokan Kabushiki Kaisha | Surface combustion burner |
JP2550419B2 (en) * | 1990-01-31 | 1996-11-06 | 日本鋼管株式会社 | Surface burning burner |
WO2004076928A2 (en) | 2003-02-21 | 2004-09-10 | Middleby Corporation | Self-cleaning oven |
TWI570362B (en) * | 2010-12-20 | 2017-02-11 | 索拉羅尼克斯股份有限公司 | Gas fired radiation emitter with embossed screen |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1830826A (en) * | 1925-08-17 | 1931-11-10 | Cox Frederick John | Refractory diaphragm for use in surface-combustion apparatus |
US2194208A (en) * | 1937-01-12 | 1940-03-19 | Clarence E Moran | Fluid fuel burner |
US3216478A (en) * | 1962-04-13 | 1965-11-09 | Electro Refractories & Abrasiv | Radiant gas burner tile |
US3885907A (en) * | 1970-10-06 | 1975-05-27 | Columbia Gas Syst | Infrared burner and apparatus for producing same |
US3947233A (en) * | 1971-04-26 | 1976-03-30 | C. A. Sundberg Ab | Free-burning equipment |
GB1439767A (en) * | 1972-09-25 | 1976-06-16 | Foseco Int | Radiant gas burners |
US4643667A (en) * | 1985-11-21 | 1987-02-17 | Institute Of Gas Technology | Non-catalytic porous-phase combustor |
-
1988
- 1988-06-17 JP JP50579488A patent/JPH04500997A/en active Pending
- 1988-06-17 WO PCT/US1988/002085 patent/WO1989012784A1/en active Search and Examination
- 1988-06-17 EP EP19880906429 patent/EP0419459A4/en not_active Withdrawn
-
1989
- 1989-06-16 CA CA000603136A patent/CA1336258C/en not_active Expired - Fee Related
Non-Patent Citations (2)
Title |
---|
No relevant documents disclosed * |
See also references of WO8912784A1 * |
Also Published As
Publication number | Publication date |
---|---|
WO1989012784A1 (en) | 1989-12-28 |
EP0419459A4 (en) | 1992-03-25 |
JPH04500997A (en) | 1992-02-20 |
CA1336258C (en) | 1995-07-11 |
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