Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F27—FURNACES; KILNS; OVENS; RETORTS
  • F27B—FURNACES, KILNS, OVENS, OR RETORTS IN GENERAL; OPEN SINTERING OR LIKE APPARATUS
  • F27B15/00—Fluidised-bed furnaces; Other furnaces using or treating finely-divided materials in dispersion
  • F27B15/02—Details, accessories, or equipment peculiar to furnaces of these types
  • F27B15/14—Arrangements of heating devices
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
  • F23C10/00—Fluidised bed combustion apparatus
  • F23C10/18—Details; Accessories
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
  • F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
  • F23C2900/99006—Arrangements for starting combustion

Definitions

• This invention relates to heating matter and is particularly, but not exclusively, applicable to methods of heating matter using apparatus as disclosed in Specification EP-B-68853 and copending British
• a gaseous mixture which is reactable to produce heat may be used to provide a heated fluid flow, for example the gaseous mixture may be a combustible gaseous mixture, typically comprising an air-gaseous fuel mixture.
• the reaction which produces the heated fluid flow should occur in the zone and must be rapid to ensure that the reaction is substantially completed within the extent of the band, which for example is typically 50mm deep.
• the invention in its broadest aspect includes a method of heating matter comprising supplying a gaseous mixture, which is reactable to produce heat, at a temperature above that at which spontaneous ignition occurs, to a heating zone such that the gaseous mixture reacts in said heating zone to provide a heated fluid flow therein, and supplying matter to be heated to said heating zone.
• the reaction utilised is a combustion reaction and the invention also includes a method of heating matter comprising supplying a combustible gaseous mixture at a temperature above that at which spontaneous ignition occurs to a heating zone such that a combustion reaction occurs in said heating zone to provide a heated fluid flow therein and supplying matter to be heated to said heating zone.
• a combustible air-gaseous fuel mixture is utilised and the invention further includes a method of heating matter comprising supplying a combustible air-gaseous fuel mixture at a temperature above that at which spontaneous ignition of the gaseous fuel occurs to a heating zone such that a combustion reaction occurs in said heating zone to provide a heated fluid flow therein, and supplying said matter to said heating zone.
• the invention is applicable to other methods of heating matter, it is especially applicable to the above-described method, in which case the matter to be heated is moved in a band continuously along an annular path in an annular zone by directing fluid flow into said zone over the annular extent thereof with both circumferential and vertical flow components, said fluid flow comprising said gaseous mixture over at least a portion of the annular extent of said zone, and the reaction thereof being substantially completed within the extent of said band.
• the fluid flow may comprise said gaseous mixture over the annular extent of said zone.
• the matter may comprise particulate material which forms a resident bed moving in said band along said annular path.
• the gaseous mixture may be directed into a first annular region of said annular zone, which region is contiguous with and disposed inwardly of a second annular region of said annular zone such that said reaction occurs substantially in said first annular region, and said matter is circulated between said regions whilst moving in said band.
• the gaseous mixture comprises an air- gaseous fuel mixture and the fluid flow is directed into said annular zone through an annular inlet comprising an annular array of fixed inclined vanes arranged in overlapping relationship, said gaseous fuel being mixed with heated air immediately upstream of respective passages defined between said vanes and combustion occurring downstream of said vanes.
• the air-gaseous fuel mixture is confined substantially to the region above the vanes by directing respective flows through said annular inlet at the radially inner and outer edges thereof with radially outwardly and radially inwardly flow components respectively.
• the gaseous fuel may comprise natural gas, and in an embodiment of the invention an air-natural gas mixture is supplied at a temperature greater than 700°C. The temperature of this mixture is obtained by mixing the natural gas with heated air at a temperature of less than about 1000°C, for example between 850 and 900°C.
• Figure 1 is a graph showing the effect of the temperature , of an air-gaseous fuel mixture on combustion rate
• Figure 2 is a schematic axial cross-section of an apparatus for heating matter
• Figure 3 is a cross-section along the line III- III of Figure 2;
• Figure 4 shows the portion indicated by IV in Figure 2 to a larger scale and in more detail than in Figure 2;
• Figure 5 is a section taken along the line V-V in Figure 4 showing four blades of the apparatus;
• Figure 6 is a top, part section view of three blades of the apparatus
• Figure 7 is a perspective view of a single blade of the apparatus
• Figure 8 is a schematic top plan view of another apparatus for heating matter.
• Figure 9 is an axial cross-section of the same apparatus taken along the line VIII-VIII of Figure 8.
• Figure 1 the effect of the temperature of a combustible air-gaseous fuel mixture prior to combustion on the rate of combustion is indicated.
• combustion of the mixture at the lowest temperature A is comparatively slower than combustion of the mixture at higher temperatures B and C, the temperature/time curves in the latter cases being substantially J-shaped, the temperature generated by the combustion rising rapidly soon af er combustion commences.
• an air gaseous fuel mixture is provided for combustion at a temperature above that at which dissociation of the fuel occurs so that rapid combustion is achieved.
• the illustrated apparatus comprises a chamber 10 having a circumferential wall 12 which is disposed radially outwardly of an annular inlet 14.
• the wall 12 slopes towards the annular inlet, and as shown comprises a cylindrical portion 16 extending upwardly from a sloping portion 18.
• the sloping portion 18 extends downwardly to the outer edge of the annular fluid inlet.
• Within the chamber 10 there is a first annular region disposed above the annular inlet and designated 22 in Figure 2 and a second annular region contiguous with the first annular region and disposed between that region and the circumferential wall 12. The second region is disposed above the sloping portion 18 of the wall in the embodiment.
• the apparatus also includes means for directing fluid through the annular inlet 14 with vertical and circumferential flow components.
• the direction of the fluid flow through the inlet is indicated in Figure 2 by arrows 26 and 28.
• the flow of fluid through the inlet is such that it will move matter in the chamber 10 in a band continuously along an annular path in the regions 22, 24. This matter is moved vertically and circumferentially whilst in the first region 22 by the flow of fluid therein, is moved out of this flow of fluid in the first region into the second region by circumferential force and is directed back into the first region by the slope 18.
• the movement of the matter into and out of the flow of fluid is indicated by arrows 30 in Figure 2.
• the chamber 10 includes a second circumferential wall 34 extending upwardly and disposed radially inwardly of the annular fluid inlet 14.
• This circumferential wall 34 has a slope towards the annular fluid inlet such that matter introduced centrally into the chamber as indicated by arrows 36 will be directed into the first annular region 22 above the annular fluid inlet 14. Whilst the whole of the second circumferential wall is provided with such a slope in the embodiment and this slope extends to the radially inner edge 38 of the annular fluid inlet 14, it is to be understood that only a portion of the circumferential wall 34 need be provided with such a slope and that slope need not extend to the edge 38.
• the means for directing fluid through the annular inlet 14 with vertical and circumferential flow components in the illustrated apparatus comprises an annular array of fixed inclined vanes 40 arranged in overlapping relationship, and defining therebetween respective flow passages 42 which extend vertically and circumferentially.
• a portion of the annular array of vanes is schematically illustrated in Figure 3, however it is to be understood that the array extends completely around the annular inlet 14.
• Each vane 40 is part of a respective blade 44 which is best shown in Figure 7. Adjacent blades 44 nest together as illustrated in Figures 5 and 6 so as to dispose the vanes in overlapping relationship with the passages therebetween. Each blade 44 is also provided with respective side vanes 46 and 48 extending upwardly from radially outer and radially inner sides of its vane 40. The side vanes 46 and 48 of the blades overlap to define therebetween respective flow passages 50 and 52.
• the vanes 46 and 48 are inclined towards each other and the flows through the passages 50 and 52 at the radially outer and inner edges of the inlet 14, indicated by arrows 28 in Figure 2, have radially inwardly and radially outwardly flow components respectively causing the flow through the passages 42, indicated by arrow 26 in Figure 2, to be confined substantially to the annular region 22 above the vanes 40.
• the blades are provided with radially outer and radially inner mounting portions 54 and 56, by which they are mounted on annular ledges 58 and 60 respectively radially outwardly and radially inwardly of the annular inlet 1 .
• the blades are provided with a ribbed portion 62 which extends vertically to the upstream ends of the vanes 40, 46 and 48.
• the ribs 64 of the portion 62 extend vertically and are provided on only one side of the portion 62 in the illustrated blade and define with the plain opposite side 66 of the portion 62 of an adjacent blade vertically extending flow passage means 68 communicating with the flow passages 42, 50 and 52 defined between that blade and the adjacent blade.
• Each blade is provided with a passage for receiving a gaseous fuel distributor, or so-called 'sparge', pipe 70.
• This passage comprises a bore 72 in an enlarged free end portion 74 of the mounting portion 54 and a slot 76 aligned with the bore 72 and extending therefrom through the remaining portion 78 of the mounting portion 54 into the ribbed portion 62 and terminating short of the mounting portion 56.
• the slot is completely open at the plain side 66 thereof but bridged at spaced apart locations by the ribs 64 at the other side.
• a pipe 70 is received in the passage therefor in alternate blades 44, each pipe being provided with radial openings arranged to supply gaseous fluid to the flow passages defined by the blade in which the pipe is fitted and the blades on each side of that blade.
• the pipes 70 are all connected via conduit means 80 to an annular gas header tube, or manifold, 82 disposed externally of the circumferential wall 12 of the chamber.
• heated air is caused to swirl about an annular chamber 84 beneath the annular inlet 14 and to flow through the passage means 68 defined between adjacent blades in the passages 42, 50 and 52 defined between the vanes of those blades.
• This air mixes with gaseous fuel from the pipes 70 to form a heated air-gaseous fuel mixture in the passage means 68 and this mixture is combusted in the annular region of 22 of the chamber 10 above the inlet 14.
• the air-gaseous fuel mixture is heated prior to combustion by the mixing of the gaseous fuel with the heated air to a temperature above that at which spontaneous ignition of the gaseous fuel occurs such that a rapid combustion reaction occurs as explained hereinbefore in connection with Figure 1.
• the rate of combustion is such that although the velocity of the air mixing with the fuel is greater than the flame propagation velocity thereof so that the resulting flow is able to move matter in a band along an annular path in the chamber 10, combustion occurs, and is substantially completed, within the extent of the band, that is before the mixture passes through the matter in the band. Additionally because the gaseous fuel is mixed with the air immediately upstream of the passages 42, most of the combustion occurs downstream of the blades 44 and accordingly they are not subjected to the full heat of the combustion reaction.
• the above-described embodiment is particularly applicable for use in heating matter comprising a particulate material which has to be heated to a predetermined temperature which is at or below the temperature at which fast combustion reactions occur, or which is adversely affected by being continuously subjected to temperatures above that predetermined temperature during treatment.
• the combustion reaction occurs substantially in the first annular region 22 in the chamber 10.
• the particulate matter to be heated is supplied to the chamber centrally thereof and is fed to the region 22 by the slope of the inner circumferential wall 34.
• This particulate material is then moved in a band continuously along an annular path in the regions 22 and 24.
• the particulate material is moved vertically and circumferentially by the fluid flow whilst in the first region, is moved out of the flow in the first region into the second region by circumferential force and is thereafter directed back into the first region by the slope 18 of the outer circumferential wall 12.
• the particulate material is moved in a band continuously around the regions 22, 24 whilst being circulated in this band between the regions such that the material moves into and out of the heated flow during movement around the regions.
• FIG. 8 and 9 there is illustrated an apparatus for heating matter which is similar to the apparatus illustrated in Figures 2 and 3. Accordingly like reference numerals in these figures designate like or similar parts.
• the annular inlet 14 is spanned by an annular array of inclined vanes 86 (only a portion of the array being shown in Figure 8) which are preferably arranged in overlapping relationship for directing fluid flow into the annular zone 88 above the inlet 14 with both circumferential and vertical flow components for moving a resident bed of particulate matter in the zone 88 continuously along an annular path in a compact band 90.
• Heated air is caused to swirl about annular chamber 84 beneath the inlet 14 and to flow between the vanes 86 into the zone 88.
• This air mixes with gaseous fuel from fuel pipes 70 immediately upstream of the vanes to form a heated air-gaseous fuel mixture which is combined in zone 88.
• the heated mixture prior to combustion is at a temperature above that at which spontaneous ignition of the gaseous fuel occurs such that a rapid combustion occurs.
• the rate of combustion is such that combustion is substantially completed within the extent of the band of particulate matter forming the resident -bed, thus efficiently heating -that matter.
• Further matter to be heated is either added to the resident bed or passed therethrough such that heat is transferred to the further matter from the heated particulate matter of the bed.
• This further matter may comprise gases, liquids or solids.
• the heated air-gaseous fuel mixture is passed through the bed along a portion of the annular extent of the zone 88 to heat the bed and the gas is passed through the bed along another portion of the annular extent of the zone 88 to be heated by the matter in the bed.
• One example of solid matter which may be heated by being added to the resident bed is fine powder.
• the apparatus and method described above in connection with Figures 8 and 9 may be used to heat matter, especially particulate matter directly without the use of a resident bed.
• matter to be heated is introduced into the zone 88 and is moved continuously along an annular path in a compact band by the passage of the heated fluid flow provided by the combustion of the heated air-gaseous fuel mixture through the matter whilst heating it.

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• Engineering & Computer Science (AREA)
• Chemical & Material Sciences (AREA)
• Mechanical Engineering (AREA)
• General Engineering & Computer Science (AREA)
• Dispersion Chemistry (AREA)
• Combustion & Propulsion (AREA)
• Resistance Heating (AREA)
• Control And Other Processes For Unpacking Of Materials (AREA)
• Physical Or Chemical Processes And Apparatus (AREA)
• Surface Heating Bodies (AREA)
• Manufacture, Treatment Of Glass Fibers (AREA)
• Devices And Processes Conducted In The Presence Of Fluids And Solid Particles (AREA)
• Air Bags (AREA)
• Glass Compositions (AREA)
• Ceramic Products (AREA)

Priority Applications (1)

Applications Claiming Priority (2)

Publications (1)

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Citations (3)

Family Cites Families (5)

• 1988
  • 1988-06-08 GB GB8813530A patent/GB2219521B/en not_active Expired - Fee Related
• 1989
  • 1989-06-01 WO PCT/GB1989/000603 patent/WO1989012202A1/en not_active Application Discontinuation
  • 1989-06-01 AU AU37434/89A patent/AU629556B2/en not_active Ceased
  • 1989-06-01 ES ES89305528T patent/ES2081841T3/es not_active Expired - Lifetime
  • 1989-06-01 EP EP89305528A patent/EP0346004B1/de not_active Expired - Lifetime
  • 1989-06-01 AT AT89305528T patent/ATE130082T1/de not_active IP Right Cessation
  • 1989-06-01 JP JP1506167A patent/JPH03504890A/ja active Pending
  • 1989-06-01 DE DE68924730T patent/DE68924730T2/de not_active Expired - Fee Related
  • 1989-06-01 EP EP89906416A patent/EP0418287A1/de active Pending
  • 1989-06-05 CA CA000601758A patent/CA1336389C/en not_active Expired - Fee Related
  • 1989-06-06 NZ NZ229428A patent/NZ229428A/xx unknown
  • 1989-06-06 ZA ZA894267A patent/ZA894267B/xx unknown
• 1995
  • 1995-12-29 GR GR950403700T patent/GR3018563T3/el unknown

Patent Citations (3)

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