Multi stage combustion furnace and process for the thermal expansion of mineral particles
09791147 · 2017-10-17
Assignee
Inventors
Cpc classification
F23C99/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C5/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C2900/07022
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C7/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C7/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E20/34
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
F24C1/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C7/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C5/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C99/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The present document describes a multistages combustion furnace system for thermal expansion of mineral particles which comprises: a furnace having an expansion chamber for receiving the mineral particles; a burner head to be connected at a distance for an atmospheric coupling of the furnace and for operating the multistages combustion furnace system; a furnace device to be connected at a distance for an atmospheric coupling of the burner head to offset the quenching effect of ambient air normally drawn in the furnace; and a tuyere for thermal expansion of mineral particles to be connected between the expansion chamber and the furnace device; wherein the multistage combustion furnace system is to be connected with an inlet of preheated air.
Claims
1. A multistage combustion furnace system for an open furnace for thermal expansion of mineral particles, the open furnace being open to atmosphere and comprising an expansion chamber for receiving the mineral particles, the multistage combustion furnace system comprising: a burner head connected at a burner distance from and below the expansion chamber for operating the expansion chamber, the burner distance providing an atmospheric coupling of the burner head and the expansion chamber with the atmosphere; a furnace device connected at a furnace device distance from and below the expansion chamber, in the atmosphere, the furnace device and the expansion chamber being installed separated by a gap extending below the expansion chamber, the gap being open to both the expansion chamber and the atmosphere, where unexpanded mineral can fall out of the open furnace, and to provide an atmospheric coupling of the furnace device and the expansion chamber with the atmosphere, the furnace device comprising a ring portion installed peripherally from said burner head and comprising a channel directed toward the gap to generate an air curtain extending through the gap to offset the quenching effect of ambient air from the atmosphere normally drawn in an open furnace, wherein said furnace device is installed between said burner head and a tuyere kit; and the tuyere kit connected between said expansion chamber and said furnace device at a lower portion of the expansion chamber, the tuyere kit comprising an air inlet installed inside said tuyere kit to provide a preheated air intake causing a tertiary combustion stage surrounding a burning flame with higher oxygen air; wherein an inlet of preheated air is connected to each one of the burner head and the furnace device.
2. The multistage combustion furnace system kit of claim 1, wherein the furnace device provides a controlled secondary combustion stage and an atmospheric coupling of said burner head with the tuyere kit.
3. The multistage combustion furnace system kit of claim 2, wherein said burner head is for fuel.
4. The multistage combustion furnace system kit of claim 3, wherein said fuel is oil.
5. The multistage combustion furnace system kit of claim 2, wherein said burner head is for gas.
6. The multistage combustion furnace system kit of claim 2, wherein said air curtain comprises preheated air.
7. The multistage combustion furnace system kit of claim 2, wherein said air curtain comprises preheated combustion air.
8. The multistage combustion furnace system kit of claim 2, wherein said ring portion is of a circular configuration.
9. The multistage combustion furnace system kit of claim 1, wherein said air inlet is to be positioned at a point where combustion takes place above a venturi in an atmospheric coupling.
10. The multistage combustion furnace system kit of claim 1, wherein said air inlet is to be positioned at a point where combustion takes place partly below a venturi in an atmospheric coupling.
11. The multistage combustion furnace system kit of claim 1, wherein said air inlet is to be positioned at a point where the flame front is already established to provide a tertiary combustion stage surrounding a burning flame.
12. The multistage combustion furnace system kit of claim 1, wherein said air inlet is to be positioned at a point for a gas flame pre-ignition.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Further features and advantages of the present disclosure will become apparent from the following detailed description, taken in combination with the appended drawings, in which:
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(23) It will be noted that throughout the appended drawings, like features are identified by like reference numerals.
DETAILED DESCRIPTION
(24) The present description relates to a multistage combustion furnace system and a process for the thermal expansion of mineral particles. The present description relates to a multistage combustion furnace system furnace for decreasing the energy consumption of the process for the thermal expansion of mineral particles.
(25) Now referring to the drawings, and more particularly to
(26) The hot tuyere 49 delivers the remaining air in a powerful ring jet portion 58 fully surrounding the emerging flame front rising up against the falling particles in counter current mode. As combustion progresses, the hot gases produced interact with a steady stream of mineral particles fed directly into the expansion chamber 18 above and into the flame for heat treating or expansion as the case may be. The expanded minerals rise up the multistage combustion system furnace 12 with the process air from air inlets 42, 44 and 46 while unexpanded and heavier matter simply falls out the bottom of the expansion chamber 18 of the multistage combustion furnace system 12 through the venturi 43 (extend line to reach the center of the venturi) or is ejected from the open port 15 and falls to the ground for later pickup and disposal. The furnace system 12 exhaust gases have sufficient velocity to carry the now lightweight material out the top of the multistage combustion furnace system 12. The hot exhaust gas then enters a double wall rotating drum having raw ore flowing through the inner cylinder and hot exhaust with expanded particulate matter flowing through the space formed by the fixed shell and rotating drum for ore preheating prior to entering the multistage combustion furnace system 12. Expanded material is separated from the exhaust air by a cyclone, settling chamber or other suitable collector, where after the particles are cooled and packaged or stored.
(27) Exhaust air leaves the furnace top at about 1 832° F. or about 1000° C., in the case of perlite. Due mainly to air leaks in the rotary heater, through slip flanges and radiation losses, the air temperature drops to about 1000 to about 1,200° F. (about 538-about 650° C.). The heat exchanger 56 is positioned after both the ore preheater and product separator so as to protect the heat transfer elements from undue abrasive wear. The hot air expelled from the multistage combustion furnace system 12 is further diluted with cold air bleed-in ducts in order to protect the bag filter and fan from high temperature. The multistage combustion furnace system 12 operates under negative pressure so that all openings draw cold air in.
(28) The typical perlite furnace uses more combustion air than is necessary for expansion. The high value of excess air is the result of the natural suction produced by the high velocity flow of the air fuel mixture through the venturi 43 without a hot air ring or furnace device. Far greater thermal efficiency can be obtained by reducing the air flow that enters the system 10 to just above the stochiometric or theoretical levels required to burn the fuel instead of the 40-60% excess air as typical of conventional furnaces. Because the process 10, having a hot air ring or furnace device 45 and hot tuyere 49, needs very little excess air, fuel consumption and exhaust air heat losses are significantly reduced. As a result of using near stoichiometric air to fuel ratios, the flame burns hotter, more evenly and intensively and it glows brighter. At this point, mineral particles expand in a more lively fashion resulting in higher volume output for the same feed input of particles. Moreover, the production rate goes up, while the specific fuel consumption goes down which translates into higher production using less fuel. This positively affects all plant inputs: mineral ore mass, fuel consumption and labor.
(29) Still referring to
(30) Preheated air 13 that is required for combustion of fuel or gas and lift for the expanded mineral particles is supplied by the combustion air fan 40. Ducts direct this air to the heat exchanger 56 which transfers heat from the hot exhaust air 17 to the combustion air 19.
(31) Now referring to
(32) Now referring to
(33) In the furnace device 45 as described above, the air drawn may be preheated combustion air 13. It is also to be noted that the ring jet portion 48 may be circular. Moreover, the ring jet portion 48 of the multistage combustion furnace system 12 may be made of a metallic material suitable for the temperature encountered. Additionally, the multistage combustion furnace system 12 operates with a neutral pressure point above the flame.
(34) Now referring to
(35) In the case of oil fired multistage combustion furnace systems, an additional flat disc may be fitted to the crossbars of the venturi crown 50. In another embodiment, the inclined elements or radial elements 52 have a V-shaped cross section with the apex on the upper side so that the radial elements 52 form an inclined channel to radially distribute the preheated air 13 across the shearing force of the annular air curtain. The venturi crown 50 adds turbulence to the combustion process and positively contributes to the intimate mixing of the centrally rich air fuel cloud with the remainder of the combustion air as supplied by the annular air curtain.
(36) Now referring to
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(41) The process 10 and the furnace system 12 can be used with both liquid and gaseous fuels however, there are significant differences in the venturi 43 and annulus area 58 and in the velocity through the hot air ring device, or furnace device 45. The rest of the process 10 and of the furnace system remains the same system as described above.
(42) In the case of the oil-fired multistage combustion furnace system 12 as shown in
(43) The pre-heated air 13 initiates fuel oil evaporation providing a higher energy state before the combustion chamber above the venturi 43. This method of fuel/air preparation provides excellent conditions for complete combustion. The three stages combustion air inlets (inlet 42, 44 and 46) allows the operator to control the air to fuel ratio at three points; in the traditional burner head 47, at the atmospheric coupling via the hot air ring (or furnace device 45) and above the venturi 43 in the furnace system 12. It has been found that perlite expansion increases by 10 to 20% when the central air rising up across the atmospheric coupling into the venturi 43 is near half of the air required for complete combustion. This results in an extremely fuel rich and hot fuel cloud entering the furnace system 12 through the venturi 43 (inlet 46). Final combustion air enters the final firing zone in a high speed annulus surrounding the fuel cloud as it emerges vertically up from the venturi 43.
(44) On the other hand, with a gas-fired furnace system 12, there is no need for any flow restrictor (venturi crown 50) across the venturi since the fuel is perfectly miscible in the air by its nature. Also, with gaseous fuel, combustion begins below the venturi 43 (below inlet 46) and traditionally this presents operational problems defined as flame spill. With any significant gas burning in the region of the atmospheric coupling, a pressure wave results from the expanding gas that acts in all directions. Flame spilling pushes gas away from the center where it is falling away from the pressure pull of the venturi 43 (inlet 46) and is fuel lost to the process 10.
(45) This problem is alleviated by greatly reducing the amount of air delivered below the venturi 43 (below inlet 46). It is advantageous to split the three pre-heated combustion air inlets 42, 44 and 46 as follows: about 5-15% of the preheated air 13 to the hot air ring device (or furnace device 45) to fill the atmospheric coupling (inlet 44), about 20-30% through the burner head 47 (inlet 42) and the balance, being the major portion, up through the annulus area 58 of the venturi 43 (inlet 46). This results in a larger annulus 58 (inlet 46) than required for oil fired furnace systems 12. Additionally, it is advantageous to provide air jets in rings supplying oxygen rich air at the base of the flame inside the tuyere 49. For example,
(46) Moreover, flame spills are further abated in gaseous systems by increasing the exit velocity of the air leaving the hot air ring device (or furnace device 45) compared to the case when burning fuel oil.
(47) The process 10 and the furnace system 12 provides the ability to keep the air fuel mixture seriously oxygen deficient below the venturi 43 thereby reducing flame spill as an inefficiency factor and reserving the needed oxygen for addition to the burning air/fuel mixture above the venturi inside the tuyere 49.
(48) It is to be noted that the pre-heated air 13 is returned to the base of the furnace system 12 where it is split into three adjustable streams in the air inlets. The major portion is supplied to the burner head 47; secondly a hot air curtain peripherally extends the burner head 47 to replace the ingress of cold air between the burner head 47 and venturi 43 with now preheated air 13 freely obtained via the heat exchanger 56; the third air input enters the hot tuyere 49 above the established flame to provide a tertiary combustion stage surrounding the richly burning flame with higher oxygen lean air enveloping the advancing fuel cloud. Together with the automatic pressure control acting on the exhaust air drawn through the furnace system 12 the combustion thus achieved, having three stages of air admission advantageously arranged beginning at the center of the burner head 47, and peripherally above the burner head 47 and finally above the venturi 43 throat surrounding the rapidly evolving rising flame front is more uniform and complete, burning more powerfully than ever before and this produces a greater expansion effect in the mineral particles. In the case of perlite the expanded material produced is lighter as evidenced by a reduction in bulk density. Production rates go up in consequence. The invention saves fuel, ore and production time.
(49) The furnace exhaust air 17 leaving the heat exchanger will be at a lower air temperature than before, so that the air temperature in the bag house filter will be reduced by a significant degree leading to longer bag life and lower maintenance costs.
(50) Then, it is well known that inputs to any expanded mineral expansion process in order of costs are mineral ore, fuel (typically natural gas, propane or oil) and labour. At the opposite, the major output will be expanded mineral particles measured by volume.
(51) The present invention will be more readily understood by referring to the following examples which are given to illustrate the invention rather than to limit its scope.
Example 1
Perlite Production
(52) The process 10 of
(53) While preferred embodiments have been described above and illustrated in the accompanying drawings, it will be evident to those skilled in the art that modifications may be made without departing from this disclosure. Such modifications are considered as possible variants comprised in the scope of the disclosure.