METHOD AND SYSTEM FOR THE THERMAL TREATMENT OF DISPERSIBLE RAW MATERIAL
20170260089 · 2017-09-14
Assignee
Inventors
Cpc classification
Y02E20/30
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
C04B7/4446
CHEMISTRY; METALLURGY
F27B7/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F27B7/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23G2206/201
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F27B7/34
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F27B7/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A method for the thermal treatment of dispersible raw material may inovlve introducing raw material into a riser tube that is perfused by hot gases and thermally treating the raw material with the hot gases. Furthermore, the method may inovle feeding a fuel to the riser tube. The fuel may initially dwell in a fuel-conditioning region on a bearing face, where the fuel comes into contact with a part of the hot gas that is mixed with the raw material. Consequently, the fuel is dried and/or at least partially de-gassed and/or at least partially reacted and subsequently transferred into the riser tube.
Claims
1.-12. (canceled).
13. A method for thermal treatment of dispersible raw material, the method comprising: introducing raw material into a riser tube that is perfused by hot gases; thermally treating the raw material in the riser tube with the hot gases; feeding a fuel into a fuel-conditioning region and onto a bearing face disposed in a conditioning chamber that leads into the riser tube, wherein at least 50% of the hot gases that come into contact with the fuel is formed by a part of the hot gases that is mixed with the raw material and deflected into the conditioning chamber, whereby as a result the fuel is at least one of dried, partially or completely de-gassed, or partially or completely reacted; and transferring the fuel into the riser tube.
14. The method of claim 13 wherein the fuel is fed onto the bearing face mechanically or by gravity.
15. The method of claim 13 further comprising conveying the dried, partially or completely de-gassed, or partially or completely reacted fuel mechanically or pneumatically along the bearing face before being transferred into the riser tube.
16. The method of claim 13 further comprising setting in a targeted manner an amount of the hot gases that is mixed with the raw material and comes into contact with the fuel in the fuel-conditioning region by adding an oxygen-containing gas.
17. The method of claim 13 further comprising decelerating or completely stopping a combustion reaction of the fuel on the bearing face by using an inert material.
18. A system for thermal treatment of dispersible raw material, the system comprising: a riser tube that is perfusable by hot gases; means for introducing raw material into the riser tube; and a fuel-conditioning region that comprises means for adding fuel, a bearing face for the fuel, and means for conveying the fuel along the bearing face and transferring the fuel into the riser tube, wherein the fuel-conditioning region is connected to the riser tube such that a part of the hot gases that is mixed with the raw material reaches the fuel-conditioning region and comes into contact with the fuel, whereby the fuel is at least one of dried, partially or completely de-gassed, or partially or completely reacted.
19. The system of claim 18 wherein the means for adding the fuel comprises at least one of a spiral conveyor, a gate, a pump, a tappet, a chute, a cellular wheel sluice, or a flap system.
20. The system of claim 18 wherein the means for conveying and transferring the fuel into the riser tube are formed in a shape of at least one of: gates or tappets for mechanically conveying, or air-surge apparatuses or blowers for pneumatic conveying.
21. The system of claim 18 further comprising a propulsion jet nozzle disposed in the fuel-conditioning region for deflecting the part of the hot gases that is mixed with the raw material into the fuel-conditioning region.
22. The system of claim 18 wherein a ratio of a diameter of the riser tube to a depth of the bearing surface is in a range from 5 to 1.5. (New) The system of claim 18 wherein a ratio of a diameter of the riser tube to a depth of the bearing surface is in a range from 5 to 1.5.
23. The system of claim 18 wherein a ratio of a diameter of the riser tube to a depth of the bearing surface is in a range from 5 to 1.5. (New) The system of claim 18 wherein a ratio of a diameter of the riser tube to a depth of the bearing surface is in a range from 3 to 1.5.
24. The system of claim 18 wherein the bearing face comprises at least one of: at least two successive steps, or a table and a step that adjoins the table.
25. The system of claim 18 wherein the fuel-conditioning region comprises a conditioning chamber configured in a portion of the riser tube that is disposed so as to be oblique to a vertical, wherein the bearing face comprises an outwardly offset wall region of the riser tube.
Description
[0021] Further advantages and design embodiments of the invention will be explained in more detail by means of the following description of a few exemplary embodiments and of the drawing.
[0022] In the drawing:
[0023]
[0024]
[0025]
[0026]
[0027] Various exemplary embodiments for the configuration of the calcinator are shown by means of
[0028] The system for the thermal treatment of dispersible raw material that is illustrated in the
[0029] The fuel 11 is pushed onto the bearing face 7 by way of the means 10. The raw material 4 to be thermally treated is fed in a lower region of the riser tube 1 by way of the means 3. Furthermore, oxygen-containing combustion air 8 (for example cooler exhaust air 107, according to
[0030] A bunker 9 for an inert material 9a can furthermore be provided, so as to decelerate or largely bring to a stop the as yet continuing fuel reaction by covering the fuel bed with an inert material (for example sand or limestone meal), for example in the case of sudden stopping of the system.
[0031] The fuel that is dropped into the riser tube 2 is entrained by the hot gas and is further reacted or combusted, respectively. The effect of the “reverse flow”, in which the part 1a of the hot gases 1 that flow upward in the riser tube 2 reaches the conditioning chamber 6, is in this instance achieved in a particularly effective manner when the ratio of the diameter D of the riser tube 2 to the depth T of the bearing face 7 of the fuel in the fuel-conditioning region 5 is in the range of 5>D/T>1.5, preferably of 3>D/T>1.5.
[0032]
[0033] Furthermore, means 19′ for conveying the fuel 11′ along the bearing face 7′ are provided in the exemplary embodiment illustrated, which means 19′ here are formed by a gate. Air-surge apparatuses 15′, 16′ are again provided in the region of the steps. This oblique arrangement of the table 7′a has the advantage that conveying of the fuel 11′ is facilitated. Moreover, the deflection of a part 1′a of the hot gas 1′ that is mixed with the raw material 4′ can be facilitated by this geometry of the conditioning chamber 6′. In order for this deflection to be further facilitated, propulsion jet nozzles 20′ which are aligned in such a manner that the latter induct a part of the hot gases 1′ that are blended with the raw material 4′ into the conditioning chamber 6′ are provided in the region of the conditioning chamber 6.
[0034] A particularly efficient reaction of the fuel in the region of the fuel-conditioning region 5, 5′ results when the ratio of the height H of the fuel-conditioning region to the depth T of the bearing face is between 0.5 and 2, preferably 0.75 and 1.5. If the bearing face 7, 7′, as is the case with the two exemplary embodiments, is formed by one table 7a, 7′a and at least one step 7b, 7c, 7′b, 7′c adjoining the latter, the depth t of the step is preferably 0.2 to 1 times, preferably 0.2 to 0.6 times, the depth t.sub.T of the table. A value between 0.5 and 2.5, preferably 1 and 2, has proven advantageous for the ratio of the width to the depth T of the bearing face 7, 7′.
[0035] In the case of the exemplary embodiment according to
[0036] In the context of the invention, the design embodiments shown in the three exemplary embodiments, such as the design embodiment of the bearing face, for example, or the type of feeding and conveying of the fuel, can be arbitrarily combined with one another.