EP0015037A1 - Apparatus for the gasification of coal powder - Google Patents
Apparatus for the gasification of coal powder Download PDFInfo
- Publication number
- EP0015037A1 EP0015037A1 EP80200134A EP80200134A EP0015037A1 EP 0015037 A1 EP0015037 A1 EP 0015037A1 EP 80200134 A EP80200134 A EP 80200134A EP 80200134 A EP80200134 A EP 80200134A EP 0015037 A1 EP0015037 A1 EP 0015037A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- rotor
- casing
- pump
- powder
- inlet
- 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.)
- Granted
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Classifications
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- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10J—PRODUCTION OF PRODUCER GAS, WATER-GAS, SYNTHESIS GAS FROM SOLID CARBONACEOUS MATERIAL, OR MIXTURES CONTAINING THESE GASES; CARBURETTING AIR OR OTHER GASES
- C10J3/00—Production of combustible gases containing carbon monoxide from solid carbonaceous fuels
- C10J3/46—Gasification of granular or pulverulent flues in suspension
- C10J3/48—Apparatus; Plants
- C10J3/50—Fuel charging devices
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- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10J—PRODUCTION OF PRODUCER GAS, WATER-GAS, SYNTHESIS GAS FROM SOLID CARBONACEOUS MATERIAL, OR MIXTURES CONTAINING THESE GASES; CARBURETTING AIR OR OTHER GASES
- C10J3/00—Production of combustible gases containing carbon monoxide from solid carbonaceous fuels
- C10J3/46—Gasification of granular or pulverulent flues in suspension
- C10J3/48—Apparatus; Plants
- C10J3/485—Entrained flow gasifiers
- C10J3/487—Swirling or cyclonic gasifiers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D23/00—Other rotary non-positive-displacement pumps
- F04D23/001—Pumps adapted for conveying materials or for handling specific elastic fluids
- F04D23/003—Pumps adapted for conveying materials or for handling specific elastic fluids of radial-flow type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23K—FEEDING FUEL TO COMBUSTION APPARATUS
- F23K3/00—Feeding or distributing of lump or pulverulent fuel to combustion apparatus
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- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10J—PRODUCTION OF PRODUCER GAS, WATER-GAS, SYNTHESIS GAS FROM SOLID CARBONACEOUS MATERIAL, OR MIXTURES CONTAINING THESE GASES; CARBURETTING AIR OR OTHER GASES
- C10J2200/00—Details of gasification apparatus
- C10J2200/15—Details of feeding means
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- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10J—PRODUCTION OF PRODUCER GAS, WATER-GAS, SYNTHESIS GAS FROM SOLID CARBONACEOUS MATERIAL, OR MIXTURES CONTAINING THESE GASES; CARBURETTING AIR OR OTHER GASES
- C10J2200/00—Details of gasification apparatus
- C10J2200/15—Details of feeding means
- C10J2200/158—Screws
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- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10J—PRODUCTION OF PRODUCER GAS, WATER-GAS, SYNTHESIS GAS FROM SOLID CARBONACEOUS MATERIAL, OR MIXTURES CONTAINING THESE GASES; CARBURETTING AIR OR OTHER GASES
- C10J2300/00—Details of gasification processes
- C10J2300/18—Details of the gasification process, e.g. loops, autothermal operation
- C10J2300/1846—Partial oxidation, i.e. injection of air or oxygen only
Definitions
- the invention relates to a centrifugal pump for the introduction of powder into a pressurized space, comprising an inlet and a rotor, the inlet leading to the centre of the rotor and the rotor having one or more essentially radial passages normal to the axis of rotation which passages communicate with the said inlet and are open at their outward extremity.
- Such pumps are known from the U.S. patent specifications Nos. 2,822,097; 3,182,825; 4,049,133 and 4,120,410 and act as ejecting centrifugal pump, i.e. the powder is ejected by the rotor at high velocity into a large vessel, in which vessel the velocity of the particles is reduced to zero.
- These pumps are used, for example, to introduce pulverulent solid fuel into a pressurized vessel, such as coal powder which is passed via a vessel to a reactor for the partial combustion of coal which reactor is connected to the vessel.
- the pressure in the vessel is usually at least 10 atm. and the pump serves to introduce the coal powder which is at atmospheric pressure into the vessel against the pressure difference.
- the velocity at which the particles leave the rotor is high, in the order of 100 m/sec. in a tangential direction and 10 m/sec. in a radial direction.
- the present invention envisages the removal of these disadvantages and to this end proposes surrounding the rotor by a casing of which the radial distance to the rotor increases in the direction of rotation to a point at which the casing leads away from the rotor in a tangential direction.
- the resultant space between the rotor and the casing ensures optimum retention of momentum of the medium ultimately leaving the pump, i.e., the powder particles optimally retain the initial tangential velocity component in the said space and also the gas entrained by the particles optimally assumes this velocity.
- both sides of the casing may border the lateral faces of the rotor at which locations some clearance may be left between casing and rotor and/or a seal may be provided between casing and rotor.
- gas inlets are preferably present in the casing which issue into the clearance between the casing and the lateral faces of the rotor. This has the advantage that the powder which finds its way into these spaces is blown back into the space of the casing situated radially outside the rotor.
- the casing is advantageously provided with one or more gas inlets tangentially issuing into the space around the rotor.
- the gas which may be injected or drawn in through these gas inlets is then accelerated by the powder particles. It will be evident that providing these gas inlets in the pump will augment the controllability of the powder flow since there will be a degree of freedom in respect of the quantity of gas supplied and of the initial pressure and velocity of this gas.
- Centrifugal pumps of the type according to the invention are very suitable for the supply of pulverulent solid fuel to a reactor for the partial combustion of this powder at elevated pressure, either by having the pump directly connected to a burner debouching into the reactor or by having the pump introduce the powder into a high pressure-operated fluidization vessel from which the fluidized powder is supplied to the burner.
- casing may also consist of more than two identical parts.
- An advantage of directly connecting the burner(s) to the pump resides in the fact that the velocity of the powder particles is not reduced to zero on their way from the pump to the reactor (as was the case in the above-mentioned state of the art), so that the powder particles need not be accelerated again.
- the part or each part of the casing leading tangentially away from the rotor is preferably designed as a diffuser.
- the space in the pump between casing and rotor may have any suitable cross-section, for example a rectangular or more rounded profile. It will be clear that the part of the casing which leads tangentially away from the rotor will have a cross-sectional shape which will gradually change from that of the said space into a circular shape (if the cross-section of the said space is not also circular). If a diffuser is used, it may provide the gradual change.
- the invention also relates to a method for the partial combustion.
- c pulverulent solid fuel at elevated pressure, in which method the powder is passed either directly or via an intermediate vessel to the reactor for partial combustion through a centrifugal pump according to the invention.
- the exclusive right also pertains to an apparatus for the partial combustion of pulverulent solid fuel at elevated pressure, comprising a reactor into which one or more burners debouch, the burner(s) being connected either directly or via an intermediate vessel to a pump according to the invention.
- the centrifugal pump depicted in Figs. 1 and 2 comprises a flat snail-shell shaped casing 1 on a pedestal 2 and provided with a diffuser-shaped discharge 3, a central inlet 4 and a central bearing housing 5.
- a flat, disc- shaped rotor 6 is present, the rotation shaft 7 of which coincides with the axis of the inlet 4 and with the axis of the bearing housing 5.
- Three radial passages 10 connect the centre 8 with the circumference 9 of the rotor, which passages, in the centre 8, communicate with an axial bore 11 which extends from the centre to the left-hand lateral face 12 of the rotor and communicates with the inlet 4 of the casing 1.
- a central drive shaft 14 which passes through the bearing housing 5 and Which is provided with a drive 15.
- the lateral faces 12 and 13 of the rotor 6 run clear of the inner wall of the casing 1, since both faces are provided at 16 and 17 with a shoulder.
- the disc 6 is rotatably mounted on bearings in the casing 1 (in a manner not shown in the drawing) and these bearings are sealed against coal powder.
- the gaps 18 between the lateral faces 12 and 13 of the rotor and the casing are sealed against the powder to be transported which may find its way into the gaps from the space 3, by gas supplied through the inlet openings 19.
- the inlet 4 of the casing is provided with a funnel-shaped connection 20 which may be connected to a bunker with powder by means of a flange 21.
- a worm screw 22 with drive 23 is arranged in the tubular inlet 4.
- the powder is passed through the tube 4 via the funnel 20 by means of the rotating screw 22. Together with the powder an inert gas, such as cold recirculated product gas from the partial combustion of the coal powder, is supplied from the space (not shown) connected to the funnel 20.
- an inert gas such as cold recirculated product gas from the partial combustion of the coal powder
- the powder and the entrained gas thus find their way into the centre 8 of the rotor 6 via the passage 11.
- the particles and the entrained gas are forced from the centre 8 to the open extremities 24 of the radial passages 10 under the influence of the centrifugal force, from which extremities the particles leave the rotor at high velocity.
- the tangential velocity of the particles upon leaving the rotor is more than 20 m/sec., and is mostly in the order of 100 m/sec.
- the space 25 between the rotor 6 and the casing 1 is formed in such a way that, starting from the highest point 26 in the direction of rotation 27, the radial distance 28 between the circumference 9 of the rotor 6 and the inner side of the wall 29 of the casing increases gradually to the point (in this case the same point 26) at which the space leads tangentially away from the rotor, i.e. the line I-I in Fig. 2 where the diffuser 3 begins.
- Each of the passages 1C in the rotor 6 will at any point during the rotation of the rotor eject powder into the space 25 in an essentially tangential direction so that the initial flow of powder which is entrained from point 26 in the direction 27 of the rotor 6 gradually increases in volume. Little velocity is lost by the powder on its way throngh the space 25.
- the cross-section of the diffuser is at thai point essentially rectangular (see Fig. 1), whereas at the end of the diffuser (at the level of the flange 30) the cross-section is larger and circular.
- This transition and'the flange 30 serve to connect the pump as apparatus for the supply of powder.
- the velocity of the particles decreases and the pressure of the gas entrained with the particles increases.
- Fig. 3 is a very diagrammatic representation of a cross-section, comparable with Fig. 2, of a double-acting pump according to the invention.
- the rotor 31 again comprises a disc which is rotatably mounted on bearings around a shaft in a casing.
- the casing comprises two walls 32 and 33 which are complementary and each surround the rotor 31 for 180°.
- the rotor 31 and the wall 32 enclose a space 34 which diverges in the direction of rotation 35 and which at 36 joints with a diffuser 37
- the rotor 31 and wall 33 enclose a space 38 which diverges in the direction of rotation 35 and which at 39 joints with a diffuser 40. Seen along the circumference of the rotor, the space 34 begins where the space 38 ends and vice versa.
- the rotor 31 has a central powder inlet 41 and two radial passages 42 and 43 which in turn eject powder (and gas) into the space 34 and 38, respectively, during rotation of the rotor.
- FIG. 4 depicts a single-acting pump of which the rotor 44 has four radial passages 45 and of which the casing 46 is provided with a number of gas-supply nozzles 48 which tangentially issue into the space 47 between casing and rotor.
- the gas introduced into the space 47 through these nozzles 48 is accelerated in said space under the influence of the powder which is ejected into the space 47 by the rotor 44.
- the gas may be drawn in by the space 47 or be injected into it at the required initial velocity.
- influence may be exerted on the pressure and/or the velocity of the gas/powder mixture leaving the diffuser 49.
- the quantity of gas and/or the velocity of the gas may be adapted to the rotational velocity of the rotor 44.
- the shape of the rotor may, for example, consist of two discs between which the radial passage comprises a single slot
- the rotor may, for example, consist of two discs between which the radial passage comprises a single slot
- the feed and drive of the pump shown may, of course, also be effected in a different manner.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Organic Chemistry (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Air Transport Of Granular Materials (AREA)
Abstract
Description
- The invention relates to a centrifugal pump for the introduction of powder into a pressurized space, comprising an inlet and a rotor, the inlet leading to the centre of the rotor and the rotor having one or more essentially radial passages normal to the axis of rotation which passages communicate with the said inlet and are open at their outward extremity.
- Such pumps are known from the U.S. patent specifications Nos. 2,822,097; 3,182,825; 4,049,133 and 4,120,410 and act as ejecting centrifugal pump, i.e. the powder is ejected by the rotor at high velocity into a large vessel, in which vessel the velocity of the particles is reduced to zero. The powder is passed to the centre of the rotor via the inlet and moves i= the rotor by the effect of the centrifugal force through the radial passages away from the centre of the rotor in an outward direction and finally leaves these passages through the open extremity with a radial and tangential velocity component.
- These pumps are used, for example, to introduce pulverulent solid fuel into a pressurized vessel, such as coal powder which is passed via a vessel to a reactor for the partial combustion of coal which reactor is connected to the vessel. The pressure in the vessel is usually at least 10 atm. and the pump serves to introduce the coal powder which is at atmospheric pressure into the vessel against the pressure difference. Under these conditions the velocity at which the particles leave the rotor is high, in the order of 100 m/sec. in a tangential direction and 10 m/sec. in a radial direction.
- The energy invested in this velocity has so far not been put to'further use, which is a drawback. Besides, it may under certain conditions be disadvantageous for the powder particles to be subjected to a rise in temperature by the friction caused by rapid deceleration in the equipment described in the above-mentioned patent specifications.
- The present invention envisages the removal of these disadvantages and to this end proposes surrounding the rotor by a casing of which the radial distance to the rotor increases in the direction of rotation to a point at which the casing leads away from the rotor in a tangential direction. The resultant space between the rotor and the casing ensures optimum retention of momentum of the medium ultimately leaving the pump, i.e., the powder particles optimally retain the initial tangential velocity component in the said space and also the gas entrained by the particles optimally assumes this velocity.
- In this respect it is essential that starting from the point where the distance between rotor and casing is smallest - seen in the direction of rotation - the space becomes larger as the rotor ejects more powder into the space.
- In the axial direction both sides of the casing may border the lateral faces of the rotor at which locations some clearance may be left between casing and rotor and/or a seal may be provided between casing and rotor.
- If some clearance is left between the casing and the lateral faces of the rotor, gas inlets are preferably present in the casing which issue into the clearance between the casing and the lateral faces of the rotor. This has the advantage that the powder which finds its way into these spaces is blown back into the space of the casing situated radially outside the rotor.
- The casing is advantageously provided with one or more gas inlets tangentially issuing into the space around the rotor. The gas which may be injected or drawn in through these gas inlets is then accelerated by the powder particles. It will be evident that providing these gas inlets in the pump will augment the controllability of the powder flow since there will be a degree of freedom in respect of the quantity of gas supplied and of the initial pressure and velocity of this gas.
- Centrifugal pumps of the type according to the invention are very suitable for the supply of pulverulent solid fuel to a reactor for the partial combustion of this powder at elevated pressure, either by having the pump directly connected to a burner debouching into the reactor or by having the pump introduce the powder into a high pressure-operated fluidization vessel from which the fluidized powder is supplied to the burner.
- Especially in the case of reactors in which two burners are arranged diametrically opposite each other in the wall it is important for both burners to be invariably fed in an identical manner. Particularly in this instance it is most advantageous to provide the pump, if it is directly connected to the burners, with a casing consisting of two identical halves each surrounding half of the rotor and of which casing the radial distance to the rotor increases in an equal manner up to the point where the casing half leads tangentially away from the rotor. Now if each casing half is connected to a burner, there is a high degree of certainty that both burners will be equally loaded.
- It will be obvious that the casing may also consist of more than two identical parts.
- An advantage of directly connecting the burner(s) to the pump resides in the fact that the velocity of the powder particles is not reduced to zero on their way from the pump to the reactor (as was the case in the above-mentioned state of the art), so that the powder particles need not be accelerated again.
- In order to produce an increase in pressure of the gases entrained by the powder, according to the invention, the part or each part of the casing leading tangentially away from the rotor is preferably designed as a diffuser.
- As is known the cross-section of a diffuser increases in the direction of flow and the velocity of the. gas flowing through the diffuser decreases while the pressure increases.
- The space in the pump between casing and rotor may have any suitable cross-section, for example a rectangular or more rounded profile. It will be clear that the part of the casing which leads tangentially away from the rotor will have a cross-sectional shape which will gradually change from that of the said space into a circular shape (if the cross-section of the said space is not also circular). If a diffuser is used, it may provide the gradual change.
- The invention also relates to a method for the partial combustion. c= pulverulent solid fuel at elevated pressure, in which method the powder is passed either directly or via an intermediate vessel to the reactor for partial combustion through a centrifugal pump according to the invention.
- The exclusive right also pertains to an apparatus for the partial combustion of pulverulent solid fuel at elevated pressure, comprising a reactor into which one or more burners debouch, the burner(s) being connected either directly or via an intermediate vessel to a pump according to the invention.
- The invention will now be further elucidated with reference to the attached drawing, to which it is not restricted.
- Fig. 1 of the drawing is a schematic representation of an axial cross-section of a centrifugal pump according to the invention;
- Fig. 2 of the drawing is a cross-section taken on plane II-II of Fig. 1;
- Fig. 3 of the drawing is a schematic representation of a "double-acting" pump according to the invention; and
- Fig. 4 of the drawing is a schematic representation of a pump with gas inlets according to the invention.
- The centrifugal pump depicted in Figs. 1 and 2 comprises a flat snail-shell shaped
casing 1 on apedestal 2 and provided with a diffuser-shaped discharge 3, acentral inlet 4 and a central bearinghousing 5. Within the casing 1 a flat, disc-shaped rotor 6 is present, therotation shaft 7 of which coincides with the axis of theinlet 4 and with the axis of thebearing housing 5. - Three
radial passages 10 connect thecentre 8 with thecircumference 9 of the rotor, which passages, in thecentre 8, communicate with anaxial bore 11 which extends from the centre to the left-handlateral face 12 of the rotor and communicates with theinlet 4 of thecasing 1. - At the side of the right-hand
lateral face 13 of the rotor there is acentral drive shaft 14 which passes through the bearinghousing 5 and Which is provided with adrive 15. The 12 and 13 of thelateral faces rotor 6 run clear of the inner wall of thecasing 1, since both faces are provided at 16 and 17 with a shoulder. At the 16 and 17 theshoulders disc 6 is rotatably mounted on bearings in the casing 1 (in a manner not shown in the drawing) and these bearings are sealed against coal powder. Thegaps 18 between the 12 and 13 of the rotor and the casing are sealed against the powder to be transported which may find its way into the gaps from thelateral faces space 3, by gas supplied through theinlet openings 19. - The
inlet 4 of the casing is provided with a funnel-shaped connection 20 which may be connected to a bunker with powder by means of aflange 21. In order to ensure uninterrupted supply of powder to thecentre 8 of the rotor, aworm screw 22 withdrive 23 is arranged in thetubular inlet 4. - The operation of the centrifugal pump depicted in Figs. 1 and 2 is as follows.
- The powder is passed through the
tube 4 via thefunnel 20 by means of the rotatingscrew 22. Together with the powder an inert gas, such as cold recirculated product gas from the partial combustion of the coal powder, is supplied from the space (not shown) connected to thefunnel 20. - The powder and the entrained gas thus find their way into the
centre 8 of therotor 6 via thepassage 11. In the rotating rotor the particles and the entrained gas are forced from thecentre 8 to theopen extremities 24 of theradial passages 10 under the influence of the centrifugal force, from which extremities the particles leave the rotor at high velocity. The tangential velocity of the particles upon leaving the rotor is more than 20 m/sec., and is mostly in the order of 100 m/sec. - The
space 25 between therotor 6 and thecasing 1 is formed in such a way that, starting from thehighest point 26 in the direction ofrotation 27, theradial distance 28 between thecircumference 9 of therotor 6 and the inner side of thewall 29 of the casing increases gradually to the point (in this case the same point 26) at which the space leads tangentially away from the rotor, i.e. the line I-I in Fig. 2 where thediffuser 3 begins. - Each of the passages 1C in the
rotor 6 will at any point during the rotation of the rotor eject powder into thespace 25 in an essentially tangential direction so that the initial flow of powder which is entrained frompoint 26 in thedirection 27 of therotor 6 gradually increases in volume. Little velocity is lost by the powder on its way throngh thespace 25. - At the moment when the powder reaches the
diffuser 3 it leaves thespace 25 and, as appears from the drawing, the cross-section of the diffuser is at thai point essentially rectangular (see Fig. 1), whereas at the end of the diffuser (at the level of the flange 30) the cross-section is larger and circular. This transition and'theflange 30 serve to connect the pump as apparatus for the supply of powder. In the diffuser the velocity of the particles decreases and the pressure of the gas entrained with the particles increases. - Fig. 3 is a very diagrammatic representation of a cross-section, comparable with Fig. 2, of a double-acting pump according to the invention.
- The
rotor 31 again comprises a disc which is rotatably mounted on bearings around a shaft in a casing. In addition to walls which run parallel to the disc, the casing comprises two 32 and 33 which are complementary and each surround thewalls rotor 31 for 180°. In this way therotor 31 and thewall 32 enclose aspace 34 which diverges in the direction ofrotation 35 and which at 36 joints with adiffuser 37 and therotor 31 andwall 33 enclose aspace 38 which diverges in the direction ofrotation 35 and which at 39 joints with adiffuser 40. Seen along the circumference of the rotor, thespace 34 begins where thespace 38 ends and vice versa. - The
rotor 31 has acentral powder inlet 41 and two 42 and 43 which in turn eject powder (and gas) into theradial passages 34 and 38, respectively, during rotation of the rotor.space - It will be clear that, provided the two halves of the casing are identical in design, fluctuations in the flow of powder or, for example, deliberate variations in the speed of the rctor will be noticeable in a perfectly identical manner at the outlets of the
37 and 40.diffusers - Finally, Fig. 4 depicts a single-acting pump of which the
rotor 44 has fourradial passages 45 and of which thecasing 46 is provided with a number of gas-supply nozzles 48 which tangentially issue into thespace 47 between casing and rotor. - The gas introduced into the
space 47 through thesenozzles 48 is accelerated in said space under the influence of the powder which is ejected into thespace 47 by therotor 44. The gas may be drawn in by thespace 47 or be injected into it at the required initial velocity. By controlling the quantity of gas and/or the velocity of the gas, influence may be exerted on the pressure and/or the velocity of the gas/powder mixture leaving thediffuser 49. Alternatively, the quantity of gas and/or the velocity of the gas may be adapted to the rotational velocity of therotor 44. - It will be evident that many variations are possible in the shape of the rotor, the shape and number of-the radial passages therein (the rotor may, for example, consist of two discs between which the radial passage comprises a single slot) as well as in the shape and cross-section of the space between the rotor and the casing. The feed and drive of the pump shown may, of course, also be effected in a different manner.
Claims (8)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NL7901452A NL7901452A (en) | 1979-02-23 | 1979-02-23 | CENTRIFUGAL PUMP FOR CARBON POWDER, METHOD AND APPARATUS FOR GASIFICATION OF CARBON POWDER. |
| NL7901452 | 1979-02-23 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0015037A1 true EP0015037A1 (en) | 1980-09-03 |
| EP0015037B1 EP0015037B1 (en) | 1983-10-19 |
Family
ID=19832684
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP80200134A Expired EP0015037B1 (en) | 1979-02-23 | 1980-02-15 | Apparatus for the gasification of coal powder |
Country Status (8)
| Country | Link |
|---|---|
| EP (1) | EP0015037B1 (en) |
| JP (1) | JPS55117093A (en) |
| AU (1) | AU538472B2 (en) |
| CA (1) | CA1150570A (en) |
| DE (1) | DE3065339D1 (en) |
| IN (1) | IN152641B (en) |
| NL (1) | NL7901452A (en) |
| ZA (1) | ZA801001B (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1983002134A1 (en) * | 1981-12-14 | 1983-06-23 | Lockheed Missiles Space | Single stage high pressure centrifugal slurry pump |
| FR2713720A1 (en) * | 1993-12-14 | 1995-06-16 | Unir | Rotor for use in a centrifugal air pump |
| US8061509B2 (en) | 2007-06-13 | 2011-11-22 | Shell Oil Company | Bulk materials pump and its use |
| US8182561B2 (en) | 2008-01-16 | 2012-05-22 | Shell Oil Company | Process to provide a particulate solid material to a pressurised reactor |
| WO2011133321A3 (en) * | 2010-04-19 | 2012-10-26 | General Electric Company | Solid feed guide apparatus for a solid feed pump |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0434491U (en) * | 1990-07-20 | 1992-03-23 |
Citations (12)
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|---|---|---|---|---|
| FR499422A (en) * | 1918-02-14 | 1920-02-11 | John E Greenawalt | Improvements to compressors, fans, blowers, centrifugal pumps and the like |
| FR522769A (en) * | 1920-08-21 | 1921-08-06 | Etienne Joseph Louis Delsol | Further training in centrifugal fans and compressors |
| GB212888A (en) * | 1923-03-15 | 1925-05-25 | Int Comb Eng Corp | Improvements in or relating to pulverisers |
| US2008446A (en) * | 1935-01-09 | 1935-07-16 | Gaskoal Corp | Apparatus for feeding powdered fuel |
| US2341871A (en) * | 1939-07-29 | 1944-02-15 | Oerlikon Maschf | Centrifugal blower with spiral casing |
| US2385508A (en) * | 1943-10-23 | 1945-09-25 | Blaw Knox Co | Combustion of coal |
| CH286975A (en) * | 1951-05-01 | 1952-11-15 | Karrer Josef | Centrifugal fan, in particular fan with spiral housing. |
| US3181471A (en) * | 1961-06-23 | 1965-05-04 | Babcock & Wilcox Co | Centrifugal pump construction |
| FR1402582A (en) * | 1964-07-29 | 1965-06-11 | Blower for transporting materials | |
| DE1428081A1 (en) * | 1964-03-18 | 1968-11-21 | Daimler Benz Ag | Centrifugal blowers, in particular for charging internal combustion engines |
| US3746465A (en) * | 1971-08-11 | 1973-07-17 | Lummus Industries | Centrifugal fan for handling material |
| CH559084A5 (en) * | 1973-11-22 | 1975-02-28 | Fischer Ag Georg |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2707266A1 (en) * | 1977-02-19 | 1978-08-24 | Krupp Koppers Gmbh | METHOD FOR THE GASIFICATION OF FINE-GRAINED TO DUST-SHAPED FUELS |
-
1979
- 1979-02-23 NL NL7901452A patent/NL7901452A/en not_active Application Discontinuation
-
1980
- 1980-01-04 CA CA000343022A patent/CA1150570A/en not_active Expired
- 1980-01-07 IN IN25/CAL/80A patent/IN152641B/en unknown
- 1980-02-15 EP EP80200134A patent/EP0015037B1/en not_active Expired
- 1980-02-15 DE DE8080200134T patent/DE3065339D1/en not_active Expired
- 1980-02-21 ZA ZA00801001A patent/ZA801001B/en unknown
- 1980-02-21 JP JP1979480A patent/JPS55117093A/en active Granted
- 1980-02-21 AU AU55771/80A patent/AU538472B2/en not_active Ceased
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR499422A (en) * | 1918-02-14 | 1920-02-11 | John E Greenawalt | Improvements to compressors, fans, blowers, centrifugal pumps and the like |
| FR522769A (en) * | 1920-08-21 | 1921-08-06 | Etienne Joseph Louis Delsol | Further training in centrifugal fans and compressors |
| GB212888A (en) * | 1923-03-15 | 1925-05-25 | Int Comb Eng Corp | Improvements in or relating to pulverisers |
| US2008446A (en) * | 1935-01-09 | 1935-07-16 | Gaskoal Corp | Apparatus for feeding powdered fuel |
| US2341871A (en) * | 1939-07-29 | 1944-02-15 | Oerlikon Maschf | Centrifugal blower with spiral casing |
| US2385508A (en) * | 1943-10-23 | 1945-09-25 | Blaw Knox Co | Combustion of coal |
| CH286975A (en) * | 1951-05-01 | 1952-11-15 | Karrer Josef | Centrifugal fan, in particular fan with spiral housing. |
| US3181471A (en) * | 1961-06-23 | 1965-05-04 | Babcock & Wilcox Co | Centrifugal pump construction |
| DE1428081A1 (en) * | 1964-03-18 | 1968-11-21 | Daimler Benz Ag | Centrifugal blowers, in particular for charging internal combustion engines |
| FR1402582A (en) * | 1964-07-29 | 1965-06-11 | Blower for transporting materials | |
| US3746465A (en) * | 1971-08-11 | 1973-07-17 | Lummus Industries | Centrifugal fan for handling material |
| CH559084A5 (en) * | 1973-11-22 | 1975-02-28 | Fischer Ag Georg |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1983002134A1 (en) * | 1981-12-14 | 1983-06-23 | Lockheed Missiles Space | Single stage high pressure centrifugal slurry pump |
| FR2713720A1 (en) * | 1993-12-14 | 1995-06-16 | Unir | Rotor for use in a centrifugal air pump |
| US8061509B2 (en) | 2007-06-13 | 2011-11-22 | Shell Oil Company | Bulk materials pump and its use |
| US8182561B2 (en) | 2008-01-16 | 2012-05-22 | Shell Oil Company | Process to provide a particulate solid material to a pressurised reactor |
| US9149779B2 (en) | 2008-01-16 | 2015-10-06 | Shell Oil Company | Process to provide a particulate solid material to a pressurised reactor |
| WO2011133321A3 (en) * | 2010-04-19 | 2012-10-26 | General Electric Company | Solid feed guide apparatus for a solid feed pump |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS55117093A (en) | 1980-09-09 |
| AU538472B2 (en) | 1984-08-16 |
| DE3065339D1 (en) | 1983-11-24 |
| EP0015037B1 (en) | 1983-10-19 |
| IN152641B (en) | 1984-02-25 |
| NL7901452A (en) | 1980-08-26 |
| CA1150570A (en) | 1983-07-26 |
| JPH0116353B2 (en) | 1989-03-23 |
| ZA801001B (en) | 1981-03-25 |
| AU5577180A (en) | 1980-08-28 |
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