EP0722999B1 - Appareil pour refroidir des gaz chauds chargés de solides - Google Patents
Appareil pour refroidir des gaz chauds chargés de solides Download PDFInfo
- Publication number
- EP0722999B1 EP0722999B1 EP96200115A EP96200115A EP0722999B1 EP 0722999 B1 EP0722999 B1 EP 0722999B1 EP 96200115 A EP96200115 A EP 96200115A EP 96200115 A EP96200115 A EP 96200115A EP 0722999 B1 EP0722999 B1 EP 0722999B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- gas
- heat transfer
- inlet
- transfer surfaces
- outlet
- 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.)
- Expired - Lifetime
Links
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Classifications
-
- 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
- C10J3/72—Other features
- C10J3/86—Other features combined with waste-heat boilers
-
- 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
- C10J3/02—Fixed-bed gasification of lump fuel
-
- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10K—PURIFYING OR MODIFYING THE CHEMICAL COMPOSITION OF COMBUSTIBLE GASES CONTAINING CARBON MONOXIDE
- C10K1/00—Purifying combustible gases containing carbon monoxide
- C10K1/04—Purifying combustible gases containing carbon monoxide by cooling to condense non-gaseous materials
-
- 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
- C10J2300/1861—Heat exchange between at least two process streams
- C10J2300/1884—Heat exchange between at least two process streams with one stream being synthesis gas
Definitions
- the present invention to an apparatus for cooling solids laden hot gases.
- a solids laden gas is, for example, synthesis gas obtainable from a coal gasification process.
- the coal gasification process is a well-known process for partial oxidation of finely divided solid carbonaceous fuel wherein an oxygen-containing gas, which is applied as an oxidiser, and a finely divided solid carbonaceous fuel are supplied to a gasification zone wherein substantially autothermically under appropriate conditions of temperature and pressure a gaseous stream containing synthesis gas (which is substantially a gaseous mixture of hydrogen and carbon monoxide) is produced.
- solid impurities such as fly ash particles are usually present in the synthesis gas. Such particles may be sticky.
- the oxygen-containing gas, which is applied as an oxidiser is usually air or (pure) oxygen or steam or a mixture thereof.
- the above partial oxidation reaction usually takes place in a gasification reactor.
- a moderator gas e.g. steam, water or carbon dioxide or a combination thereof
- a moderator gas e.g. steam, water or carbon dioxide or a combination thereof
- the said carbonaceous fuel (optionally with a moderator gas) and the said oxygen-containing gas, applied as oxidiser (optionally with a moderator gas) are supplied to the reactor via at least a burner.
- the hot raw effluent gas stream leaving the reactor, usually at or near its top, is optionally quenched and is usually cooled in an indirect heat exchanger such as a convection cooler.
- the raw gas stream is cooled off by means of convective heat transfer surfaces arranged in a gascooler located next to the gasification reactor and connected through a duct to the said reactor.
- the gases are solids laden and therefore problems may arise with respect to erosion of the heat transfer surfaces (when the gas velocity is too high) or with respect to fouling/blocking the gas passages between the heat transfer surfaces (when the gas velocity is too low).
- the gas velocity will decrease when operating at a constant throughput and pressure, to such an extent that fouling/blocking of the equipment may occur (e.g. by sticky particles) and expensive rapping devices are required to avoid fouling/blocking.
- the invention therefore provides a self-cleaning apparatus for cooling a solids laden hot gas, said apparatus comprising a vessel with a gas inlet and a gas outlet and heat transfer structure comprising a plurality of heat transfer surfaces extending in the vessel between said inlet and said outlet in a longitudinal direction and forming a plurality of gas passages in the said structure, wherein the said plurality of heat transfer surfaces is arranged in such a way that the overall cross-sectional inlet area of the said gas passages in the said structure is larger than the overall cross-sectional outlet area between said gas passages and that the said gas passages are arranged in such a manner that, in operation, the velocity of the gas flowing through the said gas passages, is kept substantially constant between the cross-sectional inlet area of the said gas passages and the cross-sectional outlet area of the said gas passages.
- a vessel 1, made of any material suitable for the purpose, is shown.
- the vessel 1 has a vessel wall 1a and is provided at its upstream side with an inlet 2 for solids laden gas A from a reactor (not shown for reasons of clarity) and at its downstream side with an outlet 3 for cooled gas B which is supplied in any suitable manner to any suitable further gas treating and processing equipment (not shown for reasons of clarity).
- the inlet 2 is located at or near the top of vessel 1 and the outlet 3 is located at or near the bottom of vessel 1.
- the gascooler is substantially cylindrical and arranged substantially vertically, but it will be appreciated by those skilled in the art that any arrangement suitable for the purpose can be applied.
- the cooler 1 is internally provided in any suitable manner with a heat transfer structure comprising a plurality of panels 4 of (convective) heat transfer surfaces arranged in such a manner, that a plurality of gas passages 13 from said inlet to said outlet extending in downstream direction is provided (i.e. in the direction of decreasing process temperature).
- the arrangement of the heat transfer surfaces is such that the overall cross-sectional inlet area of the gas passages 13 is larger than the overall cross-sectional outlet area of the gas passages 13.
- the height of the heat transfer structure is M, whereas the distances between the outer heat transfer surfaces of said structure are W1 (inlet) and W2 (outlet) respectively.
- each panel 4 of heat transfer surfaces arranged in the gas cooler comprises a plurality of cooling tubes (not shown in fig. 1 for reasons of clarity) in mutual mechanical connection by any suitable means such as a webbing, through which tubes any suitable cooling fluid flows (e.g. water or steam, advantageously in counter current flow with the gas) and these panels are designed such that the cross-sectional areas of the passages between the heat transfer surfaces are in tapering arrangement aiming at keeping the gas velocity substantially constant, advantageously in the velocity region of 6-12 m/s.
- the tubes are provided with fins.
- the overall cross-sectional area decrease of the gas passages between the said heat transfer surfaces is such that the gas flow A is smoothly directed to the said surfaces and the gas flow impingement represented by the arrow C on the heat transfer surfaces is at small angles ⁇ such that the gas flow substantially parallel to the said surfaces from erosion point of view.
- An advantageous impact angle ⁇ of the gas flow is 2.5 degrees.
- the gascooler is provided at its one end with a plurality of inlet headers feeding the panels of cooling tubes with any suitable cooling medium.
- the gascooler is provided at its other end with a plurality of outlet headers.
- outlet headers For reasons of clarity the inlet headers, outlet headers and the mechanical connections of the tubes with said headers have not been shown in fig. 1.
- Each end of a cooling tube of a panel is connected to an outlet header 6 and inlet header 5 respectively as will be explained in more detail below referring to figs. 2a and 2b.
- the arrangement of the panels and tubes is such that a so-called membrane pipe wall is formed, the (ring-shaped) inlet of which and the (ring-shaped) outlet of which have been represented schematically in fig. 1 by reference numerals 8 and 9 respectively.
- the membrane pipe wall forms within the vessel 1a a "cage" surrounding the said panels and will be shown in more detail below by reference to figs. 3a and 3b.
- Fig. 2a represents a partial side view of the inlet header arrangement applied in the gascooler of the invention as shown in fig. 1. For reasons of clarity only 7 tubes have been shown.
- the inlet header 5 is in any suitable manner connected to each cooling tube 10 of a panel 4.
- Reference numeral 1a represents the vessel wall.
- the tubes 10 of the panel 4 are mechanically connected via webbings 10a (e.g. by welding).
- end or outer tube 10' of a panel 4 is part of the "cage" formed by the membrane pipe wall and is in fluid-connection to the inlet 8 (Fig. 1).
- the membrane pipe wall tube is not connected to the inlet header 5. It will be appreciated that where appropriate the tubes of the membrane pipe wall are suitably bent to provide space for the connecting tubes between the panel 4 and the inlet header 5.
- Fig. 2b represents a partial side view of a similar arrangement for an outlet header 6 applied in the gascooler of the invention as shown in fig. 1. For reasons of clarity only 7 tubes have been shown. The same reference numerals as in fig. 2a have been used and where appropriate the tubes of the membrane pipe wall are suitably bent. The end or outer tube 10' is part of the "cage" and is in fluid-connection to the outlet 9 (fig. 1).
- Fig. 3a represents a cross-sectional view of the arrangement of heat transfer surfaces along the line I-I of fig. 1.
- thirteen panels 4 have been shown, each panel 4 comprising a plurality of cooling tubes 10 and end or outer tubes 10'.
- the tubes 10 of each panel are connected via webbings 10a.
- the end or outer tubes 10' of each panel 4 are connected to the end or outer tubes 10' of the adjacent panel 4 via tubes 7.
- the outer tubes 7 and 10' form the "cage" 11.
- the tubes 7 (except two which are arranged in a symmetry-plane of the arrangement) are diminishing in diameter from top to bottom so that a tapering arrangement and a sloping position of the panels 4 at both sides of a symmetry-plane are obtained. For reasons of clarity, only a limited number of tubes 10 of each panel 4 is represented.
- Reference numeral 13 represents the gas passages between the heat transfer surfaces.
- the panel distance C 1 at the inlet side of the panels is larger than the panel distance at the outlet side (C 2 ) due to the arrangement of tapering tubes 7 arranged between the outer tubes 10' of each panel 4.
- the cage overall dimensions are V x W1 (inlet) and V x W2 (outlet) wherein W1 > W2 and V remaining constant.
- Fig. 3b represents a top view of the outlet header arrangement of fig. 1.
- the same reference numerals have been used as in previous figures.
- Fig. 4 represents an advantageous embodiment (partially represented) of a tapering tube 7 of the "cage", arranged between the outer tubes 10' of each panel 4 (vide figs. 3a and 3b).
- Z represents a tapered webbing.
- the diameter of the tube 7 decreases gradually from inlet end to outlet end with a suitable tapering angle ⁇ (e.g. 2.5°) for the plurality of tapered parts of the said tube.
- ⁇ e.g. 2.5°
- the diameter of the tube is gradually decreasing in downflow direction from 60 to 30 mm and the length M is 25-35 m.
- headers suitable for the purpose can be applied.
- E.g. two headers per panel of tubes can be used.
- the webbings between the tubes are provided with openings. More advantageously, the webbings are 25-90% open.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Claims (13)
- Appareil autonettoyant pour refroidir un gaz chaud chargé en solides, ledit appareil comportant une cuve (1) dotée d'un orifice d'entrée de gaz (2) et d'un orifice de sortie de gaz (3) et d'une structure (7, 10') de transfert de chaleur comportant plusieurs surfaces (4) de transfert de chaleur s'étendant dans la cuve (1) entre ledit orifice d'entrée (2) et ledit orifice de sortie (3) dans le sens de sa longueur et formant une pluralité de passages de gaz (13) dans ladite structure, ladite pluralité de surfaces de transfert de chaleur étant agencée de telle sorte que la superficie totale de la section transversale d'entrée desdits passages de gaz (13) de ladite structure est plus grande que la superficie totale de la section transversale de sortie entre lesdits passages de gaz (13), et en ce que lesdits passages de gaz sont agencés de telle sorte qu'en fonctionnement, la vitesse des gaz s'écoulant dans lesdits passages de gaz est maintenue essentiellement constante entre la superficie de la section transversale d'entrée et la superficie de la section transversale de sortie desdits passages de gaz.
- Appareil selon la revendication 1, dans lequel la cuve (1) est de forme essentiellement cylindrique.
- Appareil selon la revendication 1 ou 2, dans lequel la cuve (1) est agencée essentiellement à la verticale.
- Appareil selon l'une quelconque des revendications 1 à 3, dans lequel l'orifice d'entrée des gaz (2) est situé au sommet de la cuve (1) ou à proximité de ce dernier et l'orifice de sortie des gaz (3) est situé à la base de la cuve (1) ou à proximité de celle-ci.
- Appareil selon l'une quelconque des revendications 1 à 4, dans lequel la structure de transfert de chaleur (7, 10') est une paroi de tubes en membrane ou "cage".
- Appareil selon l'une quelconque des revendications 1 à 5, dans lequel lesdites surfaces (4) de transfert de chaleur sont des surfaces de transfert de chaleur par convection.
- Appareil selon l'une quelconque des revendications 1 à 6, dans lequel chaque surface de transfert de chaleur (4) comporte des panneaux de tubes de refroidissement (10), et en fonctionnement un fluide de refroidissement s'écoule dans lesdits tubes.
- Appareil selon la revendication 6 ou 7, dans lequel le fluide de refroidissement s'écoule à contre-courant par rapport au gaz.
- Appareil selon l'une quelconque des revendications 6 à 8, dans lequel le fluide de refroidissement est de l'eau ou de la vapeur.
- Appareil selon l'une quelconque des revendications 1 à 9, dans lequel la superficie totale de la section transversale de l'orifice d'entrée des passages de gaz (13) entre les surfaces de transfert de chaleur (4) diminue progressivement dans la direction aval en formant ainsi un agencement en rétrécissement des surfaces de transfert de chaleur.
- Appareil selon l'une quelconque des revendications 1 à 10, dans lequel la vitesse du gaz est comprise dans la plage de 6 à 12 m/s.
- Appareil selon la revendication 10 ou 11, dans lequel lesdites surfaces (4) de transfert de chaleur sont agencées suivant un angle α, avec α = tan [1/2(W1-W2)/M]; M étant la hauteur de la structure de transfert de chaleur; et W1 et W2 représentent respectivement les distances entre les surfaces extérieures de transfert de chaleur de ladite structure, son entrée et sa sortie.
- Appareil selon la revendication 12, dans lequel a n'est pas supérieur à 2,5°.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP96200115A EP0722999B1 (fr) | 1995-01-20 | 1996-01-18 | Appareil pour refroidir des gaz chauds chargés de solides |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP95200145 | 1995-01-20 | ||
EP95200145 | 1995-01-20 | ||
EP96200115A EP0722999B1 (fr) | 1995-01-20 | 1996-01-18 | Appareil pour refroidir des gaz chauds chargés de solides |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0722999A1 EP0722999A1 (fr) | 1996-07-24 |
EP0722999B1 true EP0722999B1 (fr) | 1999-12-29 |
Family
ID=8219967
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP96200115A Expired - Lifetime EP0722999B1 (fr) | 1995-01-20 | 1996-01-18 | Appareil pour refroidir des gaz chauds chargés de solides |
Country Status (8)
Country | Link |
---|---|
EP (1) | EP0722999B1 (fr) |
JP (1) | JP3986101B2 (fr) |
KR (1) | KR100390380B1 (fr) |
CN (1) | CN1104625C (fr) |
CA (1) | CA2167564C (fr) |
DE (1) | DE69605825T2 (fr) |
ES (1) | ES2142011T3 (fr) |
ZA (1) | ZA96390B (fr) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2290446C2 (ru) * | 2001-08-10 | 2006-12-27 | Шелл Интернэшнл Рисерч Маатсхаппий Б.В. | Способ рекуперации энергии из горячего газа |
MY136087A (en) | 2001-10-22 | 2008-08-29 | Shell Int Research | Process to reduce the temperature of a hydrogen and carbon monoxide containing gas and heat exchanger for use in said process |
JP4599291B2 (ja) * | 2005-01-07 | 2010-12-15 | 三菱重工業株式会社 | 加圧高温ガス冷却器 |
US7803216B2 (en) | 2005-12-28 | 2010-09-28 | Mitsubishi Heavy Industries, Ltd. | Pressurized high-temperature gas cooler |
CN102333850A (zh) | 2008-12-30 | 2012-01-25 | 国际壳牌研究有限公司 | 供给合成气的方法和系统 |
JP2012514039A (ja) | 2008-12-31 | 2012-06-21 | シエル・インターナシヨナル・リサーチ・マートスハツペイ・ベー・ヴエー | メタンリッチガスの生成方法 |
EP2370203A2 (fr) | 2008-12-31 | 2011-10-05 | Shell Oil Company | Réacteur adiabatique et procédé et système pour produire un gaz enrichi en méthane dans un tel réacteur adiabatique |
PL2462088T3 (pl) | 2009-08-03 | 2017-01-31 | Shell Internationale Research Maatschappij B.V. | Sposób wytwarzania metanu |
CN102482174B (zh) | 2009-08-03 | 2014-09-10 | 国际壳牌研究有限公司 | 联产过热蒸汽和甲烷的方法 |
CN109562939B (zh) * | 2016-07-21 | 2022-12-06 | 托普索公司 | 用于生产三氧化硫的方法 |
KR102316717B1 (ko) * | 2021-02-25 | 2021-10-27 | 성일하이메탈(주) | 열교환을 이용한 유해 가스 무해화 처리 장치 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4520760A (en) * | 1984-04-23 | 1985-06-04 | Combustion Engineering, Inc. | Heat exchanger outlet arrangement |
DE3929766A1 (de) * | 1989-09-07 | 1991-03-14 | Krupp Koppers Gmbh | Anlage fuer die erzeugung eines produktgases aus einem feinteiligen kohlenstofftraeger |
DK163896C (da) * | 1990-01-05 | 1992-10-26 | Burmeister & Wains Energi | Gaskoeler for varmeovergang ved konvektion |
-
1996
- 1996-01-17 CN CN96100444A patent/CN1104625C/zh not_active Expired - Lifetime
- 1996-01-18 EP EP96200115A patent/EP0722999B1/fr not_active Expired - Lifetime
- 1996-01-18 CA CA002167564A patent/CA2167564C/fr not_active Expired - Fee Related
- 1996-01-18 DE DE69605825T patent/DE69605825T2/de not_active Expired - Lifetime
- 1996-01-18 ES ES96200115T patent/ES2142011T3/es not_active Expired - Lifetime
- 1996-01-18 ZA ZA96390A patent/ZA96390B/xx unknown
- 1996-01-18 JP JP02338296A patent/JP3986101B2/ja not_active Expired - Fee Related
- 1996-01-19 KR KR1019960001087A patent/KR100390380B1/ko not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
CN1153286A (zh) | 1997-07-02 |
KR100390380B1 (ko) | 2003-09-06 |
CA2167564C (fr) | 2007-05-15 |
ES2142011T3 (es) | 2000-04-01 |
DE69605825T2 (de) | 2001-07-19 |
DE69605825D1 (de) | 2000-02-03 |
CA2167564A1 (fr) | 1996-07-21 |
ZA96390B (en) | 1996-08-15 |
EP0722999A1 (fr) | 1996-07-24 |
CN1104625C (zh) | 2003-04-02 |
JPH08231966A (ja) | 1996-09-10 |
JP3986101B2 (ja) | 2007-10-03 |
KR960028962A (ko) | 1996-08-17 |
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