Furnace wall, gasification unit and integrated gasification combined cycle, and method of manufacturing furnace wall
10954853 ยท 2021-03-23
Assignee
Inventors
Cpc classification
F22B1/1846
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23G2202/101
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C10J2300/1653
CHEMISTRY; METALLURGY
F02C6/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C3/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E20/18
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
F22B21/34
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N3/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23M5/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E20/16
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
F01K23/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K23/068
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F22B31/003
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F22B1/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F22B37/125
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K23/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F22B37/104
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C10J2300/165
CHEMISTRY; METALLURGY
F22B37/102
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02C3/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23M5/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F22B37/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C6/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K23/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F22B1/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K23/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F22B21/34
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K23/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F22B31/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F22B37/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F22B1/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F22B37/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N3/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The purpose of the present invention is to provide a furnace wall in which a throat section with a smaller channel diameter than other regions can be formed using all peripheral wall tubes. Provided is a furnace wall comprising: a plurality of peripheral wall tubes (142), which are disposed so as to form a cylindrical shape when aligned in one direction and through the interior of which cooling water flows; and fins (140) that connect neighboring peripheral wall tubes (142) in an airtight manner. In a throat section in which the diameter of a horizontal cross-section of the cylindrical shape is reduced in comparison to other regions, the peripheral wall tubes (142) are disposed so as to be in mutual contact and the fins (140) are disposed on the inner circumferential sides of the cylindrical shapes.
Claims
1. A furnace wall comprising: a plurality of tubes arrayed in a predetermined direction and defining a cylindrical construction, a coolant flowing inside the tubes; and a plurality of connections hermetically sealing spaces between the adjacent tubes, wherein the tubes are disposed in contact with each other at contact areas in a throat section of the cylindrical construction having a horizontal cross-section having a diameter smaller than the diameter of the cross-section of other portions of the cylindrical construction, and some of the connections comprise inner-circumferential-side connections disposed closer to the inner circumferential side of the cylindrical construction than contact areas, some of the connections in the throat section comprise outer-circumferential-side connections disposed closer to the outer circumferential side of the cylindrical construction than the contact areas, the outer-circumferential-side connections comprise rod-like members extending in the longitudinal direction of the tubes, the inner-circumferential-side connections comprise rod-like members extending in the longitudinal direction of the tubes, the rod-like members of the outer-circumferential-side connections are connected with the respective rod-like members of the inner-circumferential-side connections, the outer-circumferential-side connections and the inner-circumferential-side connections having end portions being folded back, and the rod-like members of the outer-circumferential-side connections each have at least one cut.
2. A furnace wall comprising: a plurality of tubes arrayed in a predetermined direction and defining a cylindrical construction, a coolant flowing inside the tubes; and a plurality of connections hermetically sealing spaces between the adjacent tubes, wherein the tubes are disposed in contact with each other at contact areas in a throat section of the cylindrical construction having a horizontal cross-section having a diameter smaller than the diameter of the cross-section of other portions of the cylindrical construction, and some of the connections comprise inner-circumferential-side connections disposed closer to the inner circumferential side of the cylindrical construction than contact areas, and the contact areas of at least some of the tubes have flat portions formed by cutting outer faces of the tubes.
3. The furnace wall according to claim 1, wherein the centers of the tubes are disposed on a horizontal cross-section of the cylindrical construction at same radial distances from the center of the cylindrical construction in the throat section.
4. A furnace wall comprising: a plurality of tubes arrayed in a predetermined direction and defining a cylindrical construction, a coolant flowing inside the tubes; and a plurality of connections hermetically sealing spaces between the adjacent tubes, wherein the tubes are disposed in contact with each other at contact areas in a throat section of the cylindrical construction having a horizontal cross-section having a diameter smaller than the diameter of the cross-section of other portions of the cylindrical construction, and some of the connections comprise inner-circumferential-side connections disposed closer to the inner circumferential side of the cylindrical construction than contact areas, and the centers of the tubes are disposed on a horizontal cross-section of the cylindrical construction at different radial distances from the center of the cylindrical construction in the throat section.
5. A gasification unit configured to generate raw syngas by combusting and gasifying carbonaceous feedstock, the gasification unit comprising: the furnace wall according to claim 1, wherein the raw syngas passes through the interior of the cylindrical construction.
6. An integrated gasification combined cycle comprising: the gasification unit according to claim 5 configured to generate raw syngas by combusting and gasifying carbonaceous feedstock; a gas turbine unit configured to be rotationally driven by combusting at least a portion of the raw syngas generated at the gasification unit; a steam turbine unit configured to be rotationally driven by steam including steam generated at a heat recovery stream generator introducing turbine flue gas discharged from the gas turbine unit; and a generator linked to the gas turbine unit and the steam turbine unit.
7. A method of manufacturing a furnace wall comprising: arraying a plurality of tubes in a predetermined direction and defining a cylindrical construction, a coolant flowing inside the tubes; and disposing a plurality of connections hermetically sealing spaces between the adjacent tubes, wherein the tubes are disposed in contact with each other at contact areas in a throat section of the cylindrical construction having a horizontal cross-section having a diameter smaller than the diameter of the cross-section of other portions of the cylindrical construction, and the connections are disposed closer to the inner circumferential side of the cylindrical construction than contact areas, some of the connections in the throat section comprise outer-circumferential-side connections disposed closer to the outer circumferential side of the cylindrical construction than the contact areas, the outer-circumferential-side connections comprise rod-like members extending in the longitudinal direction of the tubes, the inner-circumferential-side connections comprise rod-like members extending in the longitudinal direction of the tubes, the rod-like members of the outer-circumferential-side connections are connected with the respective rod-like members of the inner-circumferential-side connections, the outer-circumferential-side connections and the inner-circumferential-side connections having end portions being folded back, and the rod-like members of the outer-circumferential-side connections each have at least one cut.
Description
BRIEF DESCRIPTION OF DRAWINGS
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DESCRIPTION OF EMBODIMENTS
(14) Embodiments of the present invention will now be described with reference to the drawings.
First Embodiment
(15) A first embodiment of the present invention will now be described.
(16) An integrated gasification combined cycle (IGCC) 10 including a gasification unit 14 uses air as an oxygen containing gas and is of an air-combustion type in which raw syngas is generated from fuel in the gasification unit 14. In the integrated gasification combined cycle 10, the raw syngas generated at the gasification unit 14 is purified at a gas purification unit 16 into fuel gas, and the fuel gas is fed to a gas turbine unit 17 to generate electrical power. In specific, the integrated gasification combined cycle 10 according to this embodiment is an air-combustion (air-blown) type power plant. The fuel fed to the gasification unit 14 is pulverized coal prepared by pulverizing carbonaceous feedstock, such as coal, with a coal mill.
(17) With reference to
(18) The coal feeder 11 receives coal or raw coal and pulverizes the received coal with a coal mill (not shown), to produce minute particles of pulverized coal. The pulverized coal produced at the coal feeder 11 is fed to the gasification unit 14 together with nitrogen gas serving as a conveyor inert gas from an air separation unit 42 described below.
(19) The gasification unit 14 receives the pulverized coal produced at the coal feeder 11 and the char (unreacted coal and ash) collected by the char recovery unit 15 for reuse. An inert gas has an oxygen content of approximately 5 volume percent or less. Typical examples of inert gas include nitrogen gas, carbon dioxide gas, and argon gas and may have any volume percent besides approximately 5% or less.
(20) The gasification unit 14 is connected to a compressed-air feeding line 41 leading from the gas turbine unit 17 (compressor 61). Thus, a portion of the air compressed at the gas turbine unit 17 can be fed to the gasification unit 14 after the pressure of the compressed air is increased to a predetermined pressure at a booster 68. The air separation unit 42 separates nitrogen and oxygen from the air in the atmosphere. The air separation unit 42 is connected to the gasification unit 14 through a first nitrogen feeding line 43. The first nitrogen feeding line 43 is connected to a coal feeding line 11a leading from the coal feeder 11. A second nitrogen feeding line 45 branching from the first nitrogen feeding line 43 is also connected to the gasification unit 14. The second nitrogen feeding line 45 is connected to a char returning line 46 leading from the char recovery unit 15. The air separation unit 42 is connected to the compressed-air feeding line 41 through an oxygen feeding line 47. The nitrogen separated at the air separation unit 42 serves as a gas for conveying coal and char by flowing through the first nitrogen feeding line 43 and the second nitrogen feeding line 45. The oxygen separated at the air separation unit 42 serves as an oxygen containing gas at the gasification unit 14 by flowing through a first oxygen feeding line 47 and the compressed-air feeding line 41.
(21) The gasification unit 14 includes, for example, an air-blown two-stage entrained bed gasifier 101 (see
(22) The char recovery unit 15 includes a precipitator 51 and a feed hopper 52. In such a case, the precipitator 51 includes one or more porous filters and cyclones and can separate the char from the raw syngas generated in the gasification unit 14. The raw syngas separated from the char is sent to the gas purification unit 16 through a gas discharge line 53. The feed hopper 52 collects the char separated from the raw syngas at the precipitator 51. A bin may be disposed between the precipitator 51 and the feed hopper 52, and multiple feed hoppers 52 may be connected to this bin. The char returning line 46 leading from the feed hopper 52 is connected to the second nitrogen feeding line 45.
(23) The gas purification unit 16 purifies the gas by removing impurities, such as sulfur compounds and nitrogen compounds, from the raw syngas separated from the char at the char recovery unit 15. The gas purification unit 16 purifies the raw syngas to produce fuel gas and feeds the fuel gas to the gas turbine unit 17. The raw syngas separated from the char still has a sulfur content (such as H2S). Thus, the gas purification unit 16 removes and collects the sulfur content with an amine absorbent, for efficient use.
(24) The gas turbine unit 17 includes a compressor 61, a combustor 62, and a turbine 63. The compressor 61 and the turbine 63 are linked by a rotary shaft 64. The combustor 62 is connected to the compressed-air feed line 65 leading from the compressor 61, a fuel-gas feeding line 66 leading from the gas purification unit 16, and a combustible-gas feeding line 67 leading to the turbine 63. The compressor 61 of the gas turbine unit 17 is connected to the compress-air feeding line 41 leading from the compressor 61 to the gasification unit 14. The booster 68 is disposed at an intermediate position on the compressed-air feeding line 41. Thus, the combustor 62 produces combustion gas by mixing the compressed air fed from the compressor 61 with at least a portion of the fuel gas fed from the gas purification unit 16 and combusting the mixture, and feeds the resulting combustion gas to the turbine 63. The turbine 63 rotationally drives the rotary shaft 64 with the fed combustion gas, to rotationally drive the generator 19.
(25) The steam turbine unit 18 includes a turbine 69 linked to the rotary shaft 64 of the gas turbine unit 17. The generator 19 is linked to the proximal end of the rotary shaft 64. The heat recovery stream generator 20 is connected to an flue gas line 70 leading from the gas turbine unit 17 (turbine 63), to exchange heat between the water and the exhaust gas for steam generation. The heat recovery stream generator 20 includes a steam feeding line 71 and a steam recovery line 72, each connected to both the steam turbine unit 18 and the turbine 69. The steam recovery line 72 is connected to a condenser 73. The steam generated at the heat recovery stream generator 20 may include steam generated by heat exchange with the raw syngas at the syngas cooler 102 of the gasifier 101 and further subjected to heat exchange at the heat recovery stream generator 20. Thus, the steam turbine unit 18 rotationally drives the turbine 69 with the steam fed from the heat recovery stream generator 20, thereby rotates the rotary shaft 64 to rotationally drive the generator 19.
(26) A gas emission filter 74 is disposed between the outlet of the heat recovery stream generator 20 and the chimney 75.
(27) The operation of the above-described Integrated gasification combined cycle 10 will now be described.
(28) In the Integrated gasification combined cycle 10 according to this embodiment, the raw coal (coal) fed to the coal feeder 11 is ground into fine particles at the coal feeder 11 to produce pulverized coal. The pulverized coal produced in the coal feeder 11 is fed to the gasification unit 14 together with nitrogen fed from the air separation unit 42 through the first nitrogen feeding line 43. The char collected by the char recovery unit 15 described below is fed to the gasification unit 14 together with nitrogen fed from the air separation unit 42 through the second nitrogen feeding line 45. The compressed air extracted by the gas turbine unit 17 described below is boosted to a higher pressure at the booster 68 and fed to the gasification unit 14 through the compressed-air feeding line 41 together with the oxygen from the air separation unit 42.
(29) At the gasification unit 14, the pulverized coal and the char are combusted by the compressed air (oxygen) and gasified to generate raw syngas. The raw syngas is discharged from the gasification unit 14 through the gas production line 49 and sent to the char recovery unit 15.
(30) At the char recovery unit 15, the raw syngas is fed to the precipitator 51 to separate the micronized char in the raw syngas. The raw syngas separated from the char is sent to the gas purification unit 16 through a gas discharge line 53. In contrast, the micronized char separated from the raw syngas is accumulated in the feed hopper 52 and returned to the gasification unit 14 through the char returning line 46, for recycling.
(31) The gas purification unit 16 purifies the gas by removing impurities, such as sulfur compounds and nitrogen compounds, from the raw syngas separated from the char at the char recovery unit 15, to produce fuel gas. The compressor 61 generates compressed air and feeds the compressed air to the combustor 62. The combustor 62 generates combustion gas by mixing the compressed air fed from the compressor 61 with the fuel gas fed from the gas purification unit 16 and combusting the mixture. Electrical power can be generated by rotationally driving the turbine 63 with the combustion gas and thereby rotationally driving the generator 19 via the rotary shaft 64. In this way, the gas turbine unit 17 can generate electrical power.
(32) The heat recovery stream generator 20 then generates steam by exchanging heat between the flue gas discharged from the turbine 63 of the gas turbine unit 17 and the water and feeds the generated steam to the steam turbine unit 18. Electrical power can be generated at the steam turbine unit 18 by driving the turbine 69 with the steam fed from the heat recovery stream generator 20 and thereby rotationally driving the generator 19 via the rotary shaft 64. Besides the gas turbine unit 17 and the steam turbine unit 18 rotationally driving a single generator 19 via a single axis, the gas turbine unit 17 and the steam turbine unit 18 may rotationally drive multiple generators 19 via multiple axes.
(33) The gas emission filter 74 removes harmful substances in the exhaust gas discharged from the heat recovery stream generator 20 and releases the filtered gas from the chimney 75 to the atmosphere.
(34) The gasification unit 14 of the above-described Integrated gasification combined cycle 10 will now be described in detail with reference to
(35) The gasification unit 14 includes a gasifier 101 and a syngas cooler 102, as illustrated in
(36) The gasifier 101 extends in the vertical direction. Pulverized coal and oxygen are fed to the lower portion in the vertical direction and partially combusted and gasified into raw syngas. The generated raw syngas flows from the lower portion to the upper portion in the vertical direction. The gasifier 101 includes a pressure vessel 110 and a gasifier wall (furnace wall) 111 disposed in the interior of the pressure vessel 110. The gasifier 101 has an annular portion 115 disposed in the space between the pressure vessel 110 and the gasifier wall 111. The gasifier 101 includes a combustor 116, a diffuser 117, and a reductor 118 in the interior space of the gasifier wall 111 in order from the lower portion in vertical direction (i.e., from the upstream of the flow direction of the raw syngas).
(37) The pressure vessel 110 has a hollow cylindrical shape. A gas exhaust port 121 is disposed at the upper end portion of the pressure vessel 110, and a slag hopper 122 is disposed at the lower end portion (bottom portion) of the pressure vessel 110. The gasifier wall 111 has a hollow cylindrical shape. The wall face of the gasifier wall 111 faces the inner face of the pressure vessel 110. The pressure vessel 110 according to this embodiment has a cylindrical shape, and the diffuser 117 of the gasifier wall 111 also has a cylindrical shape. The gasifier wall 111 is connected to the inner face of the pressure vessel 110 with a supporting member (not shown).
(38) The gasifier wall 111 partitions the interior of the pressure vessel 110 into an inner space 154 and an external space 156. The gasifier wall 111 has a horizontal cross-section varying in shape at the diffuser 117 between the combustor 116 and the reductor 118, as described below. The upper end portion of the gasifier wall 111 in the vertical direction is connected to the gas exhaust port 121 of the pressure vessel 110, and the lower end portion in the vertical direction is disposed apart from the bottom portion of the pressure vessel 110 with a gap provided therebetween. The slag hopper 122 disposed at the bottom portion of the pressure vessel 110 stores water. The lower end portion of the gasifier wall 111 is immersed in the stored water to provide a seal between the interior and exterior of the gasifier wall 111. Burners 126 and 127 are disposed in the gasifier wall 111, and the syngas cooler 102 is disposed in the inner space 154. The structure of the gasifier wall 111 will be described below.
(39) The annular portion 115 is a space disposed in the interior of the pressure vessel 110 and the exterior of the gasifier wall 111, i.e., the external space 156. The nitrogen, which is an inert gas, separated at the air separation unit 42 is fed to the annular portion 115 through a nitrogen feed line (not shown). Thus, the annular portion 115 is a space filled with nitrogen. A furnace pressure equalizer (not shown) that equalizes the internal pressure of the gasifier 101 is disposed near the upper position of the annular portion 115 in the vertical direction. The furnace pressure equalizer is in communication with the interior and exterior of the gasifier wall 111, to substantially equalize the pressure of the internal components (the combustor 116, the diffuser 117, and the reductor 118) of the gasifier wall 111 and the pressure of the external components (the annular portion 115) such that the difference in pressure is within a predetermined value.
(40) The combustor 116 provides a space for partially combusting the pulverized coal, the char, and the air. A combusting device including multiple burners 126 is disposed on the gasifier wall 111 at the combustor 116. The high temperature combustion gas generated by partially combusting the pulverized coal and the char at the combustor 116 flows through the diffuser 117 to the reductor 118.
(41) The reductor 118 provides a space for raw syngas generation through gasification. In this space, which is maintained at a temperature sufficiently high for the gasification process, pulverized coal is supplied to the combustion gas fed from the combustor 116 and partially combusted to reduce the pulverized coal to volatiles (such as carbon monoxide, hydrogen, and low hydrocarbons). A combusting device including multiple burners 127 is disposed in the gasifier wall 111 at the reductor 118.
(42) The syngas cooler 102 is disposed in the interior of the gasifier wall 111 and above the burners 127 of the reductor 118 in the vertical direction. The syngas coolers 102 are heat exchangers and includes an evaporator 131, a superheater 132, and an economizer 134 is order from the lower portion of the gasifier wall 111 in the vertical direction (from the upstream of the flow direction of the raw syngas). The syngas coolers 102 exchange heat with the raw syngas generated at the reductor 118, to cool the syngas. The evaporator 131, the superheater 132, and the economizer 134 may be provided by any number beside that illustrated in the drawing.
(43) The operation of the gasification unit 14 described above will now be described.
(44) In the gasifier 101 of the gasification unit 14, the nitrogen and the pulverized coal are ignited by the burners 127 of the reductor 118, and the pulverized coal, the char, and the compressed air (oxygen) are ignited by the burners 126 of the combustor 116. The combustion of the pulverized coal and the char generates high-temperature combustion gas at the combustor 116. At the combustor 116, melted slag is generated in the high-temperature gas atmosphere through combustion of the pulverized coal and the char. The melted slag attaches to the gasifier wall 111, falls to the bottom of the gasifier, and is finally discharged to the water stored in the slag hopper 122. The high-temperature combustion gas generated at the combustor 116 flows through the diffuser 117 up to the reductor 118. In the reductor 118 maintained at a high temperature required for the gasification reaction, the pulverized coal is mixed with the high-temperature combustion gas and subjected to gasification through partial combustion under a high-temperature reducing atmosphere, to generate raw syngas. The gasified raw syngas flows from the bottom to top in the vertical direction.
(45) The gasifier wall 111 will now be described in detail.
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(47) The diffuser 117 of the gasifier wall 111, which has a cylindrical horizontal cross-section, includes multiple peripheral wall tubes 142 and fins (connections) 140 disposed between adjacent peripheral wall tubes 142.
(48) The gasification unit 14 includes a cooling-water circulating mechanism 143 that circulates a coolant (water or stream serving as cooling water) to the peripheral wall tubes 142, as illustrated in
(49) Alternatively, the circulation channel 144 may include the cooler 146. The cooler 146 cools the cooling water having an increased temperature after passing through the peripheral wall tubes 142, through heat exchange. The cooler 146 may be, for example, a steam generator. Water from the outside is fed through a water feed pipe (not shown) to the inlet header 150 by the pump 148 and to the economizer 134. A steam drum (not shown) is connected to the outlet header 152. The steam drum is also connected to the heat-exchanger tube of the evaporator 131, the heat-exchanger tube of the superheater 132, and the heat-exchanger tube of the economizer 134 through tubes (not shown). The steam drum exchanges heat with the raw syngas generated at the reductor 118 to generate steam from the fed water. The generated steam is fed to the steam turbine unit 18 through a steam exhaust pipe (not shown) together with the steam generated at the heat recovery stream generator 20. The raw syngas is cooled through heat exchange and is discharged from the gas exhaust port 121 at the upper end of the pressure vessel 110.
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(53) Fins 140 are disposed between adjacent peripheral wall tubes 142 to serve as connections hermetically sealing the spaces between adjacent peripheral wall tubes 142. The fins 140 are disposed on a line connecting the centers of the peripheral wall tubes 142. The fins 140 each include a sealing rod (rod-like member) 140a and welded portions 140b overlaid to fill a space between the adjacent peripheral wall tubes 142 around the sealing rod 140a. The sealing rod 140a and the welded portions 140b are composed of a nickel base alloy or a nickel-containing alloy having high corrosion resistance. Examples of a nickel base alloy include Inconel (registered trademark) 600, Inconel (registered trademark) 622, Inconel (registered trademark) 625, Inconel (registered trademark) 690, HR-160, HASTELLOY X (registered trademark), Alloy 72, and Alloy 72M.
(54) The annular cross-sections of the peripheral wall tubes 142 have the same inner diameter and the same outer diameter. Each peripheral wall tube 142 has a structure in which a main tube 142a composed of carbon steel or a carbon steel alloy having a chrome content of approximately 1% to 2% is covered with a corrosion resistant layer 142b. An example of carbon steel includes STB 510, and examples of a carbon steel alloy include 1 Cr steel and 2 Cr steel, such as STBA 23. The corrosion resistant layer 142b has a thickness of, for example, several millimeters and may be composed of a nickel base alloy or a nickel-containing alloy having high corrosion resistance. Examples of a nickel base alloy include Inconel (registered trademark) 600, Inconel (registered trademark) 622, Inconel (registered trademark) 625, Inconel (registered trademark) 690, HR-160, HASTELLOY X (registered trademark), Alloy 72, and Alloy 72M.
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(56) The fins 140 are disposed on the inner and outer circumferential sides of a contact area CP of the peripheral wall tubes 142, instead of on the line connecting the centers of the peripheral wall tubes 142.
(57) The centers of the peripheral wall tubes 142 are disposed at positions corresponding to the throat diameter D of the gasifier wall 111. The peripheral wall tubes 142 are in direct contact with each other at the contact areas CP disposed on the line connecting the centers of the peripheral wall tubes 142.
(58)
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(60) With reference to
(61) The end 140c (the upper end in the drawing) of the folded sealing rod 140a is welded to the lower end of the single sealing rod 140a disposed in the upper portion. Such a welded structure is also provided at the folded portion at the lower end, although not illustrated.
(62) According to this embodiment, the following advantageous effects are achieved.
(63) In the throat section 117a of the cylindrical gasifier wall 111 where the horizontal cross-section of the flow channel in the throat section 117a is smaller than that of other regions of the gasifier wall 111, the peripheral wall tubes 142 are disposed in contact with each other to reduce the diameter of the horizontal cross-section of the cylindrical construction. In this way, the throat section 117a can be constructed of all of the peripheral wall tubes 142 of the gasifier wall 111 without forming a cylindrical construction by outwardly bending some of the peripheral wall tubes 142 of the gasifier wall 111 (without a so-called culled structure (see
(64) In a culled structure, the fins 140 have a large area because the distance between the peripheral wall tubes 142 is large near the culled peripheral wall tubes 142 (see
(65) The fins 140 are disposed on the inner circumferential side of the cylindrical gasifier wall 111. Thus, the spaces between adjacent peripheral wall tubes 142 can be certainly sealed, and strength can be enhanced.
(66) The welding can be readily carried out using the sealing rods 140a while enhancing the sealing ability. Thus, corrosive gases in the furnace can be prevented from coming into direct contact with the flat portions 142c or ground faces, and a reduction in corrosion resistance of the flat portions 142c can be prevented.
(67) In the region including the throat section 117a in which the diameter of the cross-section of the flow channel decreases, the fins 140 are disposed on the outer circumferential side of the cylindrical gasifier wall 111 in addition to the inner circumferential side. This can further enhance the sealing ability and the strength of the gasifier wall 111.
(68) The outer surfaces of at least some of the peripheral wall tubes 142 are cut to form the flat portions 142c (see
(69) The sealing rods 140a disposed on the inner and outer circumferential sides can enhance the sealing ability.
(70) Since the cut 140d are disposed in at least some of the sealing rods 140a, gas can be released to prevent the gas from being trapped in the space surrounded by the sealing rods 140a on the inner and outer circumferential sides and the pressure of the gas in the space excessively increasing. The cuts 140d disposed on the outer circumferential side can prevent the intrusion of corrosive gases into the inner space 154.
(71) By disposing the centers of the peripheral wall tubes 142 at equal radial distances from the center of the horizontal cross-section of the flow channel in the throat section 117a, all peripheral wall tubes 142 can be bent at the same position and angle. This enables ready manufacturing of many peripheral wall tubes 142 and ready manufacturing of the throat section 117a.
(72) In this embodiment, the flat portions 142c are disposed at the contact positions of the peripheral wall tubes 142. Alternatively, the peripheral wall tubes 142 may be disposed in direct contact with each other without the flat portions 142c if a desired throat diameter D can be achieved on the cross-section of the flow channel in the throat section 117a.
Second Embodiment
(73) A second embodiment of the present invention will now be described with reference to
(74) In this embodiment, the positions of the peripheral wall tubes 142 differ from those in the first embodiment. Other configurations in this embodiment are the same as those in the first embodiment, and thus the descriptions thereof are omitted.
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(76) The relation between the throat diameter D and the diameters D1 and D2 are defined by the following expression:
D=(D1+D2)/2
(77) In specific, the peripheral wall tubes 142 are disposed such that the average of the diameters D1 and D2 equals the throat diameter D.
(78) According to this embodiment, the following advantageous effects are achieved.
(79) By disposing the centers of the peripheral wall tubes 142 at different radial distances from the center of the horizontal cross-section of the flow channel in the throat section 117a, the throat diameter D can be further reduced in comparison to the diameter of the horizontal cross-sections of regions in which all peripheral wall tubes 142 are disposed at the same radial distance from the center of the horizontal cross-section of the flow channel. For example, this embodiment is suitable for a case in which the throat diameter D is larger than the desired throat diameter D even when all peripheral wall tubes 142 are disposed in direct contact with each other at the same radial distances.
(80) The adjacent peripheral wall tubes 142 are alternately disposed at two different radial distances from the center of the horizontal cross-section of the flow channel. This can limit the bending of the peripheral wall tubes 142 to two states, and thus the peripheral wall tubes 142 can be relatively readily manufactured. A desired throat diameter D can be relatively readily achieved, and thus the flexibility of design is enhanced.
(81) In this embodiment, the positions of the peripheral wall tubes 142 are limited to two different radial distances from the center of the horizontal cross-section of the flow channel. In the case where the throat diameter D is larger than the desired throat diameter D even with such positions, the peripheral wall tubes 142 may be disposed at three or more different radial distances. In such a case, three or more bending state are required for the peripheral wall tubes 142, but the flexibility of design in achieving a desired throat diameter D is further enhanced.
(82) Flat portions 142c may be disposed in the areas where the peripheral wall tubes 142 come into contact with each other, as in the first embodiment.
(83) An Integrated gasification combined cycle is described above as an example in the first and second embodiments. Alternatively, the present invention is not limited thereto and may be applied to a gasifier for a chemical plant without a power plant. The present invention is not limited to the furnace wall of a gasifier and may be applied to a furnace wall of a boiler including a water-cooled wall.
(84) In the embodiments described above, the fuel is coal. Alternatively, the fuel may be any carbonaceous feedstock, such as high-grade coal and low-grade coal. Other than coal, the fuel may be biomass, which is a renewable biological, organic resource, including, for example, wood thinned from forests, wood scraps, driftwood, grass, waste, sludge, tires, and fuel (palettes and chips) recycled from such biomass.
(85) In the embodiments described above, the gasifier 101 is a tower-type gasifier. Alternatively, the gasifier 101 may be a crossover-type gasifier accommodating components disposed such that the vertical direction of the components matches the flow direction of the raw syngas.
REFERENCE SIGNS LIST
(86) 10 Integrated gasification combined cycle (IGCC) 11 Coal feeder 11a Coal feeding line 14 Gasification unit 15 Char recovery unit 16 Gas purification unit 17 Gas turbine unit 18 Steam turbine unit 19 Generator 20 Heat recovery stream generator 41, 65 Compressed-air feeding line 42 Air separation unit 43 First nitrogen feeding line 45 Second nitrogen feeding line 46 Char returning line 47 Oxygen feeding line 48 Slag discharger 49 Gas production line 51 Precipitator 52 Feed hopper 53 Gas discharge line 61 Compressor 62 Combustor 63, 69 Turbine 64 Rotary shaft 66 Fuel-gas feeding line 67 Combustible-gas feeding line 68 Booster 70 Flue gas line 71 Steam feeding line 72 Steam recovery line 73 Condenser 74 Gas emission filter 75 Chimney 101 Gasifier 102 Syngas cooler 110 Pressure vessel 111 Gasifier wall (furnace wall) 115 Annular portion 116 Combustor 117 Diffuser 117a Throat section 118 Reductor 121 Gas exhaust port 122 Slag hopper 126, 127 Burner 131 Evaporator 132 Superheater 134 Economizer 140 Fin (connector) 140a Sealing rod (rod-like member) 140b Welded portion 140c End 140d Cut 142 Peripheral wall tube 142a Main tube 142b Corrosion resistant layer 142c Flat portion 143 Cooling-water circulating mechanism 144 Circulation channel 146 Cooler 148 Pump 150 Inlet header 152 Outlet header 154 Inner space 156 External space CP Contact area D Throat diameter