US20150253008A1 - Arrangement of a combustion system and a flue gas treatment system, and an injection method - Google Patents
Arrangement of a combustion system and a flue gas treatment system, and an injection method Download PDFInfo
- Publication number
- US20150253008A1 US20150253008A1 US14/197,506 US201414197506A US2015253008A1 US 20150253008 A1 US20150253008 A1 US 20150253008A1 US 201414197506 A US201414197506 A US 201414197506A US 2015253008 A1 US2015253008 A1 US 2015253008A1
- Authority
- US
- United States
- Prior art keywords
- flue gas
- arrangement
- combustion chamber
- fuel
- compressed
- 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.)
- Abandoned
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
- F23L7/00—Supplying non-combustible liquids or gases, other than air, to the fire, e.g. oxygen, steam
- F23L7/007—Supplying oxygen or oxygen-enriched air
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C9/00—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D1/00—Burners for combustion of pulverulent fuel
- F23D1/005—Burners for combustion of pulverulent fuel burning a mixture of pulverulent fuel delivered as a slurry, i.e. comprising a carrying liquid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23J—REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES
- F23J15/00—Arrangements of devices for treating smoke or fumes
- F23J15/02—Arrangements of devices for treating smoke or fumes of purifiers, e.g. for removing noxious material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
- F23L7/00—Supplying non-combustible liquids or gases, other than air, to the fire, e.g. oxygen, steam
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2202/00—Fluegas recirculation
- F23C2202/20—Premixing fluegas with fuel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23J—REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES
- F23J2215/00—Preventing emissions
- F23J2215/50—Carbon dioxide
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23J—REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES
- F23J2900/00—Special arrangements for conducting or purifying combustion fumes; Treatment of fumes or ashes
- F23J2900/15061—Deep cooling or freezing of flue gas rich of CO2 to deliver CO2-free emissions, or to deliver liquid CO2
-
- Y—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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery
Definitions
- the present invention relates to an arrangement of a combustion system and a flue gas treatment system, and an injection method.
- the combustion system can be a combustion system of a boiler of a power plant or an industrial furnace.
- the fuel is preferably a high density fuel, i.e. a fuel that needs the help of an additional fluid in order to be injected into a combustion chamber because of its high viscosity.
- heavy residue is a high viscosity fuel.
- the invention is applicable with any fuel also different from heavy residue when a fluid to help injection is required.
- High viscosity fuel can be used as fuel in combustion chambers of boilers or industrial furnaces; in this respect combustion chambers or furnaces are provided with injectors with nozzles.
- the injectors are supplied with fuel and in addition a gas or vapor, usually steam, to help injection.
- steam is supplied at one end of the nozzle and fuel is supplied through a side port into the nozzle, such that the steam passes through the nozzle and is injected into the combustion chamber and, while passing through the nozzle, the steam draws fuel through the port; the fuel is thus also injected into the combustion chamber.
- the steam used to promote fuel injection is usually withdrawn from the steam cycle; this is disadvantageous because steam is needed for power generation.
- An aspect of the invention includes providing an arrangement and a method that avoid or reduce the need of withdrawing steam from the steam cycle for fuel injection promotion.
- Another aspect of the invention includes providing an arrangement and a method by which the water consumption for fuel injection promotion can be avoided or reduced.
- FIG. 1 shows an example of the arrangement in a first embodiment
- FIG. 2 shows an example of the arrangement in a second embodiment
- FIG. 3 shows an example of the arrangement in a third embodiment
- FIG. 4 shows an example of the arrangement in a fourth embodiment
- FIG. 5 shows an example of injection.
- combustion system 2 preferably an oxy fuel combustion system, i.e. a combustion system in which fuel is combusted with pure or substantially pure oxygen; also combustion with air is anyhow possible
- flue gas treatment system 3 preferably an oxy fuel combustion system, i.e. a combustion system in which fuel is combusted with pure or substantially pure oxygen; also combustion with air is anyhow possible
- the combustion system 2 comprises a combustion chamber 5 of for example a boiler for generating steam to be expanded in a steam turbine for generating power or industrial furnace.
- the combustion chamber 5 has one or more injectors 6 that are connected to a gas supply line 7 and a fuel supply line 8 , such that the injectors 6 are supplied with both gas and fuel.
- the gas supply line 7 is connected to a source of compressed gas containing CO 2 .
- the source of compressed gas containing CO 2 is included in the arrangement 1 ; for example the source can be any connection to any part of the arrangement from which compressed gas containing CO 2 (such as flue gas and/or CO 2 with different purity degree) can be extracted.
- the compressed gas containing CO 2 can be pure or substantially pure CO2 or a gas mixture containing CO 2 , such as flue gas.
- FIG. 5 shows an example of a standard injector 6 .
- the injector of FIG. 5 comprises two nozzles 11 , but any number of nozzles 11 is possible, i.e. the injector 6 can have one or more nozzles 11 .
- the nozzles 11 are connected to the gas supply line 7 , for injecting the compressed gas containing CO 2 .
- Each nozzle 11 is connected to a side passage 12 , which in turn is connected to the fuel supply line 8 .
- the fuel is drawn from the compressed gas containing CO 2 that passes through the nozzles 11 .
- the flue gas treatment system 3 comprises a compressor 15 for compressing the flue gas discharged from the combustion chamber 5 .
- a mercury removal unit 16 and a dryer 17 are provided downstream of the compressor 15 .
- a mercury removal unit 16 and a dryer 17 are provided downstream of the mercury removal unit 16 and the dryer 17 heat exchangers 18 , 19 are provided; anyhow the mercury removal unit 16 , dryer 17 and heat exchangers 18 , 19 are not necessary and are installed according to the design and needs.
- the flue gas is supplied into a separation stage 20 that is downstream of the compressor 15 and is used for separating CO 2 from other gas contained in the flue gas.
- the separation stage 20 is connected to a line 21 for venting gas separated from the CO 2 and a line 22 for supplying the CO 2 into a compressor 23 (typically an intercooled, multistage compressor), a pump 24 (for supercritical CO 2 ) and storage 25 .
- a compressor 23 typically an intercooled, multistage compressor
- pump 24 for supercritical CO 2
- the source of compressed gas containing CO 2 is a connection 27 downstream of the compressor 15 and upstream of the separation stage 20 ; thus the compressed gas containing CO 2 is flue gas coming from the combustion chamber 5 .
- the gas supply line 7 is preferably connected immediately downstream of the compressor 15 , i.e. without any components between the compressor 15 and the connection 27 .
- the combustion chamber 5 is preferably an oxy-fuel combustion chamber; this allows generation of flue gas at the combustion chamber having a high CO 2 content, such as between 75-85% or even more.
- FIG. 2 shows an example of an arrangement similar to the first example (i.e. with the connection 27 between the compressor 15 and the separation stage) and two separation stages 20 a, 20 b.
- FIG. 3 shows an example (preferred example) in which the source of compressed gas containing CO 2 is a connection 27 at an interstage of the multistage flue gas compressor 15 .
- combustion chamber 5 is preferably an oxy-fuel combustion chamber.
- FIG. 4 shows an example of an arrangement in which the source of compressed gas containing CO 2 is a connection downstream of the separation stage (for example downstream the separation stage 20 a and/or 20 b ); thus the compressed gas containing CO 2 is substantially pure CO 2 coming from the separation stage.
- a heat exchanger 28 can also be provided; the heat exchanger 28 is used for heating the CO 2 separated at the separation stage 20 a by cooling the flue gas passing from the compressor 15 to the mercury removal unit 16 .
- the heat exchanger 28 is connected downstream of the compressor 15 and upstream of the separation stages 20 a, 20 b.
- the separation stages 20 a, 20 b can be realised in different ways and according to different technologies.
- they can include a plurality of separation stages 20 a, 20 b (in the examples of the drawings two separation stages); each separation stage can include a condensation step by cooling, in order to separate CO 2 from the other gas of the flue gas.
- Flue gas produced at the combustion chamber 5 is compressed at the compressor 15 and is then treated at the mercury removal unit 16 and dryer 17 (after cooling in the heat exchangers 18 , 19 ) and is then supplied into the separation stage 20 .
- the CO 2 is discharged and supplied to the compressor 23 , the pump and finally the CO 2 is fed into pipeline for use or storage 25 .
- the gas separated from the CO 2 (such as nitrogen, argon, etc.) is vented via line 21 .
- a part of the flue gas (as the compressed gas containing CO 2 ) at a pressure of about 10-15 bar and at a temperature of about 110° C. is diverted through the gas supply line 7 to the injectors 6 .
- fuel such as heavy residue is supplied; flue gas and fuel are thus injected into the combustion chamber 5 where combustion occurs.
- connection 27 which is at an interstage of the multistage compressor 15
- a part of the flue gas (as the compressed gas containing CO 2 ) at a pressure of about 10-15 bar is diverted through the gas supply line 7 to the injectors 6 .
- fuel such as heavy residue is supplied; flue gas and fuel are thus injected into the combustion chamber 5 where combustion occurs.
- the operation of the arrangement of FIG. 4 is also similar to the operation described.
- a part of the compressed CO 2 (as the compressed gas containing CO 2 ) at a pressure of about 10-15 bar is diverted through the gas supply line 7 ; this compressed CO 2 is heated at the heat exchanger 28 and is then forwarded to the injectors 6 .
- fuel such as heavy residue is supplied; compressed CO 2 and fuel are thus injected into the combustion chamber 5 where combustion occurs.
- the present invention also refers to a method for injecting fuel into a combustion chamber.
- the method comprises supplying a compressed gas containing CO 2 to injectors 6 , supplying a fuel to the injectors 6 , injecting the compressed gas containing CO 2 and the fuel into the combustion chamber 5 together.
- Injecting comprises injecting the compressed gas containing CO 2 through nozzles 11 , and having the fuel drawn from the gas passing through the nozzle 11 and injected from the nozzle 11 together with the compressed gas containing CO 2 .
- supplying the compressed gas containing CO 2 comprises withdrawing at least a part of flue gas at an interstage during multistage compression and/or downstream of compression and/or upstream of the separation, and/or withdrawing at least a part of the separated CO 2 .
- the separated CO 2 is preferably heated by cooling the flue gas.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Treating Waste Gases (AREA)
Abstract
Description
- The present invention relates to an arrangement of a combustion system and a flue gas treatment system, and an injection method.
- The combustion system can be a combustion system of a boiler of a power plant or an industrial furnace. In addition the fuel is preferably a high density fuel, i.e. a fuel that needs the help of an additional fluid in order to be injected into a combustion chamber because of its high viscosity. For example heavy residue is a high viscosity fuel. The invention is applicable with any fuel also different from heavy residue when a fluid to help injection is required.
- High viscosity fuel can be used as fuel in combustion chambers of boilers or industrial furnaces; in this respect combustion chambers or furnaces are provided with injectors with nozzles.
- The injectors are supplied with fuel and in addition a gas or vapor, usually steam, to help injection.
- Typically steam is supplied at one end of the nozzle and fuel is supplied through a side port into the nozzle, such that the steam passes through the nozzle and is injected into the combustion chamber and, while passing through the nozzle, the steam draws fuel through the port; the fuel is thus also injected into the combustion chamber.
- The steam used to promote fuel injection is usually withdrawn from the steam cycle; this is disadvantageous because steam is needed for power generation.
- In addition, since the steam injected into the combustion chamber with the fuel becomes contaminated from the combustion products, the steam from the flue gas is not recovered and recycled. This causes a water consumption that can be very disadvantageous, in particular in countries where water is expensive (water can be more expensive than oil).
- An aspect of the invention includes providing an arrangement and a method that avoid or reduce the need of withdrawing steam from the steam cycle for fuel injection promotion.
- Another aspect of the invention includes providing an arrangement and a method by which the water consumption for fuel injection promotion can be avoided or reduced.
- These and further aspects are attained by providing an arrangement and a method in accordance with the accompanying claims.
- Further characteristics and advantages will be more apparent from the description of a preferred but non-exclusive embodiment of the arrangement and method, illustrated by way of non-limiting example in the accompanying drawings, in which:
-
FIG. 1 shows an example of the arrangement in a first embodiment; -
FIG. 2 shows an example of the arrangement in a second embodiment; -
FIG. 3 shows an example of the arrangement in a third embodiment; -
FIG. 4 shows an example of the arrangement in a fourth embodiment; and -
FIG. 5 shows an example of injection. - With reference to the figures, these show an
arrangement 1 of a combustion system 2 (preferably an oxy fuel combustion system, i.e. a combustion system in which fuel is combusted with pure or substantially pure oxygen; also combustion with air is anyhow possible) and a fluegas treatment system 3. - The
combustion system 2 comprises acombustion chamber 5 of for example a boiler for generating steam to be expanded in a steam turbine for generating power or industrial furnace. - The
combustion chamber 5 has one ormore injectors 6 that are connected to agas supply line 7 and afuel supply line 8, such that theinjectors 6 are supplied with both gas and fuel. - The
gas supply line 7 is connected to a source of compressed gas containing CO2. Preferably the source of compressed gas containing CO2 is included in thearrangement 1; for example the source can be any connection to any part of the arrangement from which compressed gas containing CO2 (such as flue gas and/or CO2 with different purity degree) can be extracted. The compressed gas containing CO2 can be pure or substantially pure CO2 or a gas mixture containing CO2, such as flue gas. -
FIG. 5 shows an example of astandard injector 6. The injector ofFIG. 5 comprises twonozzles 11, but any number ofnozzles 11 is possible, i.e. theinjector 6 can have one ormore nozzles 11. Thenozzles 11 are connected to thegas supply line 7, for injecting the compressed gas containing CO2. - Each
nozzle 11 is connected to aside passage 12, which in turn is connected to thefuel supply line 8. During operation, the fuel is drawn from the compressed gas containing CO2 that passes through thenozzles 11. - The flue
gas treatment system 3 comprises acompressor 15 for compressing the flue gas discharged from thecombustion chamber 5. - Usually, downstream of the compressor 15 a
mercury removal unit 16 and adryer 17 are provided. Upstream of themercury removal unit 16 and thedryer 17heat exchangers mercury removal unit 16,dryer 17 andheat exchangers - From the
dryer 17 the flue gas is supplied into aseparation stage 20 that is downstream of thecompressor 15 and is used for separating CO2 from other gas contained in the flue gas. - The
separation stage 20 is connected to aline 21 for venting gas separated from the CO2 and aline 22 for supplying the CO2 into a compressor 23 (typically an intercooled, multistage compressor), a pump 24 (for supercritical CO2) andstorage 25. - In a first example (
FIG. 1 ), the source of compressed gas containing CO2 is aconnection 27 downstream of thecompressor 15 and upstream of theseparation stage 20; thus the compressed gas containing CO2 is flue gas coming from thecombustion chamber 5. - In this embodiment, the
gas supply line 7 is preferably connected immediately downstream of thecompressor 15, i.e. without any components between thecompressor 15 and theconnection 27. - The
combustion chamber 5 is preferably an oxy-fuel combustion chamber; this allows generation of flue gas at the combustion chamber having a high CO2 content, such as between 75-85% or even more. -
FIG. 2 shows an example of an arrangement similar to the first example (i.e. with theconnection 27 between thecompressor 15 and the separation stage) and twoseparation stages -
FIG. 3 shows an example (preferred example) in which the source of compressed gas containing CO2 is aconnection 27 at an interstage of the multistageflue gas compressor 15. - Also in this example the
combustion chamber 5 is preferably an oxy-fuel combustion chamber. -
FIG. 4 shows an example of an arrangement in which the source of compressed gas containing CO2 is a connection downstream of the separation stage (for example downstream theseparation stage 20 a and/or 20 b); thus the compressed gas containing CO2 is substantially pure CO2 coming from the separation stage. - In this embodiment, a
heat exchanger 28 can also be provided; theheat exchanger 28 is used for heating the CO2 separated at theseparation stage 20 a by cooling the flue gas passing from thecompressor 15 to themercury removal unit 16. Theheat exchanger 28 is connected downstream of thecompressor 15 and upstream of theseparation stages - The
separation stages separation stages - The operation of the arrangement is apparent from that described and illustrated and is substantially the following (reference to
FIG. 1 is made). - Flue gas produced at the
combustion chamber 5 is compressed at thecompressor 15 and is then treated at themercury removal unit 16 and dryer 17 (after cooling in theheat exchangers 18, 19) and is then supplied into theseparation stage 20. From theseparation stage 20 the CO2 is discharged and supplied to thecompressor 23, the pump and finally the CO2 is fed into pipeline for use orstorage 25. In addition, the gas separated from the CO2 (such as nitrogen, argon, etc.) is vented vialine 21. - At the connection 27 (between the
compressor 15 and the separation stage 20) a part of the flue gas (as the compressed gas containing CO2) at a pressure of about 10-15 bar and at a temperature of about 110° C. is diverted through thegas supply line 7 to theinjectors 6. At theinjectors 6 also fuel such as heavy residue is supplied; flue gas and fuel are thus injected into thecombustion chamber 5 where combustion occurs. - The operation of the arrangement of
FIG. 3 is similar to the operation described; in particular at the connection 27 (which is at an interstage of the multistage compressor 15) a part of the flue gas (as the compressed gas containing CO2) at a pressure of about 10-15 bar is diverted through thegas supply line 7 to theinjectors 6. At theinjectors 6 also fuel such as heavy residue is supplied; flue gas and fuel are thus injected into thecombustion chamber 5 where combustion occurs. - The operation of the arrangement of
FIG. 4 is also similar to the operation described. In particular, at the connection 27 (between theseparation stage 20 and the compressor 23) a part of the compressed CO2 (as the compressed gas containing CO2) at a pressure of about 10-15 bar is diverted through thegas supply line 7; this compressed CO2 is heated at theheat exchanger 28 and is then forwarded to theinjectors 6. At theinjectors 6 also fuel such as heavy residue is supplied; compressed CO2 and fuel are thus injected into thecombustion chamber 5 where combustion occurs. - The present invention also refers to a method for injecting fuel into a combustion chamber.
- The method comprises supplying a compressed gas containing CO2 to
injectors 6, supplying a fuel to theinjectors 6, injecting the compressed gas containing CO2 and the fuel into thecombustion chamber 5 together. - Injecting comprises injecting the compressed gas containing CO2 through
nozzles 11, and having the fuel drawn from the gas passing through thenozzle 11 and injected from thenozzle 11 together with the compressed gas containing CO2. - In different examples, supplying the compressed gas containing CO2 comprises withdrawing at least a part of flue gas at an interstage during multistage compression and/or downstream of compression and/or upstream of the separation, and/or withdrawing at least a part of the separated CO2. In this last case the separated CO2 is preferably heated by cooling the flue gas.
- Naturally the features described may be independently provided from one another.
- In practice the materials used and the dimensions can be chosen at will according to requirements and to the state of the art.
Claims (16)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/197,506 US20150253008A1 (en) | 2014-03-05 | 2014-03-05 | Arrangement of a combustion system and a flue gas treatment system, and an injection method |
EP15154546.4A EP2916071A1 (en) | 2014-03-05 | 2015-02-10 | Combustion system with co2-sequestration and recirculation |
SA116370651A SA116370651B1 (en) | 2014-03-05 | 2015-02-26 | An arrangement of a combustion system and a flue gas treatment system, and an injection method |
SA115360334A SA115360334B1 (en) | 2014-03-05 | 2015-02-26 | An arrangement of a combustion system and a flue gas treatment system, and an injection method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/197,506 US20150253008A1 (en) | 2014-03-05 | 2014-03-05 | Arrangement of a combustion system and a flue gas treatment system, and an injection method |
Publications (1)
Publication Number | Publication Date |
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US20150253008A1 true US20150253008A1 (en) | 2015-09-10 |
Family
ID=52814786
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US14/197,506 Abandoned US20150253008A1 (en) | 2014-03-05 | 2014-03-05 | Arrangement of a combustion system and a flue gas treatment system, and an injection method |
Country Status (3)
Country | Link |
---|---|
US (1) | US20150253008A1 (en) |
EP (1) | EP2916071A1 (en) |
SA (2) | SA116370651B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN119150759A (en) * | 2024-11-21 | 2024-12-17 | 北京宇航系统工程研究所 | Interstage heat separation equivalent simulation test method based on explosion impact |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
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US20120304905A1 (en) * | 2011-06-05 | 2012-12-06 | Chendhil Periasamy | Solid Fuel and Oxygen Combustion with Low NOx and Efficient Burnout |
US20130092062A1 (en) * | 2010-06-16 | 2013-04-18 | Masahiko Matsuda | Combustion system |
US20130125555A1 (en) * | 2010-08-06 | 2013-05-23 | Franklin F. Mittricker | Systems and Methods For Optimizing Stoichiometric Combustion |
US20130244190A1 (en) * | 2010-09-29 | 2013-09-19 | Fortum Corporation | Oxygen combustion system and method for operating same |
US20130319303A1 (en) * | 2011-02-14 | 2013-12-05 | Alstom Technology Ltd | Method and system for milling a fuel for an oxy-fuel combustion burner |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8636500B2 (en) * | 2008-09-26 | 2014-01-28 | Air Products And Chemicals, Inc. | Transient operation of oxy/fuel combustion system |
DE102010026792B4 (en) * | 2010-07-10 | 2012-02-16 | Messer Group Gmbh | Method of operating an oxyfuel power plant |
-
2014
- 2014-03-05 US US14/197,506 patent/US20150253008A1/en not_active Abandoned
-
2015
- 2015-02-10 EP EP15154546.4A patent/EP2916071A1/en not_active Withdrawn
- 2015-02-26 SA SA116370651A patent/SA116370651B1/en unknown
- 2015-02-26 SA SA115360334A patent/SA115360334B1/en unknown
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20130092062A1 (en) * | 2010-06-16 | 2013-04-18 | Masahiko Matsuda | Combustion system |
US20130125555A1 (en) * | 2010-08-06 | 2013-05-23 | Franklin F. Mittricker | Systems and Methods For Optimizing Stoichiometric Combustion |
US20130244190A1 (en) * | 2010-09-29 | 2013-09-19 | Fortum Corporation | Oxygen combustion system and method for operating same |
US20130319303A1 (en) * | 2011-02-14 | 2013-12-05 | Alstom Technology Ltd | Method and system for milling a fuel for an oxy-fuel combustion burner |
US20120304905A1 (en) * | 2011-06-05 | 2012-12-06 | Chendhil Periasamy | Solid Fuel and Oxygen Combustion with Low NOx and Efficient Burnout |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN119150759A (en) * | 2024-11-21 | 2024-12-17 | 北京宇航系统工程研究所 | Interstage heat separation equivalent simulation test method based on explosion impact |
Also Published As
Publication number | Publication date |
---|---|
SA115360334B1 (en) | 2016-06-15 |
SA116370651B1 (en) | 2020-08-13 |
EP2916071A1 (en) | 2015-09-09 |
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