[go: up one dir, main page]

WO2002053969A1 - Dispositif destine a la combustion d'un combustible carbone dans une atmosphere sans azote et procede d'utilisation de ce dispositif - Google Patents

Dispositif destine a la combustion d'un combustible carbone dans une atmosphere sans azote et procede d'utilisation de ce dispositif Download PDF

Info

Publication number
WO2002053969A1
WO2002053969A1 PCT/NO2001/000499 NO0100499W WO02053969A1 WO 2002053969 A1 WO2002053969 A1 WO 2002053969A1 NO 0100499 W NO0100499 W NO 0100499W WO 02053969 A1 WO02053969 A1 WO 02053969A1
Authority
WO
WIPO (PCT)
Prior art keywords
oxygen
gas stream
gas
combustion
stream
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.)
Ceased
Application number
PCT/NO2001/000499
Other languages
English (en)
Inventor
Tor Bruun
Leif GRØNSTAD
Kåre KRISTIANSEN
Bjørnar WERSWICK
Ulf Linder
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Norsk Hydro ASA
GE Power Sweden AB
Original Assignee
Norsk Hydro ASA
Alstom Power Sweden AB
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=19911963&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=WO2002053969(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Norsk Hydro ASA, Alstom Power Sweden AB filed Critical Norsk Hydro ASA
Priority to EP01985460A priority Critical patent/EP1356233A1/fr
Priority to US10/451,729 priority patent/US20050053878A1/en
Priority to JP2002554435A priority patent/JP2004533594A/ja
Publication of WO2002053969A1 publication Critical patent/WO2002053969A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • 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 
    • F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
    • F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D53/00—Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols
    • B01D53/22—Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols by diffusion
    • C—CHEMISTRY; METALLURGY
    • C01—INORGANIC CHEMISTRY
    • C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
    • C01B13/00—Oxygen; Ozone; Oxides or hydroxides in general
    • C01B13/02—Preparation of oxygen
    • C01B13/0229—Purification or separation processes
    • C01B13/0248—Physical processing only
    • C01B13/0251—Physical processing only by making use of membranes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
    • F02C1/04—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid the working fluid being heated indirectly
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
    • 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
    • F23L15/00—Heating of air supplied for combustion
    • F23L15/04—Arrangements of recuperators
    • 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
    • C—CHEMISTRY; METALLURGY
    • C01—INORGANIC CHEMISTRY
    • C01B—NON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
    • C01B2210/00—Purification or separation of specific gases
    • C01B2210/0043—Impurity removed
    • C01B2210/0046—Nitrogen
    • 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
    • F23L2900/00—Special arrangements for supplying or treating air or oxidant for combustion; Injecting inert gas, water or steam into the combustion chamber
    • F23L2900/07006—Control of the oxygen supply
    • 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
    • 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
    • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P20/00—Technologies relating to chemical industry
    • Y02P20/10—Process efficiency

Definitions

  • the present invention relates to a device for combustion of a carbon containing fuel in a nitrogen free atmosphere and a method for operating said device.
  • C0 2 can be removed from cooled exhaust gas, normally discharged at near atmospheric pressure, by means of several separation processes, e.g. chemical active separation processes, physical absorption processes, adsorption by molecular sieves, membrane separation and cryogenic techniques. Chemical absorption, for instance by means of alkanole amines, is considered as the most practical and economical method to separate C0 2 from exhaust gas. These separation processes consume energy and require heavy and voluminous equipment. Applied in connection with a power generation process, these separation processes will reduce the power output with 10% or more.
  • separation processes e.g. chemical active separation processes, physical absorption processes, adsorption by molecular sieves, membrane separation and cryogenic techniques.
  • Chemical absorption for instance by means of alkanole amines, is considered as the most practical and economical method to separate C0 2 from exhaust gas. These separation processes consume energy and require heavy and voluminous equipment. Applied in connection with a power generation process, these separation processes will reduce the power output with 10% or more.
  • a sweep gas is applied to reduce the partial pressure of oxygen on the oxygen receiving side of the membrane and thereby increase the flux of oxygen through the membrane; as e.g. described in US 5562754 and NO-A-972632.
  • Combustion of natural gas with pure oxygen will produce an exhaust gas containing the two main products carbon dioxide and water (steam).
  • the exhaust gas is utilized as the oxygen receiving gas.
  • the oxygen rich gas stream i.e. the oxygen enriched exhaust gas
  • the thermal energy produced by the combustion reaction is by means of heat exchanger(s) utilized to heat air fed to the MCM-module(s) as well as to heat oxygen depleted air leaving the MCM-module(s) before it may enter a power generation turbine or a chemical plant performing an endothermic reaction.
  • the exhaust gas is utilized as a sweep gas to pick up oxygen in the membrane module(s) and transport oxygen to one or more combustion chambers where fuel is added.
  • the heat generated in the exhaust gas should in an efficient way be transported to the air stream, and in such a way, that leakage between sweep gas and air is prevented or minimised to an acceptable level.
  • This feature is very important because a controlled leakage of gas is necessary to build up and equalise the pressure inside the reactor house, and only one of the gases is allowed to leak to prevent mixing. This controlled and necessary leakage allows a flexible sealing of defined leakage rate for the bypassing connectors of the second gas. Flexibility to avoid thermal stress in connecting parts/monolithic structures is very important to prevent fatal cracks.
  • Fig. 1 shows a sketch of one embodiment of the device according to the present invention including its functional parts as heat exchange module, MCM-module and combustion chamber. Also included is a pressure booster, here shown as a jet ejector driven by high pressure (HP) steam. In this embodiment the modules are all installed within the reactor.
  • HP high pressure
  • Fig. 3 shows a sketch of a multichannel monolith structure utilized as a MCM- module and/or as a heat exchange module.
  • Fig. 4 shows one embodiment of the reactor with the different modules as well as the other functional components in the reactor.
  • Fig. 5 shows different shapes of connectors between the MCM- and the heat exchange modules as well as different methods applied for sealing of the connectors between the modules.
  • FIG 1 shows a principal sketch of the device according to the present invention where the process streams and the important process units (H-01), (X-01), (H-02), (F-01) and (1-01) are shown.
  • the units are all installed inside the reactor pressure shell which is in this example identical to the device shell.
  • the figure shows that an oxygen containing gas stream (here air) is conducted trough a compressor.
  • the compressed air stream (AN-030) is further fed to the heat exchange module (H-01) where it is heated (AN-050) before entering the mixed conducting membrane module (X-01) in which oxygen is separated from the air stream resulting in an oxygen depleted air stream (AL-010).
  • the oxygen depleted air stream (AL-010) enters the heat exchanger (H-02) for further heating before leaving the device (AL-020).
  • the depleted air stream (AL-020) may be fed to a power generation turbine or a chemical plant performing endothermic reactions.
  • a sweep gas (EG-020) is fed to the MCM-module (X-01 ) and is picking up oxygen at the oxygen receiving side of the membrane and further transported through heat exchange module (H-01).
  • the oxygen enriched gas stream (EGO-030) is then pressurized in a pressure booster (1-01) before entering the combustion chamber (F-01).
  • the combustion chamber (F-01) where fuel (NG-010) is added and burned is in this example installed inside the reactor pressure shell.
  • the combustion gas or exhaust (EG-010) is now almost oxygen free due to combustion in (F-01).
  • this is a jet pump driven by injection of high pressure (HP) steam.
  • the jet pump has the advantage of no moving parts and might be built in a material (i.e. ceramic) that can withstand very high temperatures.
  • the oxygen depleted gas stream (AL-020) and the bleed gas stream (EG-040) may be fed to gas turbines to generate power.
  • the bleed gas (EG-040) containing the main combustion products (C0 2 + H 2 0) will have a high temperature (combustion gas temperature).
  • a gas turbine capable of handling the CO2 and H 2 0 mixture is needed.
  • Another power generating alternative for this stream is to cool down the gas to a temperature ⁇ 550°C where a conventional steam turbine can be used.
  • FIG. 2 shows another embodiment of the device according to the present invention where the pressure booster (1-01) and the combustion chamber (F-01) are installed outside the reactor pressure shell but within the device shell. This feature contributes to simplify the construction of the device.
  • the advantage of installing (1-01) and (F-01) outside the reactor is to facilitate the maintenance work and makes it possible to apply cooling apparatus.
  • a rotary pressure increasing machine can be used as a pressure booster (1-01) as envisaged in this figure.
  • the flow path in this embodiment is the same as in the embodiment shown in Figure 1.
  • An external combustion chamber will also simplify the fuel (NG-010) injection system and makes it easier to upscale the device as will be shown in Figure 8.
  • Figure 3 shows a multichannel monolith structure which, according to the present invention might preferably be utilized as both a heat exchange module and a membrane module.
  • such structures are advantageous mainly because of their simple way to be manufactured.
  • the present invention is not restricted to application of such structures only and other configurations (e.g. plates) may be an alternative.
  • Gas 1 represents gas streams (AN-030) and (AN-050) if the monolith structure is module (H-01), gas streams (AN-050) and (AL-010) if the monolith structure is module (X-01). If the monolith structure is module (H-02), then Gas 1 is gas streams (AL-010) and (AL-020).
  • Gas 2 represents the gas streams (EGO-020) and (EGO-030) if the module is (H-01), the gas streams (EG-030) and (EGO-010/020) if the module is (X-01) and gas streams (EG-020) and (EG-030) if the module is (H-02).
  • FIG 6 shows one embodiment of the device according to the illustration in Figure 2, where the combustion chamber (F-01), as well as the pressure booster (1-01) are installed outside the reactor.
  • Fuel (NG) is injected in the low temperature zone prior to (1-01) to ensure a good mixing with the oxygen enriched sweep gas (EGO) before entering the combustion chamber (F-01). Due to a too low temperature the combustion, at least partly, might be enhanced by a catalyst.
  • the sweep gas stream (EGO) leaving (H-01) is cooled down by the air stream (AN) and has its lowest temperature before (1-01).
  • the pressure in the stream (EGO) is increased by means of (1-01) before entering the combustion chamber (F-01) outside the reactor.
  • oxygen in stream (EGO) reacts with added fuel and a combustion is obtained.
  • bleed gas Either from the oxygen enriched sweep gas (EGO) or from the exhaust gas (EG) a bleed gas has to be taken out to prevent accumulation of mass in the sweep gas loop due to the oxygen transfer from the air and the addition of the fuel.
  • Example of bleed gas outlet is shown in Figures 8.1 and 9.1.
  • the coupling part 11 preferably will be glass sealed in both ends to 9 and 15 and part 21 respectively will be sealed to 15 and 19.
  • the material in 11 has to match the thermal expansion of both 9 and 15 and respectively the material in 21 has to match the thermal expansion of 15 and 19.
  • One option is to extrude these connec- tion parts 11 and 21 with a gradual change in composition of material such that the material in the end of 11 connected to 9 matches its thermal expansion, respectively the other end of 11 matches the thermal expansion of 14.
  • 21 also could be made in such a way that thermal expansion is matching material in both 15 and 19 to prevent cracks.
  • the inlet plenum room for air, unit 7 could be glass sealed to the low temperature heat exchanger 9 to ensure minimum leakage.
  • the material in 7 has to match the thermal expansion of 9.
  • the outlet plenum 23 for oxygen depleted air might be glass sealed to 18 and 19 and thus 23 has to be made of a material that matches 18 and 19 in thermal expansion.
  • Part 7 is in the inlet end (incoming air) made of a round shape (pipe) to make it easier to fit into a flexible sealing 5. Respectively this is also done for the outlet plenum 23 (of the oxygen depleted high temperature air).
  • a ring sealing, 24 is shown. For a vertical orientation as shown in Figure 7 a lower flexible sealing may not be necessary.
  • Figure 8.1 shows one embodiment of the device according to the present invention where the device is integrated with gas turbines.
  • Figure 8.2 shows another embodiment of integrating the reactor with gas turbines where more than one reactor have a common combustion chamber.
  • FIG.1 shows the device according to the present invention with the flow direction of the different gas streams.
  • the figure shows that an oxygen containing gas stream (AN-030), preferably a compressed air stream, is fed to the heat exchange module (H-01) where the gas stream is heated before entering the mixed conducting membrane module (X-01). Oxygen is transported through the membrane wall to be picked up by the sweep gas stream (EG-030). An oxygen enriched sweep gas stream leaves the module (X-01) now named (EGO-010).
  • AN-030 preferably a compressed air stream
  • F-02 additional combustion chamber
  • the sweep gas stream (EGO-020) entering the heat exchanger (H-01) will have somewhat higher temperature than the stream (EGO-010) and somewhat lower content of oxygen.
  • the sweep gas stream (EGO-020) is then fed to the heat exchanger (H-01) for heating incoming air to the MCM-module (X-01).
  • the sweep gas stream (EGO-030) leaving (H-01) has now its lowest temperature and is supplied to the main combustion chamber (F-01) outside the reactor where most of the fuel (NG-020) is burned.
  • a pressure booster (1-01) is installed close to the inlet of the main combustion chamber (F-01). The pressure increase from (EGO-030) to (EGO-040) enhanced by the pressure booster (1-01) is to ensure circulation in the sweep/exhaust gas loop.
  • a part of the hot exhaust gas (EG-040) is discharged as a bleed stream to prevent accumulation of mass in the exhaust/sweep gas loop.
  • the bleed gas stream (EG-040) can be discharged anywhere in the sweep gas circulation loop. For example it can be discharged in the cold end, from (EGO-030), and sent directly to a steam turbine.
  • the exhaust gas (EG-020) is fed via the high temperature heat exchanger (H-02) to the membrane module (X-01).
  • Acting as sweep gas, (EG-030) is receiving oxygen transported through the membrane from the air side and further transports the oxygen to the combustion chamber.
  • a closed loop with a continuous combustion of a carbon rich fuel with O2 in a C0 2 and H 2 0 rich atmosphere is obtained.
  • Figure 9.2 shows how the plenum inlet and outlet 7 and 23 and heat exchangers (H-01) and (H-02) and the MCM-module (X-01) can be built into one sealed unit.
  • This is to illustrate one important feature of the present invention which is the flow direction or flow paths of the two main streams air and sweep gas that contributes to minimize the leakage between air and sweep gas stream.
  • the air stream has a straight flow and flows directly through the inner closed rooms between the heat exchangers (H-01) and (H-02) and the MCM-module (X-01), while the sweep gas stream flows in and out of the open side slots of (H-01), (X-01) and (H-02).
  • the sweep gas should be allowed to fill the open space of the reactor.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Analytical Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Inorganic Chemistry (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Separation Using Semi-Permeable Membranes (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Air Supply (AREA)
  • Solid Fuels And Fuel-Associated Substances (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Feeding And Controlling Fuel (AREA)

Abstract

La présente invention concerne un dispositif destiné à la combustion d'un combustible carboné dans une atmosphère sans azote et un procédé d'utilisation de ce dispositif. Ce dispositif peut être intégré dans un groupe de production d'énergie (c'est-à-dire une ou plusieurs turbines à gaz) pour obtenir un procédé à haut rendement énergétique destiné à la production d'énergie avec réduction des émissions de dioxyde de carbone et de NOx dans l'atmosphère. Par ailleurs, ce dispositif peut être intégré dans une usine chimique procédant à des réactions endothermiques.
PCT/NO2001/000499 2000-12-29 2001-12-19 Dispositif destine a la combustion d'un combustible carbone dans une atmosphere sans azote et procede d'utilisation de ce dispositif Ceased WO2002053969A1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP01985460A EP1356233A1 (fr) 2000-12-29 2001-12-19 Dispositif destine a la combustion d'un combustible carbone dans une atmosphere sans azote et procede d'utilisation de ce dispositif
US10/451,729 US20050053878A1 (en) 2000-12-29 2001-12-19 Device for combustion of a carbon containing fuel in a nitrogen free atmosphere and a method for operating said device
JP2002554435A JP2004533594A (ja) 2000-12-29 2001-12-19 無窒素雰囲気中での炭素含有燃料の燃焼のための装置およびその装置を運転するための方法

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
NO20006690A NO318619B1 (no) 2000-12-29 2000-12-29 Anordning for forbrenning av et karbonholdig brensel, en fremgangsmate for a betjene nevnte anordning, samt anvendelse av anordningen.
NO200006690 2000-12-29

Publications (1)

Publication Number Publication Date
WO2002053969A1 true WO2002053969A1 (fr) 2002-07-11

Family

ID=19911963

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/NO2001/000499 Ceased WO2002053969A1 (fr) 2000-12-29 2001-12-19 Dispositif destine a la combustion d'un combustible carbone dans une atmosphere sans azote et procede d'utilisation de ce dispositif

Country Status (5)

Country Link
US (1) US20050053878A1 (fr)
EP (1) EP1356233A1 (fr)
JP (1) JP2004533594A (fr)
NO (1) NO318619B1 (fr)
WO (1) WO2002053969A1 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004065770A1 (fr) * 2003-01-20 2004-08-05 Alstom Power Sweden Ab Regulation d'une turbine a gaz au moyen d'un reacteur generant de l'air chaud
WO2008087150A1 (fr) * 2007-01-19 2008-07-24 Siemens Aktiengesellschaft Installation de combustion
WO2009064539A3 (fr) * 2007-11-14 2010-04-15 Alstom Technology Ltd Chaudière et dispositif de production d'oxygène intégré
US20140231588A1 (en) * 2004-11-23 2014-08-21 Biosphere Aerospace, Llc Method and system for loading and unloading cargo assembly onto and from an aircraft

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AUPR421501A0 (en) 2001-04-04 2001-05-03 U.S. Filter Wastewater Group, Inc. Potting method
AUPR692401A0 (en) 2001-08-09 2001-08-30 U.S. Filter Wastewater Group, Inc. Method of cleaning membrane modules
CA2544626C (fr) 2003-11-14 2016-01-26 U.S. Filter Wastewater Group, Inc. Dispositif d'aeration et de lavage a contre-courant ferme pour utilisation avec un module de filtration a membrane
WO2005092799A1 (fr) 2004-03-26 2005-10-06 U.S. Filter Wastewater Group, Inc. Processus et appareil de purification d'eau impure au moyen d'une microfiltration ou d'une ultrafiltration associee a une osmose inversee
WO2006026814A1 (fr) 2004-09-07 2006-03-16 Siemens Water Technologies Corp. Reduction des rejets liquides de decolmatage
CN101039739B (zh) 2004-09-14 2014-10-08 伊沃夸水处理技术有限责任公司 从薄膜组件上去除固体的方法和设备
NZ553771A (en) 2004-09-15 2010-11-26 Siemens Water Tech Corp Continuously variable aeration of membrane filtration system and flow control device when used in such application
CA2591580A1 (fr) 2004-12-24 2006-06-29 Siemens Water Technologies Corp. Procede et appareil simples de lavage au gaz
EP2394731A1 (fr) 2004-12-24 2011-12-14 Siemens Industry, Inc. Clarification dans des systèmes de filtration sur membrane
EP1885475B1 (fr) * 2005-04-29 2015-03-25 Evoqua Water Technologies LLC Système de nettoyage chimique pour filtre à membrane
EP1945333B1 (fr) 2005-08-22 2011-06-08 Siemens Industry, Inc. Ensemble pour filtration d'eau pour réduire le volume de lavage à contre-courant
US8318028B2 (en) 2007-04-02 2012-11-27 Siemens Industry, Inc. Infiltration/inflow control for membrane bioreactor
US9764288B2 (en) 2007-04-04 2017-09-19 Evoqua Water Technologies Llc Membrane module protection
CN109107392B (zh) 2007-05-29 2024-11-01 杜邦特种材料新加坡私人有限公司 使用脉冲气提泵的膜清洗
EP2026004A1 (fr) * 2007-08-07 2009-02-18 Siemens Aktiengesellschaft Procédé de fonctionnement d'une installation de combustion et installation de combustion
GB0808200D0 (en) * 2008-05-06 2008-06-11 Invista Technologies Srl Power recovery
WO2010009518A1 (fr) 2008-07-24 2010-01-28 Siemens Water Technologies Corp. Système de cadre pour modules de filtration sur membrane
AU2009281935A1 (en) * 2008-08-14 2010-02-18 Siemens Industry, Inc. Block configuration for large scale membrane distillation
CA2734796A1 (fr) 2008-08-20 2010-02-25 Siemens Water Technologies Corp. Rendement energetique ameliore du lavage a contre-courant d'un systeme a membrane
WO2010142673A1 (fr) * 2009-06-11 2010-12-16 Siemens Water Technologies Corp. Procédés de nettoyage d'une membrane polymère poreuse et kit pour le nettoyage d'une membrane polymère poreuse
US8858223B1 (en) * 2009-09-22 2014-10-14 Proe Power Systems, Llc Glycerin fueled afterburning engine
WO2011136888A1 (fr) 2010-04-30 2011-11-03 Siemens Industry, Inc Dispositif de distribution d'un écoulement de fluide
US9856769B2 (en) 2010-09-13 2018-01-02 Membrane Technology And Research, Inc. Gas separation process using membranes with permeate sweep to remove CO2 from combustion exhaust
US9457313B2 (en) * 2010-09-13 2016-10-04 Membrane Technology And Research, Inc. Membrane technology for use in a power generation process
CN103118766B (zh) 2010-09-24 2016-04-13 伊沃夸水处理技术有限责任公司 膜过滤系统的流体控制歧管
JP2014528352A (ja) 2011-09-30 2014-10-27 エヴォクア ウォーター テクノロジーズ エルエルシーＥｖｏｑｕａ Ｗａｔｅｒ Ｔｅｃｈｎｏｌｏｇｉｅｓｌｌｃ 改良したマニホルド構造
KR102177864B1 (ko) 2011-09-30 2020-11-13 에보쿠아 워터 테크놀로지스 엘엘씨 아이솔레이션 밸브
AU2013280452B2 (en) 2012-06-28 2017-07-20 Evoqua Water Technologies Llc A potting method
WO2014052071A1 (fr) 2012-09-26 2014-04-03 Evoqua Water Technologies Llc Dispositif de sécurisation de membrane
AU2013231145B2 (en) 2012-09-26 2017-08-17 Evoqua Water Technologies Llc Membrane potting methods
AU2013323934A1 (en) 2012-09-27 2015-02-26 Evoqua Water Technologies Llc Gas scouring apparatus for immersed membranes
WO2015050764A1 (fr) 2013-10-02 2015-04-09 Evoqua Water Technologies Llc Procédé et dispositif de réparation de module de filtration sur membrane
AU2016294153B2 (en) 2015-07-14 2022-01-20 Evoqua Water Technologies Llc Aeration device for filtration system
US9782718B1 (en) 2016-11-16 2017-10-10 Membrane Technology And Research, Inc. Integrated gas separation-turbine CO2 capture processes
CN116447012A (zh) * 2023-03-10 2023-07-18 广西大学 一种基于热流逸效应的新型开式燃气轮机装置

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0882486A1 (fr) * 1997-06-05 1998-12-09 Praxair Technology, Inc. Procédé pour la combustion enrichie utilisant des systèmes avec une membrane solide électrolytique
WO1998055208A1 (fr) * 1997-06-06 1998-12-10 Norsk Hydro Asa Procede servant a produire de l'energie et comprenant un processus de combustion
WO2000033942A1 (fr) * 1998-12-04 2000-06-15 Norsk Hydro Asa Procede de recuperation de co¿2?
EP1040861A1 (fr) * 1999-03-29 2000-10-04 Praxair Technology, Inc. Procédé pour la combustion enrichie utilisant des systèmes avec une membrane solide électrolitique

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2020416A1 (de) * 1970-04-27 1971-11-11 Motoren Turbinen Union Brennkammer fuer Gasturbinentriebwerke
US4787919A (en) * 1987-06-23 1988-11-29 Union Carbide Corporation Membrane separation system and process
SE462446B (sv) * 1989-06-29 1990-06-25 Abb Stal Ab Foerraadsbehaallare foer baeddmaterial vid en kraftanlaeggning med braennkammare foer fluidiserad baedd
US5954859A (en) * 1997-11-18 1999-09-21 Praxair Technology, Inc. Solid electrolyte ionic conductor oxygen production with power generation
US6048472A (en) * 1997-12-23 2000-04-11 Air Products And Chemicals, Inc. Production of synthesis gas by mixed conducting membranes
US6537514B1 (en) * 1999-10-26 2003-03-25 Praxair Technology, Inc. Method and apparatus for producing carbon dioxide

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0882486A1 (fr) * 1997-06-05 1998-12-09 Praxair Technology, Inc. Procédé pour la combustion enrichie utilisant des systèmes avec une membrane solide électrolytique
WO1998055208A1 (fr) * 1997-06-06 1998-12-10 Norsk Hydro Asa Procede servant a produire de l'energie et comprenant un processus de combustion
WO2000033942A1 (fr) * 1998-12-04 2000-06-15 Norsk Hydro Asa Procede de recuperation de co¿2?
EP1040861A1 (fr) * 1999-03-29 2000-10-04 Praxair Technology, Inc. Procédé pour la combustion enrichie utilisant des systèmes avec une membrane solide électrolitique

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004065770A1 (fr) * 2003-01-20 2004-08-05 Alstom Power Sweden Ab Regulation d'une turbine a gaz au moyen d'un reacteur generant de l'air chaud
US20140231588A1 (en) * 2004-11-23 2014-08-21 Biosphere Aerospace, Llc Method and system for loading and unloading cargo assembly onto and from an aircraft
US9108720B2 (en) * 2004-11-23 2015-08-18 Biosphere Aerospace, Llc Method and system for loading and unloading cargo assembly onto and from an aircraft
WO2008087150A1 (fr) * 2007-01-19 2008-07-24 Siemens Aktiengesellschaft Installation de combustion
WO2009064539A3 (fr) * 2007-11-14 2010-04-15 Alstom Technology Ltd Chaudière et dispositif de production d'oxygène intégré
US7954458B2 (en) 2007-11-14 2011-06-07 Alstom Technology Ltd Boiler having an integrated oxygen producing device

Also Published As

Publication number Publication date
NO20006690L (no) 2002-07-01
JP2004533594A (ja) 2004-11-04
EP1356233A1 (fr) 2003-10-29
NO20006690D0 (no) 2000-12-29
NO318619B1 (no) 2005-04-18
US20050053878A1 (en) 2005-03-10

Similar Documents

Publication Publication Date Title
US20050053878A1 (en) Device for combustion of a carbon containing fuel in a nitrogen free atmosphere and a method for operating said device
US6764784B2 (en) Standard package design for both atmospheric and pressurized SOFC power generation system
US7658788B2 (en) Ion transport membrane module and vessel system with directed internal gas flow
EP1146951B1 (fr) Procede de recuperation de co 2
US7217304B2 (en) Electric power generation with heat exchanged membrane reactor
US5573867A (en) Purge gas protected transportable pressurized fuel cell modules and their operation in a power plant
US7703271B2 (en) Cogeneration method and device using a gas turbine comprising a post-combustion chamber
US7160357B2 (en) Oxygen transport membrane reactor and method
JP4842805B2 (ja) マルチチャネルモノリシック構造のチャネルに出入りするよう２つの流体を分配する方法及び装置、並びにそれらの使用
CA2080257A1 (fr) Pile a combustible a oxyde solide
CA2202767A1 (fr) Perfectionnements concernant la combustion et l'utilisation des gaz combustibles
CA2432745A1 (fr) Dispositif et procede pour la separation et la combustion de l'oxygene
RU2661581C2 (ru) Система и способ регулирования температуры в реакторе на основе кислородпроводящих мембран
US9803512B2 (en) Reactor system and solid fuel composite therefor
US20190203643A1 (en) Systems and methods for power production including ion transport components
EP2300129B1 (fr) Centrale électrique thermique avec séquestration du co2
US9725662B2 (en) Method and membrane module for the energy-efficient oxygen generation during biomass gasification
WO2001079754A1 (fr) Procede de generation de chaleur et d'energie et utilisation de ces dernieres
US20070175411A1 (en) Oxygen-producing oxycombustion boiler
Griffin et al. Advanced zero emissions gas turbine power plant
CN115367704B (zh) 一种撬装式甲醇重整制氢提纯设备及其制氢提纯方法
KR20240007129A (ko) 공기 존재 하에 수소의 연소에 의해 질소(n2)와 수소(h2)를 포함하는 가스를 생성하기 위한 프로세스 및 시스템
MXPA98003329A (en) Separator-integrated conductor cooler ionicode electrolito sol
ITGE940117A1 (it) Turbina a gas ad accensione indiretta.

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NO NZ PL PT RO RU SD SE SG SI SK SL TJ TM TR TT TZ UA UG US UZ VN YU ZA ZW

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): GH GM KE LS MW MZ SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG

DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
121 Ep: the epo has been informed by wipo that ep was designated in this application
WWE Wipo information: entry into national phase

Ref document number: 2002554435

Country of ref document: JP

WWE Wipo information: entry into national phase

Ref document number: 2001985460

Country of ref document: EP

WWP Wipo information: published in national office

Ref document number: 2001985460

Country of ref document: EP

REG Reference to national code

Ref country code: DE

Ref legal event code: 8642

WWE Wipo information: entry into national phase

Ref document number: 10451729

Country of ref document: US

WWR Wipo information: refused in national office

Ref document number: 2001985460

Country of ref document: EP

WWW Wipo information: withdrawn in national office

Ref document number: 2001985460

Country of ref document: EP