EP2014984A1 - Utilisation de matières inertes destinées à la protection de composants d'une chambre de combustion et de composants de brûleur - Google Patents

Utilisation de matières inertes destinées à la protection de composants d'une chambre de combustion et de composants de brûleur Download PDF

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Publication number
EP2014984A1
EP2014984A1 EP07013410A EP07013410A EP2014984A1 EP 2014984 A1 EP2014984 A1 EP 2014984A1 EP 07013410 A EP07013410 A EP 07013410A EP 07013410 A EP07013410 A EP 07013410A EP 2014984 A1 EP2014984 A1 EP 2014984A1
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EP
European Patent Office
Prior art keywords
combustion chamber
components
inert gas
protected
burner
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.)
Withdrawn
Application number
EP07013410A
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German (de)
English (en)
Inventor
Malte Dr. Blomeyer
Olga Deiss
Andre Kluge
Thomas Kunadt
Berthold Köstlin
Martin Lenze
Paul Pixner
Uwe Sieber
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.)
Siemens AG
Original Assignee
Siemens AG
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
Application filed by Siemens AG filed Critical Siemens AG
Priority to EP07013410A priority Critical patent/EP2014984A1/fr
Priority to PCT/EP2008/058817 priority patent/WO2009007356A1/fr
Publication of EP2014984A1 publication Critical patent/EP2014984A1/fr
Withdrawn legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • F23M5/08—Cooling thereof; Tube walls
    • F23M5/085—Cooling thereof; Tube walls using air or other gas as the cooling medium
    • 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
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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
    • F23L2900/07002—Injecting inert gas, other than steam or evaporated water, into the combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M2900/00—Special features of, or arrangements for combustion chambers
    • F23M2900/05001—Preventing corrosion by using special lining materials or other techniques
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03042—Film cooled combustion chamber walls or domes

Definitions

  • components are exposed to direct contact with a flame. This applies in particular to burner and combustion chamber components of a gas turbine. Although the direct contact of the burner or combustion chamber components with the flame should ideally not occur, it can not be avoided, for example, when a flashback occurs. In direct contact of the flame with burner components or combustion chamber surfaces, the materials of the burner are exposed to such high thermal loads that the material can be damaged.
  • hitherto high-temperature resistant materials such as Hastelloy X
  • Hastelloy X are used.
  • these materials provide a longer shelf life of the burner components, but provide no protection against temperatures of up to 1,400 ° C.
  • ceramic coatings and air-film cooling are used. In the latter case, a boundary layer is created by air inflow, in which the fuel-air mixture is diluted so much that the fuel content is below the ignition limit and thus the risk of spreading of the flame is reduced to the burner or combustion chamber components.
  • the inventive method for protecting a surface from contact with a flame is characterized in that the surface to be protected is coated with an inert gas.
  • the surface to be protected may be the surface of a burner component or of a combustion chamber component of a gas turbine. Above all, the combustion chamber wall of a gas turbine can be effectively protected with the present method.
  • An interte gas is a gas which is very inert, meaning that it only takes part in a few chemical reactions.
  • the inert gas used in the present process may be, for example, water vapor, nitrogen, carbon dioxide or a noble gas such as helium, argon, neon, krypton, radon or xenon.
  • the inert gas used in the context of the present invention may also be a mixture of the gases mentioned.
  • Advantageous is the use of nitrogen or carbon dioxide, since their use is associated with the least cost.
  • the surface to be protected may be coated with the inert gas such that the inert gas is directed onto the surface through openings located in the surface to be protected.
  • the openings may be bores which extend at right angles to the surface to be protected or, in particular, at an angle thereto, at an angle to the latter.
  • the inert gas in the direction of flow of this fluid along the surface to be protected. This can be done in particular by openings in the form of obliquely arranged to the surface holes.
  • the fluid may be, for example, fuel or a Act fuel-air mixture.
  • the fuel can be hydrogen.
  • a flow direction is predetermined by the fuel injected into it or by a fuel-air mixture injected into it. It is therefore useful to protect the surface of the combustion chamber wall against direct contact with the burner flame in such a way that the inert gas is injected into the combustion chamber along the surface of the combustion chamber wall in the direction of this flow direction.
  • possibly existing film cooling holes can be used as injection openings.
  • the coating according to the invention of the endangered components or the endangered surfaces with a boundary layer of an inert gas means that oxygen is not present as oxidizer. It is also possible to burn hydrogen without the high risk of damage to the components, in particular by possible flashbacks. This is caused by the fact that the flame does not reach the components, in particular the combustion chamber wall, due to the inert gas boundary layer. An air film cooling is due to the large ignition range of hydrogen not suitable for this purpose. Another advantage of the present invention is that it reduces the thermal stress on the components and thus extends their life.
  • FIG. 1 schematically shows a section through a part of a combustion chamber wall or a burner wall of a gas turbine.
  • FIG. 1 schematically shows a Section through a part of a combustion chamber wall or burner wall 1 of a gas turbine.
  • a fuel-air mixture 2 Inside the combustion chamber is a fuel-air mixture 2.
  • the flow direction of this fuel-air mixture 2 is indicated by an arrow 3.
  • the directed to the inside of the combustion chamber surface 7 of the combustion chamber wall 1 has an opening 6 which extends obliquely to the surface 7.
  • an inert gas 4 is passed into the interior of the combustion chamber.
  • the flow direction of the inert gas 4 is indicated by arrows 5.
  • an interface 8 is formed between the inert gas 4 introduced into the combustion chamber and the fuel-air mixture 2 located in the combustion chamber.
  • the fuel-air mixture 2 is burned via one or more flames.
  • a direct contact of the flame with the surface 7 of the combustion chamber wall 1 should be avoided.
  • an inert gas 4 is introduced into the combustion chamber via the opening 6, which is located in the combustion chamber wall 1.
  • the flow direction 3 of the fuel-air mixture 2 causes the inert gas 4 to flow parallel to the flow direction 3 along the surface 7, thereby covering the surface 7 with a protective layer. Since the inert gas 4 is very inert and in particular contains no oxidizer such as oxygen, the flame in the combustion chamber can not reach the surface 7.
  • the opening 6 may be, for example, a film cooling hole.
  • the opening can be like in FIG. 1 shown obliquely to the surface 7, but also perpendicular or at any other angle.
  • the inert gas 4 introduced into the combustion chamber through the opening 6 may be, for example, water vapor, nitrogen, carbon dioxide or a noble gas.
  • noble gases helium, argon, neon, krypton, radon or xenon are considered.
  • the presented in the present invention method provides effective protection of the surfaces of particular burner or combustion chamber components of a gas turbine against direct contact with a flame.
  • the resulting protection against high temperatures reduces the thermal load on the components and thus extends their service life.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
EP07013410A 2007-07-09 2007-07-09 Utilisation de matières inertes destinées à la protection de composants d'une chambre de combustion et de composants de brûleur Withdrawn EP2014984A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP07013410A EP2014984A1 (fr) 2007-07-09 2007-07-09 Utilisation de matières inertes destinées à la protection de composants d'une chambre de combustion et de composants de brûleur
PCT/EP2008/058817 WO2009007356A1 (fr) 2007-07-09 2008-07-08 Utilisation de substances inertes pour protéger des composants d'une chambre de combustion et des composants d'un brûleur

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP07013410A EP2014984A1 (fr) 2007-07-09 2007-07-09 Utilisation de matières inertes destinées à la protection de composants d'une chambre de combustion et de composants de brûleur

Publications (1)

Publication Number Publication Date
EP2014984A1 true EP2014984A1 (fr) 2009-01-14

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EP07013410A Withdrawn EP2014984A1 (fr) 2007-07-09 2007-07-09 Utilisation de matières inertes destinées à la protection de composants d'une chambre de combustion et de composants de brûleur

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EP (1) EP2014984A1 (fr)
WO (1) WO2009007356A1 (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010099452A3 (fr) * 2009-02-26 2011-07-21 Palmer Labs, Llc Appareil et procédé de combustion d'un combustible à haute pression et haute température, et système et dispositif associés
WO2012030820A3 (fr) * 2010-08-31 2013-04-04 Palmer Labs, Llc Appareil permettant de brûler un combustible à haute pression et haute température, et système associé
US9068743B2 (en) 2009-02-26 2015-06-30 8 Rivers Capital, LLC & Palmer Labs, LLC Apparatus for combusting a fuel at high pressure and high temperature, and associated system
US10859264B2 (en) 2017-03-07 2020-12-08 8 Rivers Capital, Llc System and method for combustion of non-gaseous fuels and derivatives thereof
US11199327B2 (en) 2017-03-07 2021-12-14 8 Rivers Capital, Llc Systems and methods for operation of a flexible fuel combustor
US11572828B2 (en) 2018-07-23 2023-02-07 8 Rivers Capital, Llc Systems and methods for power generation with flameless combustion

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8869889B2 (en) 2010-09-21 2014-10-28 Palmer Labs, Llc Method of using carbon dioxide in recovery of formation deposits

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB932980A (en) * 1960-08-27 1963-07-31 Ludwig Bolkow Combustion chambers for liquid fuels
GB2256470A (en) * 1991-06-03 1992-12-09 Mitsubishi Heavy Ind Ltd Preventing dust adhesion in a furnace
WO2004072443A1 (fr) * 2003-02-11 2004-08-26 Statoil Asa Centrale electrique a turbines a gaz a cycle combine comportant une interception de co2 et un systeme de chambre de combustion a flux separes
WO2005108864A1 (fr) * 2004-05-05 2005-11-17 Hitachi Power Europe Gmbh Chaudiere et son mode de fonctionnement
WO2008023986A1 (fr) * 2006-06-20 2008-02-28 Statoil Asa Procédé pour améliorer l'efficacité énergétique et économique d'une centrale de production d'énergie a gaz, centrale de production d'énergie thermique et brûleur destine a être utilise dans ces centrales

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB932980A (en) * 1960-08-27 1963-07-31 Ludwig Bolkow Combustion chambers for liquid fuels
GB2256470A (en) * 1991-06-03 1992-12-09 Mitsubishi Heavy Ind Ltd Preventing dust adhesion in a furnace
WO2004072443A1 (fr) * 2003-02-11 2004-08-26 Statoil Asa Centrale electrique a turbines a gaz a cycle combine comportant une interception de co2 et un systeme de chambre de combustion a flux separes
WO2005108864A1 (fr) * 2004-05-05 2005-11-17 Hitachi Power Europe Gmbh Chaudiere et son mode de fonctionnement
WO2008023986A1 (fr) * 2006-06-20 2008-02-28 Statoil Asa Procédé pour améliorer l'efficacité énergétique et économique d'une centrale de production d'énergie a gaz, centrale de production d'énergie thermique et brûleur destine a être utilise dans ces centrales

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9068743B2 (en) 2009-02-26 2015-06-30 8 Rivers Capital, LLC & Palmer Labs, LLC Apparatus for combusting a fuel at high pressure and high temperature, and associated system
EA024852B1 (ru) * 2009-02-26 2016-10-31 Палмер Лэбз, Ллк Способ и устройство для сжигания топлива при высокой температуре и высоком давлении и соответствующие система и средства
US9416728B2 (en) 2009-02-26 2016-08-16 8 Rivers Capital, Llc Apparatus and method for combusting a fuel at high pressure and high temperature, and associated system and device
WO2010099452A3 (fr) * 2009-02-26 2011-07-21 Palmer Labs, Llc Appareil et procédé de combustion d'un combustible à haute pression et haute température, et système et dispositif associés
KR20130099078A (ko) * 2010-08-31 2013-09-05 팔머 랩스, 엘엘씨 고온 및 고압에서 연료를 연소하는 장치 및 이에 관련된 시스템
CN103201562B (zh) * 2010-08-31 2016-02-10 帕尔默实验室有限责任公司 在高压高温下燃烧燃料的设备及相关系统
CN103201562A (zh) * 2010-08-31 2013-07-10 帕尔默实验室有限责任公司 在高压高温下燃烧燃料的设备及相关系统
WO2012030820A3 (fr) * 2010-08-31 2013-04-04 Palmer Labs, Llc Appareil permettant de brûler un combustible à haute pression et haute température, et système associé
EA029299B1 (ru) * 2010-08-31 2018-03-30 Палмер Лэбс, Ллк Установка для сжигания топлива при высокой температуре и высоком давлении
KR101906330B1 (ko) 2010-08-31 2018-10-10 팔머 랩스, 엘엘씨 고온 및 고압에서 연료를 연소하는 장치 및 이에 관련된 시스템
US10859264B2 (en) 2017-03-07 2020-12-08 8 Rivers Capital, Llc System and method for combustion of non-gaseous fuels and derivatives thereof
US11199327B2 (en) 2017-03-07 2021-12-14 8 Rivers Capital, Llc Systems and methods for operation of a flexible fuel combustor
US11435077B2 (en) 2017-03-07 2022-09-06 8 Rivers Capital, Llc System and method for combustion of non-gaseous fuels and derivatives thereof
US11828468B2 (en) 2017-03-07 2023-11-28 8 Rivers Capital, Llc Systems and methods for operation of a flexible fuel combustor
US11572828B2 (en) 2018-07-23 2023-02-07 8 Rivers Capital, Llc Systems and methods for power generation with flameless combustion

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WO2009007356A1 (fr) 2009-01-15

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