EP0925470B1 - Vorrichtung und verfahren zur verbrennung eines brennstoffs in luft - Google Patents
Vorrichtung und verfahren zur verbrennung eines brennstoffs in luft Download PDFInfo
- Publication number
- EP0925470B1 EP0925470B1 EP97918906A EP97918906A EP0925470B1 EP 0925470 B1 EP0925470 B1 EP 0925470B1 EP 97918906 A EP97918906 A EP 97918906A EP 97918906 A EP97918906 A EP 97918906A EP 0925470 B1 EP0925470 B1 EP 0925470B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- axis
- fuel
- air
- flow
- 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.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/02—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
-
- 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
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
- F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
-
- 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
- F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
- F23C2900/07001—Air swirling vanes incorporating fuel injectors
Definitions
- the invention also relates to a method for combustion a fuel in air, in which the air in one Axis encircling, meridional with respect to the axis and provided with a swirl continuing current and essentially is homogeneously mixed with fuel to form of a mixture used to burn the fuel is ignited.
- Such a device is known as a "premix burner" known to the relevant migrant and active persons, the name already indicates that the Fuel only after a certain time interval its interference in that provided for combustion Air is burned.
- the procedure is also relevant migrant and active people known as the process which is when operating a conventional premix burner expires.
- combustion vibrations When operating a conventional premix burner, increasing the supply of fuel to the burner is often a condition reached at which the combustion becomes unstable and in the system in which it is installed, acoustic vibrations evokes. These acoustic vibrations are below that
- the term "combustion vibrations" is known.
- the combustion vibrations can become so strong that they stop the operation of the Premix burner and the system, the component of which is the premix burner is endanger.
- the slope of a premix burner the formation of an unstable combustion becomes all the more so stronger, the more homogeneous that in the premix burner before combustion formed mixture of fuel and air.
- a mixture that is as homogeneous as possible is desirable in view insist that the production of nitrogen oxides during combustion the lower the more homogeneous the mixture. If the mixture is completely homogeneous, it takes on combustion maximum temperature of the mixture Minimum, and it is exactly this effect that is for the then particularly low production of nitrogen oxides essential is.
- Such a device and such a method are also known from EP 0 193 838 B1 or EP 0 589 520 B1.
- the invention has for its object a measure for Stabilization of the combustion process in a premix burner to indicate where it is not necessary to provide the Part of the combustion process available To withdraw air. This measure is intended both in one device as well as being embodied in a process.
- the distribution of speed in the stream as it exits the device unevenly designed in a radial direction with respect to the axis, but the homogeneity of the mixture of air and Maintain fuel in the stream.
- the unevenness in the distribution of speed in the stream can do so the meridional component of speed, the tangential Component of speed or both components the speed concern. This is done in that the Current in the ring channel is disturbed locally by means of an appropriate one Obstacle in the form of a sieve or the like, which is arranged at a corresponding point in the ring channel becomes.
- the premix burner embodied as such in the individual case stabilization by a so-called pilot flame needs, as is known from the cited prior art, and whether this pilot flame in the center or on the outer circumference of the stream is arranged, or whether the premix burner does not need a pilot flame at all, in the present case it is of minor importance Importance.
- fuel is of minor importance; basically the supply of fuel in any In this way, for example, via nozzles in guide vanes of the swirl grille or separate mixing devices in front of or behind the swirl grill.
- the means for decelerating the radially outer axis Part of the flow versus other parts of the Strom creates a local pressure drop in the stream, which causes a lower flow rate behind the agent prevails as in those unaffected by the agent Sharing the electricity. It is understood that the means of Mixing the fuel into the stream for the required Homogeneity of the mixture produced must be designed; it may be necessary to add fuel to the delayed part of the electricity compared to the supply to the reduce other parts of the current accordingly.
- a first particularly preferred further development of the device is characterized in that the intended means for decelerating one radially outside with respect to the axis part of the current lying circularly symmetrical with respect to the axis is so that the part of the Stroms is also circularly symmetrical with respect to the axis.
- the entire stream is thus enveloped by one opposite other parts significantly slowed down part.
- This slowed Part is therefore decisive for the aerodynamic conditions at an interface between that from the device leaked electricity and fuel-free air, which is due to a reduced speed gradient due to the delay to suppress vortex formation and thus for acoustic stabilization of one in the Electricity-induced combustion leads.
- the circular symmetrical means for deceleration is preferred one arranged in the ring channel and one with respect to the Radially outer part of the ring channel overlapping Throttle ring, which is particularly upstream of the Swirl grid is arranged.
- This throttle ring is still preferably arranged in the ring channel and around Axle evenly distributed throttle elements, in particular Rods, formed.
- the throttle ring is said to be the part of the Not completely covering the ring channel that he is handing over, but only throttle the flow through this part. In any case, the throttle ring is therefore as functional as a Sieve to be designed.
- the device is characterized in that the means for Delay with respect to the axis broken symmetrically, in particular is designed discreetly symmetrical.
- the means for Delay with respect to the axis broken symmetrically in particular is designed discreetly symmetrical.
- Under one broken symmetrical arrangement becomes an arrangement understood that of a circular symmetrical arrangement essential is different and is particularly characterized by that they have no (continuous) circular symmetry, but at most a discrete symmetry, e.g. described by a finite symmetry group.
- This broken So symmetrical means does not cause the current is enveloped by the total and evenly delayed Part, as is particularly the case with the first described above preferred further development results.
- the current has strands in an outside area, that are delayed compared to other parts of the stream.
- This slow strands are also apt to form Whirl the current after it exits the device could envelop prevent.
- the slow ones Strands form local disturbances in the speed field of the current, which counteract the formation of eddies and thus to the desired acoustic stabilization of a flame generated in the stream, such as already described.
- the fractionally symmetrical means of deceleration is preferred an arrangement of unevenly distributed around the axis Throttle elements, in particular rods.
- the means for mixing in the fuel is preferred an array of nozzles, the nozzles in the swirl grille can be arranged, in particular such that the nozzles are located in the guide vanes of the swirl grille.
- the object is achieved according to the invention specified a method of burning a Fuel in air, in which the air in an axis surrounding meridional with one axis Swirl continued current provided and essentially is homogeneously mixed with fuel to form a mixture, which is ignited to burn the fuel, where before the ignition a radially outside with respect to the axis Part of the current versus other parts of the Electricity is delayed.
- the delay of the radially outer part of the stream can be circularly symmetrical with respect to the axis respectively; alternatively, it is possible to delay in one to perform a broken symmetrical manner with respect to the axis. Details can be found in the above explanations to the two particularly preferred further developments the device according to the invention, to which hereby is referred.
- the drawing is not to be regarded as a concrete representation realized exemplary embodiments and is simplified to Highlighting certain features.
- the one from the drawing immediately Removable notes are for practical execution can be completed within the framework of knowledge and skills, the relevant migrant and active persons bids are taking into account this notice previous statements.
- Figure 1 shows an embodiment of the device according to of the invention
- Figure 2 shows an embodiment for comparison as defined in the introduction to this Text of the proposed proposal.
- Many components are in both embodiments available, and to explain this Components are first common to Figure 1 and Figure 2 Referred.
- Figure 1 and Figure 2 each show a premix burner an axis 1, one arranged centrally with respect to axis 1 Inner body 2 and also centrally with respect the axis 1 arranged, the inner body 2 surrounding outer body 3. Between the inner body 2 and the outer body 3 there is an annular channel 4 through which a stream 5 of air is passed becomes. The air is mixed with fuel 6 in the ring channel 4 to form a mixture which is in the combustion chamber 7 flows in and burns there.
- An ignition device for ignition the mixture is not shown for the sake of clarity. As part of normal practice for a combustion chamber 7 prefers several premix burners, is not required about an ignition device for each burner, but it can a single ignition device is sufficient for all burners.
- an ignition device is therefore not a component of a single premix burner, which also justifies that an ignition device is not shown in the figures is.
- the premix burner is embedded in a Combustion chamber wall 8, which the combustion chamber 7 upstream of the Current 5 completes.
- A is arranged in the ring channel 4 Swirl grille 9 consisting of guide vanes 9, which serves to impart a swirl 10 to the current 5.
- nozzles 11 and 12 are for the sake of clarity not shown.
- pilot burner may be required if the premix burner is below changing mixing ratios of air and fuel should be operated as a mixture which is comparatively is low in fuel, possibly without support can no longer ignite reliably.
- FIG. An exemplary embodiment of the invention is shown in FIG.
- a throttle ring 13 made of individual, attached to the outer body 3 and provided in the annular channel 4 rods. These rods cause local pressure drops in the Stream 5 and cause the outside part of the stream 5, which passes close to the outer body 3, opposite other parts of the stream 5 slowed down or delayed becomes. This slowdown continues throughout Ring channel 4 and causes the distribution of speed in the mixture that flows into the combustion chamber 7, is uneven. This has already been described in detail stabilizing effects on those in the combustion chamber 7 combustion taking place, on the above explanation is hereby referred.
- the fuel supply 6 to the stream 5 must be of uneven distribution take into account the speed in the stream 5; therefore are to supply the fuel to the largely unaffected Part of the stream large nozzles 11 and for feeding the Fuel 6 to the slowed down part of the stream 5 small Nozzles 12 are provided.
- the dimensions of these nozzles 11 and 12 should be chosen so that a largely homogeneous distribution of the fuel in the stream and thus combustion guaranteed with the lowest possible production of nitrogen oxides is.
- the relevant migrant and active persons Computer programs are available for the appropriate design of the device for numerical modeling of the current 5 for Available, using their corresponding interpretation the nozzles 11 and 12 is possible.
- Figure 2 shows a device in which the ring channel 4 is free of throttling internals. Accordingly, it requires Supply of the fuel 6 also none of different sizes Nozzles; only large nozzles 11 are provided.
- an annular nozzle 14 surrounding the outer body 3 is provided which a part of the air supplied to the device on the Ring channel 4 and the swirl grille 9 over directly into the combustion chamber 7 is performed. This air forms a veil, which the mixture of air and fuel envelops and formation of vortices that make combustion unstable could be prevented.
- a disadvantage of the embodiment according to Figure 2 is the requirement that part of the available air is not available for mixing with fuel stands. Ultimately, this means that the device in increased nitrogen oxides must produce, which in any case is undesirable.
- Figure 3 shows a partial view of an axial longitudinal section by a variant of the device according to Figure 1. Many components this device match the components 1 and therefore do not need to be described again. Of importance in Figure 3 is that for the supply of fuel 6 no longer the guide vanes 9 are used, but that separate nozzle tubes 15 are provided, which nozzles 16 for supplying the fuel 6 carry to the stream 5. Means for feeding the Fuel to the nozzle pipes 15 are for the sake of clarity again not shown. The nozzles 16 do not all have to be equal to each other; see the explanations to the nozzles 11 and 12 in FIG. 1.
- FIG. 4 shows a cross section through a preferred further development, where several alternatives for the means of Delays in part of the current can be seen. Except the rods 13 already mentioned, these are a perforated plate 17 and a wire 18 or the like fabric 18 (where the actual tissue is only partially shown). Under The guide vanes are visible to these means 13, 17 and 18 9, which is between the inner body 2 and the outer body 3 extend.
- the embodiment shown in Figure 4 is from Meaning that the deceleration of the radially outside Part of the stream 5 (see FIG. 1) in one respect axis 1 is circularly symmetrical. The one from the The device released according to FIG. 4 thus has a radial outer part, which is even compared to others Sharing the stream 5 is delayed.
- the with it and through it achievable effects are already detailed above has been explained, to which reference is hereby made.
- perforated plates 17 and sieves 18 is the number and geometry of the rods 13 based on the aerodynamic To choose conditions of the device to be realized; corresponding knowledge and resources are relevant migrant and active people at command.
- Figure 5 shows a cross section through a second preferred Further development, in contrast to the means of delay to the embodiment of Figure 4 with respect to Axis 1 is not circularly symmetrical, but broken symmetrical is executed.
- the arrangement of the rods 13 according to Figure 5 is intended to show irregularities in the Stream 5 generated, which is far behind the rods 13 and continue the swirl grille 9 and also after the exit the device is still present. After leaving the Accordingly, the device is effectively in the stream 5 uneven speed field, which also the formation of vortices that could surround stream 5, suppressed and thus to the desired acoustic stabilization a flame generated in the stream 5 can serve.
- All embodiments of the invention are of particular importance for use in a gas turbine to get one of compressed air flow provided to a compressor by heating a fuel, whereupon the heated electricity is relaxed in a turbine.
- Excellent is the invention in particular in that it on the one hand only passive measures to stabilize one Incineration and on the other hand no branching off Air from the air that is otherwise used for combustion is available requires.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Air Supply (AREA)
- Gas Burners (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
Abstract
Description
- FIG 1
- einen Längsschnitt durch eine Ausführungsform eines Vormischbrenners;
- FIG 2
- einen Längsschnitt durch einen Vormischbrenner des Standes der Technik;
- FIG 3, 4 und 5
- Ansichten von Ausführungsformen des Vormischbrenners.
Claims (14)
- Vorrichtung zur Verbrennung eines Brennstoffs (6) in Luft, umfassend:einen Ringkanal (4) zur Führung der Luft in einem bezüglich einer Achse '1) meridionalen Strom (5);ein Drallgitter (9) zur Aufprägung eines Dralls (10) auf den Strom (5); undein Mittel (11,12,16) zur Einmischung des Brennstoffs (6) in den Strom (5) unter Bildung eines im wesentlichen homogenen Gemischs;
- Vorrichtung nach Anspruch 1, bei der das Mittel (13, 17, 18) zur Verzögerung bezüglich der Achse (1) kreissymmetrisch ist.
- Vorrichtung nach Anspruch 2, bei der das Mittel (13, 17, 18) zur Verzögerung ein in dem Ringkanal (4) angeordneter und einen bezüglich der Achse (1) radial außenliegenden Teil des Ringkanals (4) überreichender Drosselring (13,17,18) ist.
- Vorrichtung nach Anspruch 3, bei der der Drosselring (13,17,18) stromaufwärts des Drallgitters (9) angeordnet ist.
- Vorricntung nach Anspruch 4, bei der der Drosselring (13, 17, 18) gebildet ist aus gleichmäßig verteilten Drosselelementen (13, 17, 18).
- Vorrichtung nach einem der Ansprüche 3 bis 5, bei der der Drosselring (13,17,18) aus in dem Ringkanal (4) angeordneten Stäben (13) gebildet ist.
- Vorrichtung nach Anspruch 1, bei der das Mittel (13, 17, 18) zur Verzögerung bezüglich der Achse (1) gebrochen symmetrisch, insbesondere diskret symmetrisch, ist.
- Vorrichtung nach Anspruch 7, bei der das Mittel (13, 17, 18) gebildet ist aus ungleichmäßig um die Achse (1) verteilten Drosselelementen (13, 17, 18), insbesondere Stäben (13).
- Vorrichtung nach einem der vorhergehenden Ansprüchen, bei der das Mittel (11, 12) zur Einmischung des Brennstoffs (6) eine Anordnung von Düsen (11, 12, 16) umfaßt.
- Vorrichtung nach Anspruch 9, bei der die Düsen (11, 12) in dem Drallgitter (9) angeordnet sind.
- Vorrichtung nach Anspruch 9, bei der die Düsen (11, 12) in Leitschaufeln (9) des Drallgitters (9) angeordnet sind.
- Verfahren zur Verbrennung eines Brennstoffs (6) in Luft, bei dem die Luft in einem eine Achse (1) umringenden, sich bezüglich der Achse (1) meridional und mit einem Drall (10) fortsetzenden Strom (5) bereitgestellt und im wesentlichen homogen mit Brennstoff (6) vermischt wird unter Bildung eines Gemisches, das zur Verbrennung des Brennstoffs (6) entzündet wird, dadurch gekennzeichnet, daß vor der Entzündung ein bezüglich der Achse (1) radial außenliegender Teil des Stroms (5) gegenüber anderen Teilen des Stroms (5) verzögert wird.
- Verfahren nach Anspruch 12, bei dem der radial außenliegende Teil des Stroms (5) bezüglich der Achse (1) kreissymmetrisch ist.
- Verfahren nach Anspruch 12, bei dem der radial außenliegende Teil des Stroms (5) bezüglich der Achse (1) gebrochen symmetrisch ist.
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19636556 | 1996-09-09 | ||
DE19636556 | 1996-09-09 | ||
DE19640818 | 1996-10-02 | ||
DE1996140818 DE19640818B4 (de) | 1996-10-02 | 1996-10-02 | Vorrichtung und Verfahren zur Verbrennung eines Brennstoffs in Luft |
PCT/DE1997/001852 WO1998011383A2 (de) | 1996-09-09 | 1997-08-26 | Vorrichtung und verfahren zur verbrennung eines brennstoffs in luft |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0925470A2 EP0925470A2 (de) | 1999-06-30 |
EP0925470B1 true EP0925470B1 (de) | 2000-03-08 |
EP0925470A3 EP0925470A3 (de) | 2002-11-27 |
Family
ID=26029190
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97918906A Expired - Lifetime EP0925470B1 (de) | 1996-09-09 | 1997-08-26 | Vorrichtung und verfahren zur verbrennung eines brennstoffs in luft |
Country Status (6)
Country | Link |
---|---|
US (1) | US6152724A (de) |
EP (1) | EP0925470B1 (de) |
JP (1) | JP4130475B2 (de) |
DE (1) | DE59701235D1 (de) |
RU (1) | RU2190804C2 (de) |
WO (1) | WO1998011383A2 (de) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2002095293A1 (en) | 2001-05-18 | 2002-11-28 | Siemens Aktiengesellschaft | Burner apparatus for burning fuel and air |
EP1400752A1 (de) | 2002-09-20 | 2004-03-24 | Siemens Aktiengesellschaft | Vormischbrenner mit profilierter Luftmassenströmung |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0936406B1 (de) * | 1998-02-10 | 2004-05-06 | General Electric Company | Brenner mit gleichmässiger Brennstoff/Luft Vormischung zur emissionsarmen Verbrennung |
EP1048898B1 (de) | 1998-11-18 | 2004-01-14 | ALSTOM (Switzerland) Ltd | Brenner |
US6363724B1 (en) | 2000-08-31 | 2002-04-02 | General Electric Company | Gas only nozzle fuel tip |
JP4508474B2 (ja) * | 2001-06-07 | 2010-07-21 | 三菱重工業株式会社 | 燃焼器 |
EP1394471A1 (de) | 2002-09-02 | 2004-03-03 | Siemens Aktiengesellschaft | Brenner |
WO2004065763A2 (en) * | 2003-01-22 | 2004-08-05 | Vast Power Systems Inc. | Thermodynamic cycles using thermal diluent |
US20050056313A1 (en) * | 2003-09-12 | 2005-03-17 | Hagen David L. | Method and apparatus for mixing fluids |
EP1645805A1 (de) * | 2004-10-11 | 2006-04-12 | Siemens Aktiengesellschaft | Brenner für fluidische Brennstoffe und Verfahren zum Betreiben eines derartigen Brenners |
FR2902866B1 (fr) * | 2006-06-22 | 2008-10-10 | Giat Ind Sa | Generateur de gaz chaud et installtion de sechage ou deshydratation mettant en oeuvre un tel generateur |
EP2107313A1 (de) * | 2008-04-01 | 2009-10-07 | Siemens Aktiengesellschaft | Gestufte Brennstoffversorgung in einem Brenner |
EP2107300A1 (de) * | 2008-04-01 | 2009-10-07 | Siemens Aktiengesellschaft | Dralleinrichtung mit Gasinjektor |
US20120085834A1 (en) * | 2010-10-07 | 2012-04-12 | Abdul Rafey Khan | Flame Tolerant Primary Nozzle Design |
EP2848865A1 (de) * | 2013-09-12 | 2015-03-18 | Alstom Technology Ltd | Thermoakustisches Stabilisierungsverfahren |
IT201700061780A1 (it) * | 2017-06-06 | 2018-12-06 | Ansaldo Energia Spa | Gruppo bruciatore per una turbina a gas con generatori di turbolenze |
US11396888B1 (en) | 2017-11-09 | 2022-07-26 | Williams International Co., L.L.C. | System and method for guiding compressible gas flowing through a duct |
GB201806020D0 (en) * | 2018-02-23 | 2018-05-30 | Rolls Royce | Conduit |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1215443B (de) * | 1963-09-12 | 1966-04-28 | Daimler Benz Ag | Brennkammer, insbesondere fuer Gasturbinentriebwerke |
DE3663189D1 (en) | 1985-03-04 | 1989-06-08 | Siemens Ag | Burner disposition for combustion installations, especially for combustion chambers of gas turbine installations, and method for its operation |
JP3133066B2 (ja) * | 1991-04-25 | 2001-02-05 | シーメンス アクチエンゲゼルシヤフト | 石炭ガスおよび別の燃料を有害成分の発生を少なく燃焼するための特にガスタービン用のバーナ燃焼装置 |
IT1255613B (it) | 1992-09-24 | 1995-11-09 | Eniricerche Spa | Sistema di combustione a basse emissioni inquinanti per turbine a gas |
US5251447A (en) * | 1992-10-01 | 1993-10-12 | General Electric Company | Air fuel mixer for gas turbine combustor |
US5345768A (en) * | 1993-04-07 | 1994-09-13 | General Electric Company | Dual-fuel pre-mixing burner assembly |
US5487274A (en) * | 1993-05-03 | 1996-01-30 | General Electric Company | Screech suppressor for advanced low emissions gas turbine combustor |
DE4329971C2 (de) * | 1993-09-04 | 1998-11-26 | Johannes W Graat | Brennereinrichtung für einen gasartigen Brennstoff |
US5435126A (en) * | 1994-03-14 | 1995-07-25 | General Electric Company | Fuel nozzle for a turbine having dual capability for diffusion and premix combustion and methods of operation |
DE4415916A1 (de) * | 1994-05-05 | 1995-11-09 | Siemens Ag | Verfahren und Vorrichtung zur Verbrennung eines fließfähigen Brennstoffs |
US5471840A (en) * | 1994-07-05 | 1995-12-05 | General Electric Company | Bluffbody flameholders for low emission gas turbine combustors |
US5638682A (en) * | 1994-09-23 | 1997-06-17 | General Electric Company | Air fuel mixer for gas turbine combustor having slots at downstream end of mixing duct |
DE59608389D1 (de) * | 1995-09-22 | 2002-01-17 | Siemens Ag | Brenner, insbesondere für eine gasturbine |
-
1997
- 1997-08-26 EP EP97918906A patent/EP0925470B1/de not_active Expired - Lifetime
- 1997-08-26 RU RU99107024/06A patent/RU2190804C2/ru not_active IP Right Cessation
- 1997-08-26 JP JP51311798A patent/JP4130475B2/ja not_active Expired - Fee Related
- 1997-08-26 DE DE59701235T patent/DE59701235D1/de not_active Expired - Lifetime
- 1997-08-26 WO PCT/DE1997/001852 patent/WO1998011383A2/de active IP Right Grant
-
1999
- 1999-03-09 US US09/265,443 patent/US6152724A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2002095293A1 (en) | 2001-05-18 | 2002-11-28 | Siemens Aktiengesellschaft | Burner apparatus for burning fuel and air |
US7051530B2 (en) | 2001-05-18 | 2006-05-30 | Siemens Aktiengesellschaft | Burner apparatus for burning fuel and air |
EP1400752A1 (de) | 2002-09-20 | 2004-03-24 | Siemens Aktiengesellschaft | Vormischbrenner mit profilierter Luftmassenströmung |
Also Published As
Publication number | Publication date |
---|---|
WO1998011383A3 (de) | 2002-10-10 |
EP0925470A3 (de) | 2002-11-27 |
WO1998011383A2 (de) | 1998-03-19 |
DE59701235D1 (de) | 2000-04-13 |
US6152724A (en) | 2000-11-28 |
JP2002513458A (ja) | 2002-05-08 |
RU2190804C2 (ru) | 2002-10-10 |
EP0925470A2 (de) | 1999-06-30 |
JP4130475B2 (ja) | 2008-08-06 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0925470B1 (de) | Vorrichtung und verfahren zur verbrennung eines brennstoffs in luft | |
EP0571782B1 (de) | Verfahren zum Betrieb einer Brennkammer einer Gasturbine | |
DE69715256T2 (de) | Brennkammer | |
DE4426351B4 (de) | Brennkammer für eine Gasturbine | |
DE3217674C2 (de) | Brennkammer für eine Gasturbine | |
DE69220091T2 (de) | Vormischgasdüse | |
EP1654496B1 (de) | Brenner und verfahren zum betrieb einer gasturbine | |
EP0801268B1 (de) | Verfahren zum Betreiben einer Gasturbinenbrennkammer | |
DE19510744A1 (de) | Brennkammer mit Zweistufenverbrennung | |
EP2257736B1 (de) | Verfahren zum erzeugen von heissgas | |
EP0687860A2 (de) | Brennkammer mit Selbstzündung | |
DE4411622A1 (de) | Vormischbrenner | |
EP0623786A1 (de) | Brennkammer | |
DE3222347A1 (de) | Schwingbrenner mit vormischung | |
EP1182398A1 (de) | Verfahren zur Erhöhung der strömungsmechanischen Stabilität eines Vormischbrenners sowie Vormischbrenner zur Durchführung des Verfahrens | |
EP0718561A2 (de) | Brennkammer | |
DE4320212A1 (de) | Feuerungsanlage | |
WO1999004196A1 (de) | Brenneranordnung für eine feuerungsanlage, insbesondere eine gasturbinenbrennkammer | |
EP0394800B1 (de) | Vormischbrenner für die Heissgaserzeugung | |
DE19640818B4 (de) | Vorrichtung und Verfahren zur Verbrennung eines Brennstoffs in Luft | |
DE19537636A1 (de) | Verfahren zum Betrieb einer Kraftwerksanlage | |
EP0777082A2 (de) | Vormischbrenner | |
DE19737998A1 (de) | Brennervorrichtung | |
WO1998035184A1 (de) | Vorrichtung und verfahren zum verbrennen von brennstoff | |
DE19542644B4 (de) | Vormischverbrennung |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 19990305 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): CH DE FR GB IT LI |
|
GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
17Q | First examination report despatched |
Effective date: 19990804 |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): CH DE FR GB IT LI |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: NV Representative=s name: SIEMENS SCHWEIZ AG Ref country code: CH Ref legal event code: EP |
|
REF | Corresponds to: |
Ref document number: 59701235 Country of ref document: DE Date of ref document: 20000413 |
|
ET | Fr: translation filed | ||
ITF | It: translation for a ep patent filed | ||
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20000512 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
REG | Reference to a national code |
Ref country code: GB Ref legal event code: IF02 |
|
PUAK | Availability of information related to the publication of the international search report |
Free format text: ORIGINAL CODE: 0009015 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): CH DE FR GB IT LI |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PCAR Free format text: SIEMENS SCHWEIZ AG;INTELLECTUAL PROPERTY FREILAGERSTRASSE 40;8047 ZUERICH (CH) |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20090821 Year of fee payment: 13 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: CH Payment date: 20091110 Year of fee payment: 13 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20100831 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20100831 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20110502 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20100831 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20130814 Year of fee payment: 17 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20130827 Year of fee payment: 17 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20131021 Year of fee payment: 17 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 59701235 Country of ref document: DE |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20140826 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20140826 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 59701235 Country of ref document: DE Effective date: 20150303 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20140826 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20150303 |