RU2013143396A - POWER FORCING DEVICE WITH DYNAMIC DYNAMIC PROCESSES - Google Patents
POWER FORCING DEVICE WITH DYNAMIC DYNAMIC PROCESSES Download PDFInfo
- Publication number
- RU2013143396A RU2013143396A RU2013143396/06A RU2013143396A RU2013143396A RU 2013143396 A RU2013143396 A RU 2013143396A RU 2013143396/06 A RU2013143396/06 A RU 2013143396/06A RU 2013143396 A RU2013143396 A RU 2013143396A RU 2013143396 A RU2013143396 A RU 2013143396A
- Authority
- RU
- Russia
- Prior art keywords
- transition element
- power boosting
- boosting device
- channels
- power
- Prior art date
Links
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
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- 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
- F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
- F02C3/305—Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids
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- 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
- F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
- F02C5/10—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid forming a resonating or oscillating gas column, i.e. the combustion chambers having no positively actuated valves, e.g. using Helmholtz effect
- F02C5/11—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid forming a resonating or oscillating gas column, i.e. the combustion chambers having no positively actuated valves, e.g. using Helmholtz effect using valveless combustion chambers
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- 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
- F23L7/002—Supplying water
- F23L7/005—Evaporated water; Steam
-
- 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
- F23M20/00—Details of combustion chambers, not otherwise provided for, e.g. means for storing heat from flames
- F23M20/005—Noise absorbing means
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
-
- 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
- F23R2900/00013—Reducing thermo-acoustic vibrations by active means
-
- 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
- Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
Abstract
1. Устройство форсирования мощности с демпфированием динамических процессов, предназначенное для газотурбинного двигателя и содержащеепереходный элемент камеры сгорания,паровой коллектор, расположенный вокруг переходного элемента,причем через переходный элемент проходят каналы переходного элемента, ачерез паровой коллектор проходят каналы коллектора,при этом каналы коллектора совмещены с каналами переходного элемента.2. Устройство форсирования мощности по п.1, в котором каналы переходного элемента имеют проходящие через них отверстия.3. Устройство форсирования мощности по п.2, в котором указанные отверстия содержат отверстия, расположенные под углом.4. Устройство форсирования мощности по п.1, в котором паровой коллектор имеет расположенную в нем полость.5. Устройство форсирования мощности по п.1, в котором каналы коллектора содержат трубки.6. Устройство форсирования мощности по п.5, в котором указанные трубки содержат трубки, расположенные под углом.7. Устройство форсирования мощности по п.1, в котором паровой коллектор имеет продувочные каналы.8. Устройство форсирования мощности по п.1, в котором переходный элемент содержит раму, а паровой коллектор содержит паропровод, расположенный на указанной раме.9. Устройство форсирования мощности по п.1, в котором каналы коллектора имеют заданный размер, выбранный на основании частоты колебаний, возникающих в камере сгорания.10. Устройство форсирования мощности с демпфированием динамических процессов, предназначенное для газотурбинного двигателя и содержащеепереходный элемент камеры сгорания,паровой коллектор, расположенный вокруг переходного элемента,причем �1. A device for forcing power with damping of dynamic processes, intended for a gas turbine engine and containing a transition element of the combustion chamber, a steam collector located around the transition element, and through the transition element pass channels of the transition element, through the steam header pass the channels of the collector, while the channels of the collector are aligned with channels of the transition element. 2. The power forcing device according to claim 1, wherein the channels of the adapter have holes extending therethrough. The power boosting device of claim 2, wherein said holes comprise angled holes. The power boosting device according to claim 1, wherein the steam manifold has a cavity located therein. The power boosting device of claim 1, wherein the manifold channels comprise tubes. The power boosting device of claim 5, wherein said tubes comprise angled tubes. The power boosting device of claim 1, wherein the steam manifold has purge passages. The power boosting device according to claim 1, wherein the transition element comprises a frame, and the steam manifold comprises a steam line disposed on said frame. The power boosting device of claim 1, wherein the manifold channels are of a predetermined size selected based on the frequency of vibrations occurring in the combustion chamber. Power forcing device with damping of dynamic processes, intended for a gas turbine engine and containing a transition element of the combustion chamber, a steam manifold located around the transition element, where �
Claims (20)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/RU2011/000226 WO2012134325A1 (en) | 2011-03-31 | 2011-03-31 | Power augmentation system with dynamics damping |
Publications (1)
Publication Number | Publication Date |
---|---|
RU2013143396A true RU2013143396A (en) | 2015-05-10 |
Family
ID=44863196
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2013143396/06A RU2013143396A (en) | 2011-03-31 | 2011-03-31 | POWER FORCING DEVICE WITH DYNAMIC DYNAMIC PROCESSES |
Country Status (6)
Country | Link |
---|---|
US (1) | US20140013754A1 (en) |
EP (1) | EP2691609A1 (en) |
JP (1) | JP2014509707A (en) |
CN (1) | CN103649468A (en) |
RU (1) | RU2013143396A (en) |
WO (1) | WO2012134325A1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9650955B2 (en) * | 2011-11-10 | 2017-05-16 | General Electric Company | System for purging gas fuel circuit for a gas turbine engine |
EP2725196A1 (en) | 2012-10-24 | 2014-04-30 | Alstom Technology Ltd | Combustor transition |
US10378447B2 (en) | 2016-09-30 | 2019-08-13 | General Electric Company | System and method for purging fuel or coolant from turbomachine |
US11174792B2 (en) | 2019-05-21 | 2021-11-16 | General Electric Company | System and method for high frequency acoustic dampers with baffles |
US11156164B2 (en) | 2019-05-21 | 2021-10-26 | General Electric Company | System and method for high frequency accoustic dampers with caps |
Family Cites Families (22)
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US3657884A (en) * | 1970-11-20 | 1972-04-25 | Westinghouse Electric Corp | Trans-nozzle steam injection gas turbine |
US3747336A (en) * | 1972-03-29 | 1973-07-24 | Gen Electric | Steam injection system for a gas turbine |
US5239816A (en) * | 1992-03-16 | 1993-08-31 | General Electric Company | Steam deflector assembly for a steam injected gas turbine engine |
JP3202636B2 (en) * | 1997-02-12 | 2001-08-27 | 東北電力株式会社 | Cooling wall structure of steam-cooled combustor |
JP3110338B2 (en) * | 1997-02-12 | 2000-11-20 | 東北電力株式会社 | Combustor cooling structure with steam |
US5906093A (en) * | 1997-02-21 | 1999-05-25 | Siemens Westinghouse Power Corporation | Gas turbine combustor transition |
JP3310900B2 (en) * | 1997-04-15 | 2002-08-05 | 三菱重工業株式会社 | Cooling structure of combustor transition piece |
US6018950A (en) * | 1997-06-13 | 2000-02-01 | Siemens Westinghouse Power Corporation | Combustion turbine modular cooling panel |
US6983605B1 (en) * | 2000-04-07 | 2006-01-10 | General Electric Company | Methods and apparatus for reducing gas turbine engine emissions |
EP1146289B1 (en) * | 2000-04-13 | 2008-12-24 | Mitsubishi Heavy Industries, Ltd. | Cooling structure of combustor tail tube |
JP2002243154A (en) * | 2001-02-16 | 2002-08-28 | Mitsubishi Heavy Ind Ltd | Gas turbine combustor and tail cylinder outlet structure thereof |
JP2002317650A (en) * | 2001-04-24 | 2002-10-31 | Mitsubishi Heavy Ind Ltd | Gas turbine combustor |
US6662564B2 (en) * | 2001-09-27 | 2003-12-16 | Siemens Westinghouse Power Corporation | Catalytic combustor cooling tube vibration dampening device |
JP2003214185A (en) * | 2002-01-22 | 2003-07-30 | Mitsubishi Heavy Ind Ltd | Gas turbine combustor cooling structure and gas turbine |
US6890148B2 (en) * | 2003-08-28 | 2005-05-10 | Siemens Westinghouse Power Corporation | Transition duct cooling system |
JP2005076982A (en) * | 2003-08-29 | 2005-03-24 | Mitsubishi Heavy Ind Ltd | Gas turbine combustor |
US7413053B2 (en) * | 2006-01-25 | 2008-08-19 | Siemens Power Generation, Inc. | Acoustic resonator with impingement cooling tubes |
US8387398B2 (en) * | 2007-09-14 | 2013-03-05 | Siemens Energy, Inc. | Apparatus and method for controlling the secondary injection of fuel |
US8567197B2 (en) * | 2008-12-31 | 2013-10-29 | General Electric Company | Acoustic damper |
GB0907578D0 (en) * | 2009-05-05 | 2009-06-10 | Rolls Royce Plc | A damping assembly |
US8387358B2 (en) * | 2010-01-29 | 2013-03-05 | General Electric Company | Gas turbine engine steam injection manifold |
JP5804872B2 (en) * | 2011-09-27 | 2015-11-04 | 三菱日立パワーシステムズ株式会社 | Combustor transition piece, gas turbine equipped with the same, and transition piece manufacturing method |
-
2011
- 2011-03-31 CN CN201180069734.XA patent/CN103649468A/en active Pending
- 2011-03-31 JP JP2014502504A patent/JP2014509707A/en not_active Withdrawn
- 2011-03-31 RU RU2013143396/06A patent/RU2013143396A/en not_active Application Discontinuation
- 2011-03-31 US US14/008,219 patent/US20140013754A1/en not_active Abandoned
- 2011-03-31 EP EP11775858.1A patent/EP2691609A1/en not_active Withdrawn
- 2011-03-31 WO PCT/RU2011/000226 patent/WO2012134325A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
EP2691609A1 (en) | 2014-02-05 |
JP2014509707A (en) | 2014-04-21 |
CN103649468A (en) | 2014-03-19 |
US20140013754A1 (en) | 2014-01-16 |
WO2012134325A1 (en) | 2012-10-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FA92 | Acknowledgement of application withdrawn (lack of supplementary materials submitted) |
Effective date: 20150608 |