JP5282057B2 - 燃焼器ライナ冷却システム - Google Patents
燃焼器ライナ冷却システム Download PDFInfo
- Publication number
- JP5282057B2 JP5282057B2 JP2010047247A JP2010047247A JP5282057B2 JP 5282057 B2 JP5282057 B2 JP 5282057B2 JP 2010047247 A JP2010047247 A JP 2010047247A JP 2010047247 A JP2010047247 A JP 2010047247A JP 5282057 B2 JP5282057 B2 JP 5282057B2
- Authority
- JP
- Japan
- Prior art keywords
- air
- liner
- combustor liner
- combustor
- cooling
- 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.)
- Active
Links
- 238000001816 cooling Methods 0.000 title claims abstract description 168
- 238000002485 combustion reaction Methods 0.000 claims description 51
- 239000000446 fuel Substances 0.000 claims description 35
- 238000011144 upstream manufacturing Methods 0.000 claims description 27
- 239000000567 combustion gas Substances 0.000 claims description 21
- 230000007704 transition Effects 0.000 claims description 19
- 230000004323 axial length Effects 0.000 claims description 12
- 239000000203 mixture Substances 0.000 claims description 8
- 239000007789 gas Substances 0.000 description 12
- 238000000034 method Methods 0.000 description 8
- 238000002955 isolation Methods 0.000 description 4
- 230000008901 benefit Effects 0.000 description 2
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 238000003698 laser cutting Methods 0.000 description 1
- 238000010329 laser etching Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000003345 natural gas Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000003786 synthesis reaction Methods 0.000 description 1
Images
Classifications
-
- 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
- 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
-
- 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
- F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/401,530 | 2009-03-10 | ||
| US12/401,530 US8307657B2 (en) | 2009-03-10 | 2009-03-10 | Combustor liner cooling system |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2010209912A JP2010209912A (ja) | 2010-09-24 |
| JP2010209912A5 JP2010209912A5 (enExample) | 2013-01-24 |
| JP5282057B2 true JP5282057B2 (ja) | 2013-09-04 |
Family
ID=42232685
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2010047247A Active JP5282057B2 (ja) | 2009-03-10 | 2010-03-04 | 燃焼器ライナ冷却システム |
Country Status (4)
| Country | Link |
|---|---|
| US (2) | US8307657B2 (enExample) |
| EP (1) | EP2228602B1 (enExample) |
| JP (1) | JP5282057B2 (enExample) |
| CN (1) | CN101832555B (enExample) |
Families Citing this family (86)
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|---|---|---|---|---|
| US8051663B2 (en) | 2007-11-09 | 2011-11-08 | United Technologies Corp. | Gas turbine engine systems involving cooling of combustion section liners |
| US8695322B2 (en) * | 2009-03-30 | 2014-04-15 | General Electric Company | Thermally decoupled can-annular transition piece |
| US8448416B2 (en) * | 2009-03-30 | 2013-05-28 | General Electric Company | Combustor liner |
| US8359867B2 (en) | 2010-04-08 | 2013-01-29 | General Electric Company | Combustor having a flow sleeve |
| US8959886B2 (en) * | 2010-07-08 | 2015-02-24 | Siemens Energy, Inc. | Mesh cooled conduit for conveying combustion gases |
| US8894363B2 (en) | 2011-02-09 | 2014-11-25 | Siemens Energy, Inc. | Cooling module design and method for cooling components of a gas turbine system |
| US8813501B2 (en) * | 2011-01-03 | 2014-08-26 | General Electric Company | Combustor assemblies for use in turbine engines and methods of assembling same |
| US20120198855A1 (en) * | 2011-02-03 | 2012-08-09 | General Electric Company | Method and apparatus for cooling combustor liner in combustor |
| US8955330B2 (en) * | 2011-03-29 | 2015-02-17 | Siemens Energy, Inc. | Turbine combustion system liner |
| JP5696566B2 (ja) * | 2011-03-31 | 2015-04-08 | 株式会社Ihi | ガスタービンエンジン用燃焼器及びガスタービンエンジン |
| JP5455962B2 (ja) * | 2011-04-06 | 2014-03-26 | 三菱重工業株式会社 | 冷却構造の製造方法 |
| US8601820B2 (en) * | 2011-06-06 | 2013-12-10 | General Electric Company | Integrated late lean injection on a combustion liner and late lean injection sleeve assembly |
| US20130074471A1 (en) * | 2011-09-22 | 2013-03-28 | General Electric Company | Turbine combustor and method for temperature control and damping a portion of a combustor |
| GB201116608D0 (en) * | 2011-09-27 | 2011-11-09 | Rolls Royce Plc | A method of operating a combustion chamber |
| US20130086915A1 (en) * | 2011-10-07 | 2013-04-11 | General Electric Company | Film cooled combustion liner assembly |
| US9267687B2 (en) | 2011-11-04 | 2016-02-23 | General Electric Company | Combustion system having a venturi for reducing wakes in an airflow |
| US8899975B2 (en) * | 2011-11-04 | 2014-12-02 | General Electric Company | Combustor having wake air injection |
| US9249977B2 (en) * | 2011-11-22 | 2016-02-02 | Mitsubishi Hitachi Power Systems, Ltd. | Combustor with acoustic liner |
| US9243506B2 (en) * | 2012-01-03 | 2016-01-26 | General Electric Company | Methods and systems for cooling a transition nozzle |
| KR101406065B1 (ko) * | 2012-03-16 | 2014-07-01 | 주식회사 글로벌스탠다드테크놀로지 | 선회류 예혼합 저공해 연소장치 |
| US20140047846A1 (en) * | 2012-08-14 | 2014-02-20 | General Electric Company | Turbine component cooling arrangement and method of cooling a turbine component |
| US9222672B2 (en) * | 2012-08-14 | 2015-12-29 | General Electric Company | Combustor liner cooling assembly |
| US10107497B2 (en) * | 2012-10-04 | 2018-10-23 | United Technologies Corporation | Gas turbine engine combustor liner |
| US9869279B2 (en) * | 2012-11-02 | 2018-01-16 | General Electric Company | System and method for a multi-wall turbine combustor |
| US20140130504A1 (en) * | 2012-11-12 | 2014-05-15 | General Electric Company | System for cooling a hot gas component for a combustor of a gas turbine |
| JP6025587B2 (ja) * | 2013-02-01 | 2016-11-16 | 三菱日立パワーシステムズ株式会社 | 燃焼器およびガスタービン |
| US9366438B2 (en) * | 2013-02-14 | 2016-06-14 | Siemens Aktiengesellschaft | Flow sleeve inlet assembly in a gas turbine engine |
| US9939154B2 (en) | 2013-02-14 | 2018-04-10 | United Technologies Corporation | Combustor liners with U-shaped cooling channels |
| US9988911B2 (en) * | 2013-02-26 | 2018-06-05 | United Technologies Corporation | Gas turbine engine component paired film cooling holes |
| US9322553B2 (en) | 2013-05-08 | 2016-04-26 | General Electric Company | Wake manipulating structure for a turbine system |
| US9739201B2 (en) | 2013-05-08 | 2017-08-22 | General Electric Company | Wake reducing structure for a turbine system and method of reducing wake |
| WO2015002686A2 (en) | 2013-06-14 | 2015-01-08 | United Technologies Corporation | Gas turbine engine combustor liner panel |
| US9435221B2 (en) | 2013-08-09 | 2016-09-06 | General Electric Company | Turbomachine airfoil positioning |
| CN103398398B (zh) * | 2013-08-12 | 2016-01-20 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 一种燃气轮机燃烧室火焰筒与过渡段的双密封连接结构 |
| EP3060847B1 (en) | 2013-10-24 | 2019-09-18 | United Technologies Corporation | Passage geometry for gas turbine engine combustor |
| EP3066389B1 (en) * | 2013-11-04 | 2019-01-02 | United Technologies Corporation | Turbine engine combustor heat shield with one or more cooling elements |
| WO2015077592A1 (en) * | 2013-11-22 | 2015-05-28 | United Technologies Corporation | Turbine engine multi-walled structure with cooling element(s) |
| EP2949871B1 (en) * | 2014-05-07 | 2017-03-01 | United Technologies Corporation | Variable vane segment |
| US20170167729A1 (en) * | 2014-07-30 | 2017-06-15 | Siemens Aktiengesellschaft | Multiple feed platefins within a hot gas path cooling system in a combustor basket in a combustion turbine engine |
| US10101030B2 (en) * | 2014-09-02 | 2018-10-16 | Honeywell International Inc. | Gas turbine engines with plug resistant effusion cooling holes |
| EP3189277B1 (en) | 2014-09-05 | 2020-04-15 | Siemens Aktiengesellschaft | Cross ignition flame duct |
| CN104296160A (zh) * | 2014-09-22 | 2015-01-21 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 一种具有冷却功能的燃气轮机燃烧室的导流衬套 |
| US10215418B2 (en) * | 2014-10-13 | 2019-02-26 | Ansaldo Energia Ip Uk Limited | Sealing device for a gas turbine combustor |
| CN104359126B (zh) * | 2014-10-31 | 2017-09-15 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 一种燃气轮机燃烧室火焰筒的交错式冷却结构 |
| JP6223954B2 (ja) * | 2014-12-02 | 2017-11-01 | 三菱日立パワーシステムズ株式会社 | 燃焼器及びガスタービン |
| US10316746B2 (en) * | 2015-02-04 | 2019-06-11 | General Electric Company | Turbine system with exhaust gas recirculation, separation and extraction |
| US10253690B2 (en) * | 2015-02-04 | 2019-04-09 | General Electric Company | Turbine system with exhaust gas recirculation, separation and extraction |
| US20160230993A1 (en) * | 2015-02-10 | 2016-08-11 | United Technologies Corporation | Combustor liner effusion cooling holes |
| KR101853456B1 (ko) * | 2015-06-16 | 2018-04-30 | 두산중공업 주식회사 | 가스터빈용 연소 덕트 조립체 |
| US10648669B2 (en) * | 2015-08-21 | 2020-05-12 | Rolls-Royce Corporation | Case and liner arrangement for a combustor |
| KR102075901B1 (ko) * | 2015-11-05 | 2020-02-11 | 미츠비시 히타치 파워 시스템즈 가부시키가이샤 | 연소용 통, 가스 터빈 연소기 및 가스 터빈 |
| CN105240855B (zh) * | 2015-11-16 | 2017-08-11 | 中车戚墅堰机车车辆工艺研究所有限公司 | 天然气加热炉烧嘴冷却保护装置 |
| US10815789B2 (en) * | 2016-02-13 | 2020-10-27 | General Electric Company | Impingement holes for a turbine engine component |
| US10724441B2 (en) * | 2016-03-25 | 2020-07-28 | General Electric Company | Segmented annular combustion system |
| JP6779098B2 (ja) * | 2016-10-24 | 2020-11-04 | 三菱パワー株式会社 | ガスタービン燃焼器 |
| US10619854B2 (en) * | 2016-11-30 | 2020-04-14 | United Technologies Corporation | Systems and methods for combustor panel |
| WO2018107335A1 (zh) * | 2016-12-12 | 2018-06-21 | 深圳智慧能源技术有限公司 | 依靠气源能量提供冷却空气的火炬 |
| US10577954B2 (en) | 2017-03-27 | 2020-03-03 | Honeywell International Inc. | Blockage-resistant vane impingement tubes and turbine nozzles containing the same |
| KR101986729B1 (ko) * | 2017-08-22 | 2019-06-07 | 두산중공업 주식회사 | 실 영역 집중냉각을 위한 냉각유로 구조 및 이를 포함하는 가스 터빈용 연소기 |
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| KR102050563B1 (ko) * | 2017-11-03 | 2019-11-29 | 두산중공업 주식회사 | 연소기 및 이를 포함하는 가스 터빈 |
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| US11060484B2 (en) * | 2018-06-29 | 2021-07-13 | The Boeing Company | Nozzle wall for an air-breathing engine of a vehicle and method therefor |
| US11859818B2 (en) | 2019-02-25 | 2024-01-02 | General Electric Company | Systems and methods for variable microchannel combustor liner cooling |
| CN110173897A (zh) * | 2019-07-04 | 2019-08-27 | 广东省众骋热能科技有限公司 | 一种具有多级绝热结构的燃烧换热装置 |
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| KR102282668B1 (ko) * | 2020-03-02 | 2021-07-28 | 두산중공업 주식회사 | 라이너 냉각장치, 연소기 및 이를 포함하는 가스터빈 |
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| US11255545B1 (en) | 2020-10-26 | 2022-02-22 | General Electric Company | Integrated combustion nozzle having a unified head end |
| US12454912B2 (en) * | 2020-12-03 | 2025-10-28 | Rtx Corporation | Supplemental thrust system for a gas turbine engine |
| US11371701B1 (en) | 2021-02-03 | 2022-06-28 | General Electric Company | Combustor for a gas turbine engine |
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| US11885495B2 (en) | 2021-06-07 | 2024-01-30 | General Electric Company | Combustor for a gas turbine engine including a liner having a looped feature |
| US12152777B2 (en) | 2021-06-07 | 2024-11-26 | General Electric Company | Combustor for a gas turbine engine |
| US11959643B2 (en) | 2021-06-07 | 2024-04-16 | General Electric Company | Combustor for a gas turbine engine |
| US12146660B2 (en) | 2021-06-07 | 2024-11-19 | General Electric Company | Combustor for a gas turbine engine |
| US11774098B2 (en) | 2021-06-07 | 2023-10-03 | General Electric Company | Combustor for a gas turbine engine |
| CN117091159A (zh) * | 2022-05-13 | 2023-11-21 | 通用电气公司 | 燃烧器衬里 |
| US11767766B1 (en) | 2022-07-29 | 2023-09-26 | General Electric Company | Turbomachine airfoil having impingement cooling passages |
| US12292193B2 (en) | 2023-06-28 | 2025-05-06 | Rtx Corporation | Combustor liner with pattern of voids in CMC fiber ply for cooling channels |
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-
2009
- 2009-03-10 US US12/401,530 patent/US8307657B2/en active Active
-
2010
- 2010-03-04 JP JP2010047247A patent/JP5282057B2/ja active Active
- 2010-03-09 EP EP10155880.7A patent/EP2228602B1/en active Active
- 2010-03-10 CN CN201010143929.1A patent/CN101832555B/zh not_active Expired - Fee Related
-
2012
- 2012-10-15 US US13/652,275 patent/US20130036742A1/en not_active Abandoned
Also Published As
| Publication number | Publication date |
|---|---|
| CN101832555A (zh) | 2010-09-15 |
| EP2228602B1 (en) | 2024-01-24 |
| US8307657B2 (en) | 2012-11-13 |
| US20130036742A1 (en) | 2013-02-14 |
| EP2228602A2 (en) | 2010-09-15 |
| US20100229564A1 (en) | 2010-09-16 |
| JP2010209912A (ja) | 2010-09-24 |
| CN101832555B (zh) | 2014-08-20 |
| EP2228602A3 (en) | 2017-11-01 |
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