CN103161513B - 改进的用于燃气涡轮发动机的喷嘴叶片 - Google Patents
改进的用于燃气涡轮发动机的喷嘴叶片 Download PDFInfo
- Publication number
- CN103161513B CN103161513B CN201210545238.3A CN201210545238A CN103161513B CN 103161513 B CN103161513 B CN 103161513B CN 201210545238 A CN201210545238 A CN 201210545238A CN 103161513 B CN103161513 B CN 103161513B
- Authority
- CN
- China
- Prior art keywords
- nozzle vane
- impinging
- impinging cooling
- wall surface
- nozzle
- 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 - Fee Related
Links
- 238000001816 cooling Methods 0.000 claims abstract description 67
- 239000002826 coolant Substances 0.000 claims abstract description 35
- 239000012530 fluid Substances 0.000 claims abstract description 27
- 238000012546 transfer Methods 0.000 claims description 25
- 238000003780 insertion Methods 0.000 claims description 23
- 230000037431 insertion Effects 0.000 claims description 23
- 238000011144 upstream manufacturing Methods 0.000 claims description 6
- 230000005855 radiation Effects 0.000 claims description 4
- 238000003491 array Methods 0.000 claims description 3
- 230000015556 catabolic process Effects 0.000 claims description 2
- 238000006731 degradation reaction Methods 0.000 claims description 2
- 239000000203 mixture Substances 0.000 claims description 2
- 239000007921 spray Substances 0.000 claims description 2
- 238000005452 bending Methods 0.000 claims 1
- 238000013461 design Methods 0.000 description 7
- 230000000694 effects Effects 0.000 description 6
- 230000008859 change Effects 0.000 description 5
- 239000000567 combustion gas Substances 0.000 description 5
- 239000007787 solid Substances 0.000 description 5
- 238000002485 combustion reaction Methods 0.000 description 4
- 239000012809 cooling fluid Substances 0.000 description 4
- 241000194386 Coelosis Species 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 238000009826 distribution Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000006386 neutralization reaction Methods 0.000 description 2
- 238000005086 pumping Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000007634 remodeling Methods 0.000 description 1
- 238000010025 steaming Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Classifications
-
- 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
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
- F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
- F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
-
- 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
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
-
- 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
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/13—Two-dimensional trapezoidal
- F05D2250/131—Two-dimensional trapezoidal polygonal
-
- 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
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/326,372 | 2011-12-15 | ||
| US13/326372 | 2011-12-15 | ||
| US13/326,372 US9151173B2 (en) | 2011-12-15 | 2011-12-15 | Use of multi-faceted impingement openings for increasing heat transfer characteristics on gas turbine components |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103161513A CN103161513A (zh) | 2013-06-19 |
| CN103161513B true CN103161513B (zh) | 2017-03-01 |
Family
ID=47297013
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210545238.3A Expired - Fee Related CN103161513B (zh) | 2011-12-15 | 2012-12-14 | 改进的用于燃气涡轮发动机的喷嘴叶片 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9151173B2 (enExample) |
| EP (1) | EP2604800B1 (enExample) |
| JP (1) | JP2013124663A (enExample) |
| CN (1) | CN103161513B (enExample) |
| RU (1) | RU2012153930A (enExample) |
Families Citing this family (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10100666B2 (en) * | 2013-03-29 | 2018-10-16 | General Electric Company | Hot gas path component for turbine system |
| US9849510B2 (en) | 2015-04-16 | 2017-12-26 | General Electric Company | Article and method of forming an article |
| US9976441B2 (en) | 2015-05-29 | 2018-05-22 | General Electric Company | Article, component, and method of forming an article |
| US9995151B2 (en) | 2015-08-17 | 2018-06-12 | General Electric Company | Article and manifold for thermal adjustment of a turbine component |
| US10253986B2 (en) * | 2015-09-08 | 2019-04-09 | General Electric Company | Article and method of forming an article |
| US10739087B2 (en) | 2015-09-08 | 2020-08-11 | General Electric Company | Article, component, and method of forming an article |
| US10087776B2 (en) | 2015-09-08 | 2018-10-02 | General Electric Company | Article and method of forming an article |
| US10815789B2 (en) | 2016-02-13 | 2020-10-27 | General Electric Company | Impingement holes for a turbine engine component |
| EP3236010A1 (de) * | 2016-04-21 | 2017-10-25 | Siemens Aktiengesellschaft | Leitschaufel mit einem verbindungsrohr |
| US10309228B2 (en) * | 2016-06-09 | 2019-06-04 | General Electric Company | Impingement insert for a gas turbine engine |
| US10436037B2 (en) | 2016-07-22 | 2019-10-08 | General Electric Company | Blade with parallel corrugated surfaces on inner and outer surfaces |
| US10465525B2 (en) | 2016-07-22 | 2019-11-05 | General Electric Company | Blade with internal rib having corrugated surface(s) |
| US10450868B2 (en) * | 2016-07-22 | 2019-10-22 | General Electric Company | Turbine rotor blade with coupon having corrugated surface(s) |
| US10465520B2 (en) | 2016-07-22 | 2019-11-05 | General Electric Company | Blade with corrugated outer surface(s) |
| US10443399B2 (en) * | 2016-07-22 | 2019-10-15 | General Electric Company | Turbine vane with coupon having corrugated surface(s) |
| US10655477B2 (en) | 2016-07-26 | 2020-05-19 | General Electric Company | Turbine components and method for forming turbine components |
| US10577942B2 (en) * | 2016-11-17 | 2020-03-03 | General Electric Company | Double impingement slot cap assembly |
| EP3351341A1 (de) | 2017-01-23 | 2018-07-25 | Siemens Aktiengesellschaft | Verfahren zur herstellung eines hohlraums in einer schaufelplattform |
| US20190277501A1 (en) * | 2018-03-07 | 2019-09-12 | United Technologies Corporation | Slot arrangements for an impingement floatwall film cooling of a turbine engine |
| US11192207B2 (en) | 2018-10-26 | 2021-12-07 | General Electric Company | Additive manufactured object with passage having varying cross-sectional shape |
| US10711620B1 (en) * | 2019-01-14 | 2020-07-14 | General Electric Company | Insert system for an airfoil and method of installing same |
| US11358221B2 (en) * | 2019-09-30 | 2022-06-14 | The Boeing Company | Build part and method of additively manufacturing the build part |
| US11629642B2 (en) | 2019-12-20 | 2023-04-18 | General Electric Company | System and methods for igniting and operating a gas turbine engine with alternative fuels |
| US11959641B2 (en) * | 2020-01-31 | 2024-04-16 | Rtx Corporation | Combustor shell with shaped impingement holes |
| CN112268012B (zh) * | 2020-10-10 | 2022-02-11 | 浙江理工大学 | 带尾翼射流装置的无蜗壳离心通风机叶轮及其工作方法 |
| CN113944516B (zh) * | 2021-09-28 | 2024-04-02 | 中国科学院工程热物理研究所 | 一种燃气涡轮叶尖复合冷却结构 |
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| US1545560A (en) | 1924-08-06 | 1925-07-14 | Heath Spencer | Airplane propeller |
| US1939357A (en) | 1929-02-13 | 1933-12-12 | Bendix Aviat Corp | Hollow blade for turbines |
| US3148954A (en) | 1960-06-13 | 1964-09-15 | Haas Irene | Turbine blade construction |
| GB1565361A (en) | 1976-01-29 | 1980-04-16 | Rolls Royce | Blade or vane for a gas turbine engien |
| GB2119028B (en) | 1982-04-27 | 1985-02-27 | Rolls Royce | Aerofoil for a gas turbine engine |
| US4645415A (en) | 1983-12-23 | 1987-02-24 | United Technologies Corporation | Air cooler for providing buffer air to a bearing compartment |
| FR2581708B1 (fr) | 1985-05-09 | 1989-04-28 | Snecma | Capotage pour bord d'attaque d'aube de soufflante de turboreacteur |
| US4669957A (en) | 1985-12-23 | 1987-06-02 | United Technologies Corporation | Film coolant passage with swirl diffuser |
| FR2599425B1 (fr) | 1986-05-28 | 1988-08-05 | Alsthom | Plaquette de protection pour aube en titane et procede de brasage d'une telle plaquette. |
| US5667359A (en) | 1988-08-24 | 1997-09-16 | United Technologies Corp. | Clearance control for the turbine of a gas turbine engine |
| US5210946A (en) | 1992-06-26 | 1993-05-18 | Hudson Products Corporation | Leading edge protection for fan blade |
| JP3651490B2 (ja) | 1993-12-28 | 2005-05-25 | 株式会社東芝 | タービン冷却翼 |
| US5634766A (en) | 1994-08-23 | 1997-06-03 | General Electric Co. | Turbine stator vane segments having combined air and steam cooling circuits |
| GB2293631B (en) | 1994-09-30 | 1998-09-09 | Gen Electric | Composite fan blade trailing edge reinforcement |
| US5685693A (en) | 1995-03-31 | 1997-11-11 | General Electric Co. | Removable inner turbine shell with bucket tip clearance control |
| US5779437A (en) | 1996-10-31 | 1998-07-14 | Pratt & Whitney Canada Inc. | Cooling passages for airfoil leading edge |
| JPH1144498A (ja) * | 1997-05-30 | 1999-02-16 | Showa Alum Corp | 熱交換器用偏平多孔チューブ及び同チューブを用いた熱交換器 |
| US6238182B1 (en) | 1999-02-19 | 2001-05-29 | Meyer Tool, Inc. | Joint for a turbine component |
| US6183192B1 (en) | 1999-03-22 | 2001-02-06 | General Electric Company | Durable turbine nozzle |
| JP3794868B2 (ja) | 1999-06-15 | 2006-07-12 | 三菱重工業株式会社 | ガスタービン静翼 |
| JP3322857B2 (ja) | 1999-11-30 | 2002-09-09 | モルデック株式会社 | レセプタクルコネクタのインサート成形方法 |
| US6468031B1 (en) * | 2000-05-16 | 2002-10-22 | General Electric Company | Nozzle cavity impingement/area reduction insert |
| US6428273B1 (en) * | 2001-01-05 | 2002-08-06 | General Electric Company | Truncated rib turbine nozzle |
| JP4508432B2 (ja) | 2001-01-09 | 2010-07-21 | 三菱重工業株式会社 | ガスタービンの冷却構造 |
| EP1275818B1 (de) * | 2001-07-13 | 2006-08-16 | ALSTOM Technology Ltd | Gasturbinenteil mit Kühlluftbohrungen |
| US6742991B2 (en) | 2002-07-11 | 2004-06-01 | Mitsubishi Heavy Industries, Ltd. | Turbine blade and gas turbine |
| JP4191578B2 (ja) | 2003-11-21 | 2008-12-03 | 三菱重工業株式会社 | ガスタービンエンジンのタービン冷却翼 |
| US7008178B2 (en) * | 2003-12-17 | 2006-03-07 | General Electric Company | Inboard cooled nozzle doublet |
| US20050265840A1 (en) | 2004-05-27 | 2005-12-01 | Levine Jeffrey R | Cooled rotor blade with leading edge impingement cooling |
| US7374401B2 (en) * | 2005-03-01 | 2008-05-20 | General Electric Company | Bell-shaped fan cooling holes for turbine airfoil |
| JP2010515850A (ja) * | 2007-01-04 | 2010-05-13 | アンサルド エネルジア エス．ピー．エー． | ガスタービンブレード・インサート用スペーサ |
| DE102007018061A1 (de) * | 2007-04-17 | 2008-10-23 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammerwand |
| JP2009162119A (ja) * | 2008-01-08 | 2009-07-23 | Ihi Corp | タービン翼の冷却構造 |
| US20100037620A1 (en) | 2008-08-15 | 2010-02-18 | General Electric Company, Schenectady | Impingement and effusion cooled combustor component |
| US8142137B2 (en) * | 2008-11-26 | 2012-03-27 | Alstom Technology Ltd | Cooled gas turbine vane assembly |
| CH701031A1 (de) * | 2009-05-15 | 2010-11-15 | Alstom Technology Ltd | Verfahren zum Aufarbeiten einer Turbinenschaufel. |
| US20110097191A1 (en) * | 2009-10-28 | 2011-04-28 | General Electric Company | Method and structure for cooling airfoil surfaces using asymmetric chevron film holes |
| US8529193B2 (en) * | 2009-11-25 | 2013-09-10 | Honeywell International Inc. | Gas turbine engine components with improved film cooling |
| FR2955145B1 (fr) * | 2010-01-14 | 2012-02-03 | Snecma | Distributeur de turbine haute pression d'un turboreacteur |
-
2011
- 2011-12-15 US US13/326,372 patent/US9151173B2/en not_active Expired - Fee Related
-
2012
- 2012-12-07 EP EP12196112.2A patent/EP2604800B1/en not_active Not-in-force
- 2012-12-10 JP JP2012268914A patent/JP2013124663A/ja active Pending
- 2012-12-14 CN CN201210545238.3A patent/CN103161513B/zh not_active Expired - Fee Related
- 2012-12-14 RU RU2012153930/06A patent/RU2012153930A/ru not_active Application Discontinuation
Also Published As
| Publication number | Publication date |
|---|---|
| EP2604800A3 (en) | 2015-07-22 |
| EP2604800B1 (en) | 2018-02-21 |
| RU2012153930A (ru) | 2014-06-20 |
| EP2604800A2 (en) | 2013-06-19 |
| US20130156549A1 (en) | 2013-06-20 |
| CN103161513A (zh) | 2013-06-19 |
| US9151173B2 (en) | 2015-10-06 |
| JP2013124663A (ja) | 2013-06-24 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170301 Termination date: 20181214 |