CH708700A8 - System zur Schaffung einer Kühlung für Turbinenkomponenten. - Google Patents
System zur Schaffung einer Kühlung für Turbinenkomponenten. Download PDFInfo
- Publication number
- CH708700A8 CH708700A8 CH01492/14A CH14922014A CH708700A8 CH 708700 A8 CH708700 A8 CH 708700A8 CH 01492/14 A CH01492/14 A CH 01492/14A CH 14922014 A CH14922014 A CH 14922014A CH 708700 A8 CH708700 A8 CH 708700A8
- Authority
- CH
- Switzerland
- Prior art keywords
- providing cooling
- cooled
- region
- turbine components
- support projection
- Prior art date
Links
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
- 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
-
- 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
-
- 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
- F01D5/186—Film cooling
-
- 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
- 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
- F01D5/182—Transpiration cooling
- F01D5/183—Blade walls being porous
-
- 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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/21—Manufacture essentially without removing material by casting
-
- 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
- F05D2230/00—Manufacture
- F05D2230/90—Coating; Surface treatment
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/122—Fluid guiding means, e.g. vanes related to the trailing edge of a stator vane
-
- 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
- F05D2260/202—Heat transfer, e.g. cooling by film cooling
-
- 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
- F05D2260/204—Heat transfer, e.g. cooling by the use of microcircuits
-
- 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
- F05D2260/221—Improvement of heat transfer
- F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
- F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/612—Foam
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Es ist ein System (100) zur Schaffung einer Kühlung einer Turbinenkomponente (34), die eine, zu kühlende Region enthält, geschaffen. Eine Aussparung ist innerhalb der zu kühlenden Region ausgebildet und enthält eine Innenfläche. Wenigstens ein Stützvorsprung (48) erstreckt sich von der Innenfläche aus. Der wenigstens eine Stützvorsprung (48) enthält ein freies Ende. Eine Abdeckung (54) wird mit der zu kühlenden Region verbunden, so dass eine innere Oberfläche (57) der Abdeckung (54) mit dem freien Ende des wenigstens einen Stützvorsprungs (48) derart verbunden ist, dass wenigstens ein Kühlfluidkanal innerhalb der zu kühlenden Region ausgebildet ist.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/046,437 US9458725B2 (en) | 2013-10-04 | 2013-10-04 | Method and system for providing cooling for turbine components |
Publications (2)
Publication Number | Publication Date |
---|---|
CH708700A2 CH708700A2 (de) | 2015-04-15 |
CH708700A8 true CH708700A8 (de) | 2015-07-31 |
Family
ID=52693374
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH01492/14A CH708700A8 (de) | 2013-10-04 | 2014-10-01 | System zur Schaffung einer Kühlung für Turbinenkomponenten. |
Country Status (4)
Country | Link |
---|---|
US (1) | US9458725B2 (de) |
JP (1) | JP6431737B2 (de) |
CH (1) | CH708700A8 (de) |
DE (1) | DE102014114240A1 (de) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9828915B2 (en) * | 2015-06-15 | 2017-11-28 | General Electric Company | Hot gas path component having near wall cooling features |
US9970302B2 (en) | 2015-06-15 | 2018-05-15 | General Electric Company | Hot gas path component trailing edge having near wall cooling features |
US9897006B2 (en) | 2015-06-15 | 2018-02-20 | General Electric Company | Hot gas path component cooling system having a particle collection chamber |
US9938899B2 (en) | 2015-06-15 | 2018-04-10 | General Electric Company | Hot gas path component having cast-in features for near wall cooling |
US10520193B2 (en) | 2015-10-28 | 2019-12-31 | General Electric Company | Cooling patch for hot gas path components |
EP3192970A1 (de) * | 2016-01-15 | 2017-07-19 | General Electric Technology GmbH | Gasturbinenschaufel und herstellungsverfahren |
US10260354B2 (en) * | 2016-02-12 | 2019-04-16 | General Electric Company | Airfoil trailing edge cooling |
US20170306775A1 (en) * | 2016-04-21 | 2017-10-26 | General Electric Company | Article, component, and method of making a component |
US10436048B2 (en) * | 2016-08-12 | 2019-10-08 | General Electric Comapny | Systems for removing heat from turbine components |
US10450950B2 (en) | 2016-10-26 | 2019-10-22 | General Electric Company | Turbomachine blade with trailing edge cooling circuit |
US10233761B2 (en) * | 2016-10-26 | 2019-03-19 | General Electric Company | Turbine airfoil trailing edge coolant passage created by cover |
US10352176B2 (en) | 2016-10-26 | 2019-07-16 | General Electric Company | Cooling circuits for a multi-wall blade |
US10273810B2 (en) | 2016-10-26 | 2019-04-30 | General Electric Company | Partially wrapped trailing edge cooling circuit with pressure side serpentine cavities |
US10465521B2 (en) | 2016-10-26 | 2019-11-05 | General Electric Company | Turbine airfoil coolant passage created in cover |
US10598028B2 (en) | 2016-10-26 | 2020-03-24 | General Electric Company | Edge coupon including cooling circuit for airfoil |
US10301946B2 (en) | 2016-10-26 | 2019-05-28 | General Electric Company | Partially wrapped trailing edge cooling circuits with pressure side impingements |
US10450875B2 (en) | 2016-10-26 | 2019-10-22 | General Electric Company | Varying geometries for cooling circuits of turbine blades |
US10309227B2 (en) | 2016-10-26 | 2019-06-04 | General Electric Company | Multi-turn cooling circuits for turbine blades |
US10240465B2 (en) | 2016-10-26 | 2019-03-26 | General Electric Company | Cooling circuits for a multi-wall blade |
US11505310B2 (en) | 2017-12-21 | 2022-11-22 | Airbus Operations Gmbh | Flow body for a vehicle with a compressible skin |
US10933481B2 (en) | 2018-01-05 | 2021-03-02 | General Electric Company | Method of forming cooling passage for turbine component with cap element |
US10612391B2 (en) | 2018-01-05 | 2020-04-07 | General Electric Company | Two portion cooling passage for airfoil |
US11460191B2 (en) | 2020-08-31 | 2022-10-04 | General Electric Company | Cooling insert for a turbomachine |
US11614233B2 (en) | 2020-08-31 | 2023-03-28 | General Electric Company | Impingement panel support structure and method of manufacture |
US11371702B2 (en) | 2020-08-31 | 2022-06-28 | General Electric Company | Impingement panel for a turbomachine |
US11255545B1 (en) | 2020-10-26 | 2022-02-22 | General Electric Company | Integrated combustion nozzle having a unified head end |
US11814965B2 (en) | 2021-11-10 | 2023-11-14 | General Electric Company | Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions |
US11767766B1 (en) | 2022-07-29 | 2023-09-26 | General Electric Company | Turbomachine airfoil having impingement cooling passages |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5626462A (en) | 1995-01-03 | 1997-05-06 | General Electric Company | Double-wall airfoil |
US5820337A (en) | 1995-01-03 | 1998-10-13 | General Electric Company | Double wall turbine parts |
JP3297271B2 (ja) * | 1995-11-22 | 2002-07-02 | 三菱重工業株式会社 | 蒸気冷却静翼 |
US5957657A (en) | 1996-02-26 | 1999-09-28 | Mitisubishi Heavy Industries, Ltd. | Method of forming a cooling air passage in a gas turbine stationary blade shroud |
KR20010031463A (ko) | 1997-10-27 | 2001-04-16 | 랭크 크리스토퍼 제이 | 주물 초합금을 접합하는 방법 |
US5976337A (en) * | 1997-10-27 | 1999-11-02 | Allison Engine Company | Method for electrophoretic deposition of brazing material |
US6273682B1 (en) * | 1999-08-23 | 2001-08-14 | General Electric Company | Turbine blade with preferentially-cooled trailing edge pressure wall |
US6602047B1 (en) | 2002-02-28 | 2003-08-05 | General Electric Company | Methods and apparatus for cooling gas turbine nozzles |
US7080971B2 (en) * | 2003-03-12 | 2006-07-25 | Florida Turbine Technologies, Inc. | Cooled turbine spar shell blade construction |
US6890154B2 (en) | 2003-08-08 | 2005-05-10 | United Technologies Corporation | Microcircuit cooling for a turbine blade |
US7008179B2 (en) | 2003-12-16 | 2006-03-07 | General Electric Co. | Turbine blade frequency tuned pin bank |
ATE513980T1 (de) | 2004-12-24 | 2011-07-15 | Alstom Technology Ltd | Verfahren zur herstellung eines bauteils mit eingebettetem kanal sowie bauteil |
JP2006242050A (ja) * | 2005-03-02 | 2006-09-14 | Mitsubishi Heavy Ind Ltd | ガスタービンの翼冷却構造 |
US7293688B2 (en) * | 2005-11-14 | 2007-11-13 | General Electric Company | Gold/nickel/copper/aluminum/silver brazing alloys for brazing WC-Co to titanium alloys |
US8703044B2 (en) * | 2006-01-03 | 2014-04-22 | General Electric Company | Machine components and methods of fabricating and repairing |
US7900458B2 (en) | 2007-05-29 | 2011-03-08 | Siemens Energy, Inc. | Turbine airfoils with near surface cooling passages and method of making same |
JP4929097B2 (ja) * | 2007-08-08 | 2012-05-09 | 株式会社日立製作所 | ガスタービン翼 |
US8348614B2 (en) | 2008-07-14 | 2013-01-08 | United Technologies Corporation | Coolable airfoil trailing edge passage |
US8573949B2 (en) * | 2009-09-30 | 2013-11-05 | General Electric Company | Method and system for focused energy brazing |
US20110110790A1 (en) * | 2009-11-10 | 2011-05-12 | General Electric Company | Heat shield |
US9528382B2 (en) * | 2009-11-10 | 2016-12-27 | General Electric Company | Airfoil heat shield |
US8535004B2 (en) * | 2010-03-26 | 2013-09-17 | Siemens Energy, Inc. | Four-wall turbine airfoil with thermal strain control for reduced cycle fatigue |
US8714909B2 (en) * | 2010-12-22 | 2014-05-06 | United Technologies Corporation | Platform with cooling circuit |
US10060264B2 (en) * | 2010-12-30 | 2018-08-28 | Rolls-Royce North American Technologies Inc. | Gas turbine engine and cooled flowpath component therefor |
US8734111B2 (en) * | 2011-06-27 | 2014-05-27 | General Electric Company | Platform cooling passages and methods for creating platform cooling passages in turbine rotor blades |
-
2013
- 2013-10-04 US US14/046,437 patent/US9458725B2/en active Active
-
2014
- 2014-09-30 DE DE201410114240 patent/DE102014114240A1/de active Pending
- 2014-10-01 CH CH01492/14A patent/CH708700A8/de not_active Application Discontinuation
- 2014-10-02 JP JP2014203537A patent/JP6431737B2/ja active Active
Also Published As
Publication number | Publication date |
---|---|
JP6431737B2 (ja) | 2018-11-28 |
US20150096305A1 (en) | 2015-04-09 |
CH708700A2 (de) | 2015-04-15 |
JP2015075107A (ja) | 2015-04-20 |
US9458725B2 (en) | 2016-10-04 |
DE102014114240A1 (de) | 2015-04-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CH708700A8 (de) | System zur Schaffung einer Kühlung für Turbinenkomponenten. | |
Khachatryan et al. | Observation of Y (1S) pair production in proton-proton collisions at $$\sqrt {s}= 8$$ TeV | |
CL2018001790A1 (es) | Procesos para preparar un inhibidor de jak1 y nuevas formas de este (divisional solicitud 201602748) | |
WO2017218707A3 (en) | Bispecific checkpoint inhibitor antibodies | |
CO2017006813A2 (es) | Composiciones inhibidoras de corrosion para tratamientos acidificantes | |
EA201891344A1 (ru) | Новые агонисты рецептора апелина и способы применения | |
TR201907981T4 (tr) | Heteroaromatik bileşikler ve bunların dopamin d1 ligandları olarak kullanımı. | |
PL425935A1 (pl) | Kompozycja katalityczna zawierająca nikiel, ligand typu fosfinowego oraz zasadę Lewisa oraz jej zastosowanie w sposobie oligomeryzacji olefin | |
EA201891246A1 (ru) | Способ маркирования подложки | |
MX2018008815A (es) | Inhibidores de tirosina quinasa de bruton. | |
FR3030708B1 (fr) | Plaque froide, formant notamment partie structurale d'un equipement a composants generateurs de chaleur | |
BR112016006770A2 (pt) | fração de gasóleo derivado de fischer-tropsch, formulação de fluido funcional, e, uso de uma fração de gasóleo derivado de fischer-tropsch | |
CR20170514A (es) | Combinaciones herbicidas que comprenden l-glufosinato e indiziflam. | |
AR108988A1 (es) | Procedimiento de fabricación de briquetas que contienen un compuesto calcio-magnesiano y un compuesto a base de hierro, y briquetas así obtenidas | |
BR112018000594A2 (pt) | composições nutricionais compreendendo caseína hidrolisada | |
EA201690244A1 (ru) | Ингибиторы киназ на основе простых ариловых эфиров | |
SA516380560B1 (ar) | وصلة ملولبة لتجهيزات أنبوبية تستخدم في الدول المنتجة للزيت وتركيب طلية قابلة للمعالجة ضوئياً | |
WO2016057683A3 (en) | Novel anti-nodal antibodies and methods of using same | |
WO2018104285A3 (de) | Additive für flüssigkristallmischungen | |
EA201691549A1 (ru) | Ариллактамные ингибиторы киназы | |
EA201790777A1 (ru) | Дерматологический набор, включающий композиции на основе цветка гибискуса и масла бурити | |
MX2017002015A (es) | Ligando del receptor 2 de canabinoide radiomarcado. | |
MX2016001772A (es) | Elemento de friccion. | |
BR112017004962A2 (pt) | processos e dispositivos de gestão de transações compósitas | |
IN2013CH06085A (de) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PK | Correction |
Free format text: BERICHTIGUNG ERFINDER |
|
PK | Correction |
Free format text: ERFINDER BERICHTIGT. |
|
NV | New agent |
Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH |
|
AZW | Rejection (application) |