RU2007132534A - Стенка с пазом с пленочным охлаждением и способ ее производства - Google Patents
Стенка с пазом с пленочным охлаждением и способ ее производства Download PDFInfo
- Publication number
- RU2007132534A RU2007132534A RU2007132534/06A RU2007132534A RU2007132534A RU 2007132534 A RU2007132534 A RU 2007132534A RU 2007132534/06 A RU2007132534/06 A RU 2007132534/06A RU 2007132534 A RU2007132534 A RU 2007132534A RU 2007132534 A RU2007132534 A RU 2007132534A
- Authority
- RU
- Russia
- Prior art keywords
- product according
- film
- substrate
- side wall
- shape
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—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
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
- Y10T428/24298—Noncircular aperture [e.g., slit, diamond, rectangular, etc.]
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
- Y10T428/24322—Composite web or sheet
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Processing Of Stones Or Stones Resemblance Materials (AREA)
- Structure Of Printed Boards (AREA)
Claims (9)
1. Изделие (10), содержащее
подложку (12), имеющую первую поверхность (14) и вторую поверхность (16);
паз (22), расположенный во второй поверхности (16) и имеющий нижнюю поверхность (28), по существу параллельную второй поверхности (16), первую боковую стенку (24) и вторую боковую стенку (26), причем первая боковая стенка (24) по существу перпендикулярна второй поверхности (16) и содержит множество частей (30) со скошенным краем, физически связанных со второй поверхностью (16) и нижней поверхностью (28); и
множество проходных отверстий (32), проходящих через подложку (12) от первой поверхности (14) к нижней поверхности (28), причем множество проходных отверстий (32) выстроено в пазу (22) таким образом, что, по меньшей мере, одна часть (30) со скошенным краем расположена между двумя проходными отверстиями (32).
2. Изделие по п.1, в котором вторая боковая стенка (26) по существу перпендикулярна второй поверхности (16).
3. Изделие по п.1, в котором, по меньшей мере, одно проходное отверстие (32) из множества проходных отверстий имеет форму диффузора.
4. Изделие по п.1, в котором множество проходных отверстий (32) проходит через подложку под углом.
5. Изделие по п.4, в котором угол составляет от приблизительно 10° до приблизительно 60°.
6. Изделие по п.5, в котором угол составляет от приблизительно 20° до приблизительно 40°.
7. Изделие по п.1, в котором первая поверхность (14) и вторая поверхность (16) находятся друг напротив друга и являются параллельными друг другу.
8. Изделие по п.1, в котором подложка (12) выполнена из керамики или материала на основе металла.
9. Изделие по п.1, в котором части (30) со скошенным краем имеют форму, выбранную из группы, состоящей из формы "ласточкин хвост", формы наклонной буквы V и наклонной прямоугольной формы.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/511,840 | 2006-08-29 | ||
US11/511,840 US7553534B2 (en) | 2006-08-29 | 2006-08-29 | Film cooled slotted wall and method of making the same |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2007132534A true RU2007132534A (ru) | 2009-03-10 |
RU2444634C2 RU2444634C2 (ru) | 2012-03-10 |
Family
ID=38989793
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2007132534/06A RU2444634C2 (ru) | 2006-08-29 | 2007-08-28 | Стенка компонента газотурбинного двигателя |
Country Status (5)
Country | Link |
---|---|
US (1) | US7553534B2 (ru) |
JP (1) | JP5161512B2 (ru) |
KR (1) | KR101355334B1 (ru) |
DE (1) | DE102007038858A1 (ru) |
RU (1) | RU2444634C2 (ru) |
Families Citing this family (55)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7980819B2 (en) * | 2007-03-14 | 2011-07-19 | United Technologies Corporation | Cast features for a turbine engine airfoil |
DE102007029367A1 (de) * | 2007-06-26 | 2009-01-02 | Rolls-Royce Deutschland Ltd & Co Kg | Schaufel mit Tangentialstrahlerzeugung am Profil |
US20090246011A1 (en) * | 2008-03-25 | 2009-10-01 | General Electric Company | Film cooling of turbine components |
JP4898731B2 (ja) * | 2008-03-26 | 2012-03-21 | 三菱重工業株式会社 | ガスタービン冷却構造およびこれを備えたガスタービン |
US8079810B2 (en) * | 2008-09-16 | 2011-12-20 | Siemens Energy, Inc. | Turbine airfoil cooling system with divergent film cooling hole |
DE102008052409A1 (de) * | 2008-10-21 | 2010-04-22 | Rolls-Royce Deutschland Ltd & Co Kg | Strömungsarbeitsmaschine mit saugseitennaher Randenergetisierung |
US20110097188A1 (en) * | 2009-10-23 | 2011-04-28 | General Electric Company | Structure and method for improving film cooling using shallow trench with holes oriented along length of trench |
US9181819B2 (en) | 2010-06-11 | 2015-11-10 | Siemens Energy, Inc. | Component wall having diffusion sections for cooling in a turbine engine |
US8608443B2 (en) | 2010-06-11 | 2013-12-17 | Siemens Energy, Inc. | Film cooled component wall in a turbine engine |
US9028207B2 (en) | 2010-09-23 | 2015-05-12 | Siemens Energy, Inc. | Cooled component wall in a turbine engine |
JP5517163B2 (ja) * | 2010-10-07 | 2014-06-11 | 株式会社日立製作所 | タービン翼の冷却孔加工方法 |
US20120114868A1 (en) * | 2010-11-10 | 2012-05-10 | General Electric Company | Method of fabricating a component using a fugitive coating |
US8727727B2 (en) * | 2010-12-10 | 2014-05-20 | General Electric Company | Components with cooling channels and methods of manufacture |
US20120148769A1 (en) * | 2010-12-13 | 2012-06-14 | General Electric Company | Method of fabricating a component using a two-layer structural coating |
US20120243995A1 (en) * | 2011-03-21 | 2012-09-27 | General Electric Company | Components with cooling channels formed in coating and methods of manufacture |
US8601691B2 (en) * | 2011-04-27 | 2013-12-10 | General Electric Company | Component and methods of fabricating a coated component using multiple types of fillers |
US9327384B2 (en) * | 2011-06-24 | 2016-05-03 | General Electric Company | Components with cooling channels and methods of manufacture |
EP2557269A1 (en) | 2011-08-08 | 2013-02-13 | Siemens Aktiengesellschaft | Film cooling of turbine components |
US20130045106A1 (en) * | 2011-08-15 | 2013-02-21 | General Electric Company | Angled trench diffuser |
EP2597259A1 (de) * | 2011-11-24 | 2013-05-29 | Siemens Aktiengesellschaft | Modifizierte Oberfläche um ein Loch |
US9249670B2 (en) * | 2011-12-15 | 2016-02-02 | General Electric Company | Components with microchannel cooling |
US8870536B2 (en) * | 2012-01-13 | 2014-10-28 | General Electric Company | Airfoil |
US8870535B2 (en) * | 2012-01-13 | 2014-10-28 | General Electric Company | Airfoil |
US9422815B2 (en) | 2012-02-15 | 2016-08-23 | United Technologies Corporation | Gas turbine engine component with compound cusp cooling configuration |
US9273560B2 (en) * | 2012-02-15 | 2016-03-01 | United Technologies Corporation | Gas turbine engine component with multi-lobed cooling hole |
CH706107A1 (de) * | 2012-02-17 | 2013-08-30 | Alstom Technology Ltd | Bauteil für eine thermische Maschine, insbesondere eine Gasturbine. |
US9234438B2 (en) | 2012-05-04 | 2016-01-12 | Siemens Aktiengesellschaft | Turbine engine component wall having branched cooling passages |
US10689986B1 (en) | 2012-06-01 | 2020-06-23 | United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration | High blowing ratio high effectiveness film cooling configurations |
US9080451B2 (en) * | 2012-06-28 | 2015-07-14 | General Electric Company | Airfoil |
US9470096B2 (en) * | 2012-07-26 | 2016-10-18 | General Electric Company | Turbine bucket with notched squealer tip |
DE102013109116A1 (de) * | 2012-08-27 | 2014-03-27 | General Electric Company (N.D.Ges.D. Staates New York) | Bauteil mit Kühlkanälen und Verfahren zur Herstellung |
EP2733310A1 (de) * | 2012-11-16 | 2014-05-21 | Siemens Aktiengesellschaft | Modifizierte Oberfläche um ein Loch |
US9181809B2 (en) * | 2012-12-04 | 2015-11-10 | General Electric Company | Coated article |
EP2941543B1 (en) | 2013-03-13 | 2017-03-22 | Rolls-Royce Corporation | Trenched cooling hole arrangement for a ceramic matrix composite vane |
EP3017148A1 (en) * | 2013-07-03 | 2016-05-11 | General Electric Company | Trench cooling of airfoil structures |
GB201315871D0 (en) | 2013-09-06 | 2013-10-23 | Rolls Royce Plc | A combustion chamber arrangement |
US9441488B1 (en) * | 2013-11-07 | 2016-09-13 | United States Of America As Represented By The Secretary Of The Air Force | Film cooling holes for gas turbine airfoils |
CN103696811A (zh) * | 2013-12-19 | 2014-04-02 | 中国科学院工程热物理研究所 | 一种带条缝出口的涡轮叶片圆孔气膜冷却结构 |
WO2015184294A1 (en) | 2014-05-29 | 2015-12-03 | General Electric Company | Fastback turbulator |
US10364684B2 (en) | 2014-05-29 | 2019-07-30 | General Electric Company | Fastback vorticor pin |
US11280214B2 (en) * | 2014-10-20 | 2022-03-22 | Raytheon Technologies Corporation | Gas turbine engine component |
US10233775B2 (en) | 2014-10-31 | 2019-03-19 | General Electric Company | Engine component for a gas turbine engine |
US10280785B2 (en) | 2014-10-31 | 2019-05-07 | General Electric Company | Shroud assembly for a turbine engine |
US10132166B2 (en) | 2015-02-27 | 2018-11-20 | General Electric Company | Engine component |
US10024169B2 (en) | 2015-02-27 | 2018-07-17 | General Electric Company | Engine component |
US10208602B2 (en) * | 2015-04-27 | 2019-02-19 | United Technologies Corporation | Asymmetric diffuser opening for film cooling holes |
US9752440B2 (en) | 2015-05-29 | 2017-09-05 | General Electric Company | Turbine component having surface cooling channels and method of forming same |
CN105065122A (zh) * | 2015-07-17 | 2015-11-18 | 沈阳航空航天大学 | 一种应用于涡轮叶片气膜冷却的孔-锯齿槽结构 |
US10378444B2 (en) * | 2015-08-19 | 2019-08-13 | General Electric Company | Engine component for a gas turbine engine |
US10488048B2 (en) * | 2016-01-06 | 2019-11-26 | United Technologies Corporation | Weld configuration |
DE102016203388A1 (de) * | 2016-03-02 | 2017-09-07 | Siemens Aktiengesellschaft | Schichtsystem mit Beschichtungsaussparung an Kühlluftlöchern von Turbinenschaufeln |
KR101853550B1 (ko) * | 2016-08-22 | 2018-04-30 | 두산중공업 주식회사 | 가스 터빈 블레이드 |
US10570747B2 (en) * | 2017-10-02 | 2020-02-25 | DOOSAN Heavy Industries Construction Co., LTD | Enhanced film cooling system |
JP6946225B2 (ja) * | 2018-03-29 | 2021-10-06 | 三菱重工業株式会社 | タービン動翼、及びガスタービン |
JP7362997B2 (ja) * | 2021-06-24 | 2023-10-18 | ドゥサン エナービリティー カンパニー リミテッド | タービンブレードおよびこれを含むタービン |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU1466358A1 (ru) * | 1987-04-20 | 1992-10-07 | Ленинградский Кораблестроительный Институт | Лопатка газовой турбины |
US5651662A (en) * | 1992-10-29 | 1997-07-29 | General Electric Company | Film cooled wall |
US5660525A (en) * | 1992-10-29 | 1997-08-26 | General Electric Company | Film cooled slotted wall |
US5419681A (en) * | 1993-01-25 | 1995-05-30 | General Electric Company | Film cooled wall |
EP0851098A3 (en) * | 1996-12-23 | 2000-09-13 | General Electric Company | A method for improving the cooling effectiveness of film cooling holes |
US6383602B1 (en) * | 1996-12-23 | 2002-05-07 | General Electric Company | Method for improving the cooling effectiveness of a gaseous coolant stream which flows through a substrate, and related articles of manufacture |
US6234755B1 (en) * | 1999-10-04 | 2001-05-22 | General Electric Company | Method for improving the cooling effectiveness of a gaseous coolant stream, and related articles of manufacture |
DE50009497D1 (de) * | 2000-11-16 | 2005-03-17 | Siemens Ag | Filmkühlung von Gasturbinenschaufeln mittels Schlitzen für Kühlluft |
JP3997986B2 (ja) * | 2003-12-19 | 2007-10-24 | 株式会社Ihi | 冷却タービン部品、及び冷却タービン翼 |
-
2006
- 2006-08-29 US US11/511,840 patent/US7553534B2/en not_active Expired - Fee Related
-
2007
- 2007-08-16 DE DE102007038858A patent/DE102007038858A1/de not_active Withdrawn
- 2007-08-24 JP JP2007218367A patent/JP5161512B2/ja not_active Expired - Fee Related
- 2007-08-28 RU RU2007132534/06A patent/RU2444634C2/ru not_active IP Right Cessation
- 2007-08-28 KR KR1020070086391A patent/KR101355334B1/ko active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
JP2008057534A (ja) | 2008-03-13 |
US20080057271A1 (en) | 2008-03-06 |
JP5161512B2 (ja) | 2013-03-13 |
RU2444634C2 (ru) | 2012-03-10 |
KR20080021523A (ko) | 2008-03-07 |
DE102007038858A1 (de) | 2008-03-06 |
US7553534B2 (en) | 2009-06-30 |
KR101355334B1 (ko) | 2014-01-23 |
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