RU2430240C2 - Турбинная лопатка и способ ее изготовления - Google Patents
Турбинная лопатка и способ ее изготовления Download PDFInfo
- Publication number
- RU2430240C2 RU2430240C2 RU2009132675/06A RU2009132675A RU2430240C2 RU 2430240 C2 RU2430240 C2 RU 2430240C2 RU 2009132675/06 A RU2009132675/06 A RU 2009132675/06A RU 2009132675 A RU2009132675 A RU 2009132675A RU 2430240 C2 RU2430240 C2 RU 2430240C2
- Authority
- RU
- Russia
- Prior art keywords
- support structure
- shell
- turbine blade
- blade
- cooling
- Prior art date
Links
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 8
- 238000000034 method Methods 0.000 title abstract description 9
- 238000001816 cooling Methods 0.000 claims abstract description 42
- 125000006850 spacer group Chemical group 0.000 claims abstract description 26
- 229910000679 solder Inorganic materials 0.000 claims abstract description 23
- 239000002826 coolant Substances 0.000 claims abstract description 16
- 238000005476 soldering Methods 0.000 claims abstract description 6
- 230000008093 supporting effect Effects 0.000 claims description 15
- 238000009826 distribution Methods 0.000 claims description 3
- 230000015572 biosynthetic process Effects 0.000 claims description 2
- 239000000155 melt Substances 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 2
- 239000000126 substance Substances 0.000 abstract 1
- 238000005219 brazing Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 238000004870 electrical engineering Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000003203 everyday effect Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Images
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
- F01D5/181—Blades having a closed internal cavity containing a cooling medium, e.g. sodium
-
- 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
-
- 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
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
- F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
- F05D2230/237—Brazing
-
- 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
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
- F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
- F05D2230/238—Soldering
-
- 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
- F05D2240/20—Rotors
- F05D2240/24—Rotors for turbines
- F05D2240/241—Rotors for turbines of impulse type
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49339—Hollow blade
- Y10T29/49341—Hollow blade with cooling passage
Landscapes
- Engineering & Computer Science (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 |
|---|---|---|---|
| EP07002215.7 | 2007-02-01 | ||
| EP07002215A EP1953342A1 (de) | 2007-02-01 | 2007-02-01 | Turbinenschaufel |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2009132675A RU2009132675A (ru) | 2011-03-10 |
| RU2430240C2 true RU2430240C2 (ru) | 2011-09-27 |
Family
ID=38193432
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2009132675/06A RU2430240C2 (ru) | 2007-02-01 | 2008-01-14 | Турбинная лопатка и способ ее изготовления |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US8267659B2 (enExample) |
| EP (2) | EP1953342A1 (enExample) |
| JP (1) | JP4959811B2 (enExample) |
| CN (1) | CN101600853B (enExample) |
| RU (1) | RU2430240C2 (enExample) |
| WO (1) | WO2008092725A1 (enExample) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7871246B2 (en) * | 2007-02-15 | 2011-01-18 | Siemens Energy, Inc. | Airfoil for a gas turbine |
| US8753083B2 (en) * | 2011-01-14 | 2014-06-17 | General Electric Company | Curved cooling passages for a turbine component |
| US8875870B2 (en) | 2011-03-31 | 2014-11-04 | Benetech, Inc. | Conveyor belt cleaner scraper blade and assembly |
| CN103061827B (zh) * | 2013-01-06 | 2015-05-06 | 北京航空航天大学 | 一种混合型陶瓷基复合材料涡轮导向器叶片 |
| EP3075531B1 (en) | 2015-03-31 | 2024-03-20 | Ansaldo Energia IP UK Limited | Sandwich arrangement with ceramic panels and ceramic felts |
| EP3115199A1 (en) | 2015-07-10 | 2017-01-11 | General Electric Technology GmbH | Manufacturing of single or multiple panels |
| CN105397223A (zh) * | 2015-12-25 | 2016-03-16 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种吸附式空心静子叶片的制造方法 |
| US10436048B2 (en) * | 2016-08-12 | 2019-10-08 | General Electric Comapny | Systems for removing heat from turbine components |
| US11333022B2 (en) * | 2019-08-06 | 2022-05-17 | General Electric Company | Airfoil with thermally conductive pins |
| US11203947B2 (en) * | 2020-05-08 | 2021-12-21 | Raytheon Technologies Corporation | Airfoil having internally cooled wall with liner and shell |
| CN112610285B (zh) * | 2020-12-18 | 2021-09-14 | 武汉大学 | 一种仿金刚石晶胞拓扑的汽轮机空心静叶强化除湿结构及汽轮机除湿装置 |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2642263A (en) * | 1951-01-05 | 1953-06-16 | Westinghouse Electric Corp | Blade apparatus |
| US2801073A (en) * | 1952-06-30 | 1957-07-30 | United Aircraft Corp | Hollow sheet metal blade or vane construction |
| US5328331A (en) * | 1993-06-28 | 1994-07-12 | General Electric Company | Turbine airfoil with double shell outer wall |
| EP0974735A2 (en) * | 1998-07-20 | 2000-01-26 | General Electric Company | Dimpled impingement baffle |
| RU2154169C2 (ru) * | 1998-11-10 | 2000-08-10 | Ао "К.Т.С." | Перо оболочковой турбинной лопатки "флокс 2" |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2906495A (en) * | 1955-04-29 | 1959-09-29 | Eugene F Schum | Turbine blade with corrugated strut |
| US3700348A (en) * | 1968-08-13 | 1972-10-24 | Gen Electric | Turbomachinery blade structure |
| US3806276A (en) * | 1972-08-30 | 1974-04-23 | Gen Motors Corp | Cooled turbine blade |
| JPS52139903A (en) * | 1976-05-18 | 1977-11-22 | Toyo Electric Mfg Co Ltd | Commutator manufacturing method |
| JPS55109704A (en) * | 1979-02-19 | 1980-08-23 | Hitachi Ltd | Gas-turbine blade capable of being cooled |
| JP3110227B2 (ja) * | 1993-11-22 | 2000-11-20 | 株式会社東芝 | タービン冷却翼 |
| DE19737845C2 (de) * | 1997-08-29 | 1999-12-02 | Siemens Ag | Verfahren zum Herstellen einer Gasturbinenschaufel, sowie nach dem Verfahren hergestellte Gasturbinenschaufel |
| US6238182B1 (en) * | 1999-02-19 | 2001-05-29 | Meyer Tool, Inc. | Joint for a turbine component |
| US6508000B2 (en) * | 2001-02-08 | 2003-01-21 | Siemens Westinghouse Power Corporation | Transient liquid phase bonding repair for advanced turbine blades and vanes |
| EP1533481A3 (en) * | 2003-11-19 | 2009-11-04 | General Electric Company | Hot gas path component with a meshed and dimpled cooling structure |
| 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 |
-
2007
- 2007-02-01 EP EP07002215A patent/EP1953342A1/de not_active Withdrawn
-
2008
- 2008-01-14 WO PCT/EP2008/050325 patent/WO2008092725A1/de not_active Ceased
- 2008-01-14 RU RU2009132675/06A patent/RU2430240C2/ru not_active IP Right Cessation
- 2008-01-14 EP EP08701454A patent/EP2126286A1/de not_active Withdrawn
- 2008-01-14 CN CN200880003931XA patent/CN101600853B/zh not_active Expired - Fee Related
- 2008-01-14 JP JP2009547622A patent/JP4959811B2/ja not_active Expired - Fee Related
- 2008-01-14 US US12/525,156 patent/US8267659B2/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2642263A (en) * | 1951-01-05 | 1953-06-16 | Westinghouse Electric Corp | Blade apparatus |
| US2801073A (en) * | 1952-06-30 | 1957-07-30 | United Aircraft Corp | Hollow sheet metal blade or vane construction |
| US5328331A (en) * | 1993-06-28 | 1994-07-12 | General Electric Company | Turbine airfoil with double shell outer wall |
| EP0974735A2 (en) * | 1998-07-20 | 2000-01-26 | General Electric Company | Dimpled impingement baffle |
| RU2154169C2 (ru) * | 1998-11-10 | 2000-08-10 | Ао "К.Т.С." | Перо оболочковой турбинной лопатки "флокс 2" |
Also Published As
| Publication number | Publication date |
|---|---|
| EP2126286A1 (de) | 2009-12-02 |
| JP4959811B2 (ja) | 2012-06-27 |
| US8267659B2 (en) | 2012-09-18 |
| JP2010518300A (ja) | 2010-05-27 |
| EP1953342A1 (de) | 2008-08-06 |
| RU2009132675A (ru) | 2011-03-10 |
| CN101600853B (zh) | 2013-09-11 |
| US20090324421A1 (en) | 2009-12-31 |
| WO2008092725A1 (de) | 2008-08-07 |
| CN101600853A (zh) | 2009-12-09 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20150115 |