TW200728591A - Microcircuits for small engines - Google Patents
Microcircuits for small enginesInfo
- Publication number
- TW200728591A TW200728591A TW095143427A TW95143427A TW200728591A TW 200728591 A TW200728591 A TW 200728591A TW 095143427 A TW095143427 A TW 095143427A TW 95143427 A TW95143427 A TW 95143427A TW 200728591 A TW200728591 A TW 200728591A
- Authority
- TW
- Taiwan
- Prior art keywords
- side wall
- microcircuits
- small engines
- turbine engine
- pressure side
- 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
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/02—Sand moulds or like moulds for shaped castings
- B22C9/04—Use of lost patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
-
- 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
- F01D5/26—Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
-
- 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
- F05D2230/211—Manufacture essentially without removing material by casting by precision casting, e.g. microfusing or investment 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
- F05D2240/00—Components
- F05D2240/80—Platforms for stationary or moving blades
- F05D2240/81—Cooled platforms
-
- 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
- F05D2250/18—Two-dimensional patterned
- F05D2250/185—Two-dimensional patterned serpentine-like
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/344,763 US7695246B2 (en) | 2006-01-31 | 2006-01-31 | Microcircuits for small engines |
Publications (1)
Publication Number | Publication Date |
---|---|
TW200728591A true TW200728591A (en) | 2007-08-01 |
Family
ID=37882071
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
TW095143427A TW200728591A (en) | 2006-01-31 | 2006-11-23 | Microcircuits for small engines |
Country Status (6)
Country | Link |
---|---|
US (2) | US7695246B2 (zh) |
EP (1) | EP1813776B1 (zh) |
JP (1) | JP2007205352A (zh) |
KR (1) | KR20070078974A (zh) |
SG (1) | SG134214A1 (zh) |
TW (1) | TW200728591A (zh) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8157527B2 (en) | 2008-07-03 | 2012-04-17 | United Technologies Corporation | Airfoil with tapered radial cooling passage |
US8348614B2 (en) * | 2008-07-14 | 2013-01-08 | United Technologies Corporation | Coolable airfoil trailing edge passage |
US8572844B2 (en) | 2008-08-29 | 2013-11-05 | United Technologies Corporation | Airfoil with leading edge cooling passage |
US8303252B2 (en) | 2008-10-16 | 2012-11-06 | United Technologies Corporation | Airfoil with cooling passage providing variable heat transfer rate |
US8109725B2 (en) | 2008-12-15 | 2012-02-07 | United Technologies Corporation | Airfoil with wrapped leading edge cooling passage |
US8167558B2 (en) * | 2009-01-19 | 2012-05-01 | Siemens Energy, Inc. | Modular serpentine cooling systems for turbine engine components |
US8167536B2 (en) * | 2009-03-04 | 2012-05-01 | Siemens Energy, Inc. | Turbine blade leading edge tip cooling system |
US8079814B1 (en) * | 2009-04-04 | 2011-12-20 | Florida Turbine Technologies, Inc. | Turbine blade with serpentine flow cooling |
EP2243574A1 (de) * | 2009-04-20 | 2010-10-27 | Siemens Aktiengesellschaft | Giessvorrichtung zum Herstellen einer Turbinenlaufschaufel einer Gasturbine und Turbinenlaufschaufel |
US8079821B2 (en) * | 2009-05-05 | 2011-12-20 | Siemens Energy, Inc. | Turbine airfoil with dual wall formed from inner and outer layers separated by a compliant structure |
US9121290B2 (en) * | 2010-05-06 | 2015-09-01 | United Technologies Corporation | Turbine airfoil with body microcircuits terminating in platform |
US8647064B2 (en) * | 2010-08-09 | 2014-02-11 | General Electric Company | Bucket assembly cooling apparatus and method for forming the bucket assembly |
US8794921B2 (en) * | 2010-09-30 | 2014-08-05 | General Electric Company | Apparatus and methods for cooling platform regions of turbine rotor blades |
US8807945B2 (en) | 2011-06-22 | 2014-08-19 | United Technologies Corporation | Cooling system for turbine airfoil including ice-cream-cone-shaped pedestals |
US8840370B2 (en) * | 2011-11-04 | 2014-09-23 | General Electric Company | Bucket assembly for turbine system |
US9243502B2 (en) | 2012-04-24 | 2016-01-26 | United Technologies Corporation | Airfoil cooling enhancement and method of making the same |
US9296039B2 (en) | 2012-04-24 | 2016-03-29 | United Technologies Corporation | Gas turbine engine airfoil impingement cooling |
US9551228B2 (en) * | 2013-01-09 | 2017-01-24 | United Technologies Corporation | Airfoil and method of making |
WO2014150681A1 (en) * | 2013-03-15 | 2014-09-25 | United Technologies Corporation | Gas turbine engine component having shaped pedestals |
CN105188988A (zh) * | 2013-03-15 | 2015-12-23 | 联合工艺公司 | 具有角半径以减少再结晶的铸造部件 |
WO2015080783A2 (en) | 2013-09-19 | 2015-06-04 | United Technologies Corporation | Gas turbine engine airfoil having serpentine fed platform cooling passage |
US10001013B2 (en) * | 2014-03-06 | 2018-06-19 | General Electric Company | Turbine rotor blades with platform cooling arrangements |
US9752440B2 (en) | 2015-05-29 | 2017-09-05 | General Electric Company | Turbine component having surface cooling channels and method of forming same |
US10677070B2 (en) * | 2015-10-19 | 2020-06-09 | Raytheon Technologies Corporation | Blade platform gusset with internal cooling |
US10156145B2 (en) * | 2015-10-27 | 2018-12-18 | General Electric Company | Turbine bucket having cooling passageway |
US9885243B2 (en) | 2015-10-27 | 2018-02-06 | General Electric Company | Turbine bucket having outlet path in shroud |
US10508554B2 (en) | 2015-10-27 | 2019-12-17 | General Electric Company | Turbine bucket having outlet path in shroud |
KR101866900B1 (ko) * | 2016-05-20 | 2018-06-14 | 한국기계연구원 | 가스 터빈용 블레이드 |
US10808571B2 (en) * | 2017-06-22 | 2020-10-20 | Raytheon Technologies Corporation | Gaspath component including minicore plenums |
US20190085706A1 (en) * | 2017-09-18 | 2019-03-21 | General Electric Company | Turbine engine airfoil assembly |
Family Cites Families (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2820266A (en) * | 1955-03-11 | 1958-01-21 | Everard F Kohl | Shell mold structure |
US4353679A (en) * | 1976-07-29 | 1982-10-12 | General Electric Company | Fluid-cooled element |
DE3310441C1 (de) | 1983-03-23 | 1984-09-06 | Flachglas AG, 8510 Fürth | Anlage fuer die Randversiegelung von Isolierglaseinheiten |
US4596512A (en) * | 1984-08-23 | 1986-06-24 | United Technologies Corporation | Circulation controlled rotor blade tip vent valve |
US5667359A (en) * | 1988-08-24 | 1997-09-16 | United Technologies Corp. | Clearance control for the turbine of a gas turbine engine |
US5622939A (en) * | 1992-08-21 | 1997-04-22 | Alpha-Beta Technology, Inc. | Glucan preparation |
US5813835A (en) * | 1991-08-19 | 1998-09-29 | The United States Of America As Represented By The Secretary Of The Air Force | Air-cooled turbine blade |
US5413458A (en) * | 1994-03-29 | 1995-05-09 | United Technologies Corporation | Turbine vane with a platform cavity having a double feed for cooling fluid |
US5614242A (en) * | 1995-09-27 | 1997-03-25 | Barkley Seed, Inc. | Food ingredients derived from viscous barley grain and the process of making |
US5848876A (en) * | 1997-02-11 | 1998-12-15 | Mitsubishi Heavy Industries, Ltd. | Cooling system for cooling platform of gas turbine moving blade |
JP3411775B2 (ja) * | 1997-03-10 | 2003-06-03 | 三菱重工業株式会社 | ガスタービン動翼 |
JP3457831B2 (ja) * | 1997-03-17 | 2003-10-20 | 三菱重工業株式会社 | ガスタービン動翼の冷却プラットフォーム |
CA2231988C (en) | 1998-03-12 | 2002-05-28 | Mitsubishi Heavy Industries, Ltd. | Gas turbine blade |
US6210111B1 (en) * | 1998-12-21 | 2001-04-03 | United Technologies Corporation | Turbine blade with platform cooling |
US6247896B1 (en) * | 1999-06-23 | 2001-06-19 | United Technologies Corporation | Method and apparatus for cooling an airfoil |
US6168381B1 (en) * | 1999-06-29 | 2001-01-02 | General Electric Company | Airfoil isolated leading edge cooling |
US6390774B1 (en) * | 2000-02-02 | 2002-05-21 | General Electric Company | Gas turbine bucket cooling circuit and related process |
US7011845B2 (en) * | 2000-05-09 | 2006-03-14 | Mcp Hahnemann University | β-glucans encapsulated in liposomes |
US6607356B2 (en) * | 2002-01-11 | 2003-08-19 | General Electric Company | Crossover cooled airfoil trailing edge |
US6932571B2 (en) * | 2003-02-05 | 2005-08-23 | United Technologies Corporation | Microcircuit cooling for a turbine blade tip |
FR2858352B1 (fr) | 2003-08-01 | 2006-01-20 | Snecma Moteurs | Circuit de refroidissement pour aube de turbine |
US7097425B2 (en) | 2003-08-08 | 2006-08-29 | United Technologies Corporation | Microcircuit cooling for a turbine airfoil |
US6887033B1 (en) * | 2003-11-10 | 2005-05-03 | General Electric Company | Cooling system for nozzle segment platform edges |
US7097424B2 (en) * | 2004-02-03 | 2006-08-29 | United Technologies Corporation | Micro-circuit platform |
US7217092B2 (en) * | 2004-04-14 | 2007-05-15 | General Electric Company | Method and apparatus for reducing turbine blade temperatures |
US7144220B2 (en) * | 2004-07-30 | 2006-12-05 | United Technologies Corporation | Investment casting |
US7147439B2 (en) * | 2004-09-15 | 2006-12-12 | General Electric Company | Apparatus and methods for cooling turbine bucket platforms |
US7255536B2 (en) * | 2005-05-23 | 2007-08-14 | United Technologies Corporation | Turbine airfoil platform cooling circuit |
-
2006
- 2006-01-31 US US11/344,763 patent/US7695246B2/en active Active
- 2006-11-23 TW TW095143427A patent/TW200728591A/zh unknown
- 2006-12-12 SG SG200608671-4A patent/SG134214A1/en unknown
- 2006-12-22 KR KR1020060132258A patent/KR20070078974A/ko not_active Application Discontinuation
-
2007
- 2007-01-24 JP JP2007013228A patent/JP2007205352A/ja active Pending
- 2007-01-29 EP EP07250357.6A patent/EP1813776B1/en active Active
-
2010
- 2010-02-24 US US12/711,279 patent/US7988418B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP1813776A2 (en) | 2007-08-01 |
US20100158669A1 (en) | 2010-06-24 |
US7988418B2 (en) | 2011-08-02 |
KR20070078974A (ko) | 2007-08-03 |
JP2007205352A (ja) | 2007-08-16 |
EP1813776A3 (en) | 2011-04-06 |
SG134214A1 (en) | 2007-08-29 |
EP1813776B1 (en) | 2016-03-23 |
US20070177976A1 (en) | 2007-08-02 |
US7695246B2 (en) | 2010-04-13 |
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