JP2014528538A5 - - Google Patents
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- JP2014528538A5 JP2014528538A5 JP2014533563A JP2014533563A JP2014528538A5 JP 2014528538 A5 JP2014528538 A5 JP 2014528538A5 JP 2014533563 A JP2014533563 A JP 2014533563A JP 2014533563 A JP2014533563 A JP 2014533563A JP 2014528538 A5 JP2014528538 A5 JP 2014528538A5
- Authority
- JP
- Japan
- Prior art keywords
- chamber
- downpass
- fluid communication
- cavity
- central
- 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.)
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Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/250,345 US9033652B2 (en) | 2011-09-30 | 2011-09-30 | Method and apparatus for cooling gas turbine rotor blades |
| US13/250,345 | 2011-09-30 | ||
| PCT/US2012/054563 WO2013048715A1 (en) | 2011-09-30 | 2012-09-11 | Method and apparatus for cooling gas turbine rotor blades |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2014528538A JP2014528538A (ja) | 2014-10-27 |
| JP2014528538A5 true JP2014528538A5 (enExample) | 2015-11-05 |
| JP6165740B2 JP6165740B2 (ja) | 2017-07-19 |
Family
ID=46968365
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2014533563A Expired - Fee Related JP6165740B2 (ja) | 2011-09-30 | 2012-09-11 | ガスタービンロータブレードを冷却する方法及び装置 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US9033652B2 (enExample) |
| EP (1) | EP2761138A1 (enExample) |
| JP (1) | JP6165740B2 (enExample) |
| CN (1) | CN103857881B (enExample) |
| CA (1) | CA2848867C (enExample) |
| WO (1) | WO2013048715A1 (enExample) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9995148B2 (en) | 2012-10-04 | 2018-06-12 | General Electric Company | Method and apparatus for cooling gas turbine and rotor blades |
| US9581028B1 (en) * | 2014-02-24 | 2017-02-28 | Florida Turbine Technologies, Inc. | Small turbine stator vane with impingement cooling insert |
| EP2993301B1 (en) * | 2014-08-28 | 2024-01-17 | RTX Corporation | Gas turbine engine structure, gas turbine engine and method for passing a coolant through a flow path in a gas turbine engine |
| US10029299B2 (en) | 2015-07-09 | 2018-07-24 | General Electric Company | Three-dimensional manufacturing methods and systems for turbine components |
| US10030526B2 (en) * | 2015-12-21 | 2018-07-24 | General Electric Company | Platform core feed for a multi-wall blade |
| US20170234141A1 (en) * | 2016-02-16 | 2017-08-17 | General Electric Company | Airfoil having crossover holes |
| US10480327B2 (en) * | 2017-01-03 | 2019-11-19 | General Electric Company | Components having channels for impingement cooling |
| FR3067388B1 (fr) * | 2017-04-10 | 2020-01-17 | Safran | Aube a circuit de refroidissement perfectionne |
| US10570748B2 (en) * | 2018-01-10 | 2020-02-25 | United Technologies Corporation | Impingement cooling arrangement for airfoils |
| US10837293B2 (en) * | 2018-07-19 | 2020-11-17 | General Electric Company | Airfoil with tunable cooling configuration |
| US10934854B2 (en) * | 2018-09-11 | 2021-03-02 | General Electric Company | CMC component cooling cavities |
Family Cites Families (30)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4270883A (en) | 1977-04-20 | 1981-06-02 | The Garrett Corporation | Laminated airfoil |
| GB2246174B (en) * | 1982-06-29 | 1992-04-15 | Rolls Royce | A cooled aerofoil for a gas turbine engine |
| US5484258A (en) | 1994-03-01 | 1996-01-16 | General Electric Company | Turbine airfoil with convectively cooled double shell outer wall |
| US5702232A (en) | 1994-12-13 | 1997-12-30 | United Technologies Corporation | Cooled airfoils for a gas turbine engine |
| US5931638A (en) | 1997-08-07 | 1999-08-03 | United Technologies Corporation | Turbomachinery airfoil with optimized heat transfer |
| US6220817B1 (en) | 1997-11-17 | 2001-04-24 | General Electric Company | AFT flowing multi-tier airfoil cooling circuit |
| US6036441A (en) | 1998-11-16 | 2000-03-14 | General Electric Company | Series impingement cooled airfoil |
| US6431832B1 (en) * | 2000-10-12 | 2002-08-13 | Solar Turbines Incorporated | Gas turbine engine airfoils with improved cooling |
| FR2829174B1 (fr) | 2001-08-28 | 2006-01-20 | Snecma Moteurs | Perfectionnement apportes aux circuits de refroidissement pour aube de turbine a gaz |
| US7104757B2 (en) | 2003-07-29 | 2006-09-12 | Siemens Aktiengesellschaft | Cooled turbine blade |
| US7097426B2 (en) | 2004-04-08 | 2006-08-29 | General Electric Company | Cascade impingement cooled airfoil |
| US7377746B2 (en) | 2005-02-21 | 2008-05-27 | General Electric Company | Airfoil cooling circuits and method |
| US7416390B2 (en) | 2005-03-29 | 2008-08-26 | Siemens Power Generation, Inc. | Turbine blade leading edge cooling system |
| US7413407B2 (en) * | 2005-03-29 | 2008-08-19 | Siemens Power Generation, Inc. | Turbine blade cooling system with bifurcated mid-chord cooling chamber |
| US7303376B2 (en) | 2005-12-02 | 2007-12-04 | Siemens Power Generation, Inc. | Turbine airfoil with outer wall cooling system and inner mid-chord hot gas receiving cavity |
| US7296973B2 (en) | 2005-12-05 | 2007-11-20 | General Electric Company | Parallel serpentine cooled blade |
| US7534089B2 (en) * | 2006-07-18 | 2009-05-19 | Siemens Energy, Inc. | Turbine airfoil with near wall multi-serpentine cooling channels |
| US7780413B2 (en) | 2006-08-01 | 2010-08-24 | Siemens Energy, Inc. | Turbine airfoil with near wall inflow chambers |
| US7866948B1 (en) * | 2006-08-16 | 2011-01-11 | Florida Turbine Technologies, Inc. | Turbine airfoil with near-wall impingement and vortex cooling |
| GB2443638B (en) | 2006-11-09 | 2008-11-26 | Rolls Royce Plc | An air-cooled aerofoil |
| US7568887B1 (en) * | 2006-11-16 | 2009-08-04 | Florida Turbine Technologies, Inc. | Turbine blade with near wall spiral flow serpentine cooling circuit |
| US7624787B2 (en) | 2006-12-06 | 2009-12-01 | General Electric Company | Disposable insert, and use thereof in a method for manufacturing an airfoil |
| US7938168B2 (en) | 2006-12-06 | 2011-05-10 | General Electric Company | Ceramic cores, methods of manufacture thereof and articles manufactured from the same |
| US7766618B1 (en) | 2007-06-21 | 2010-08-03 | Florida Turbine Technologies, Inc. | Turbine vane endwall with cascading film cooling diffusion slots |
| US7857589B1 (en) * | 2007-09-21 | 2010-12-28 | Florida Turbine Technologies, Inc. | Turbine airfoil with near-wall cooling |
| US7950903B1 (en) | 2007-12-21 | 2011-05-31 | Florida Turbine Technologies, Inc. | Turbine blade with dual serpentine cooling |
| US7901183B1 (en) | 2008-01-22 | 2011-03-08 | Florida Turbine Technologies, Inc. | Turbine blade with dual aft flowing triple pass serpentines |
| US8231329B2 (en) | 2008-12-30 | 2012-07-31 | General Electric Company | Turbine blade cooling with a hollow airfoil configured to minimize a distance between a pin array section and the trailing edge of the air foil |
| US8182223B2 (en) | 2009-02-27 | 2012-05-22 | General Electric Company | Turbine blade cooling |
| US8016564B1 (en) | 2009-04-09 | 2011-09-13 | Florida Turbine Technologies, Inc. | Turbine blade with leading edge impingement cooling |
-
2011
- 2011-09-30 US US13/250,345 patent/US9033652B2/en active Active
-
2012
- 2012-09-11 WO PCT/US2012/054563 patent/WO2013048715A1/en not_active Ceased
- 2012-09-11 CN CN201280047834.7A patent/CN103857881B/zh active Active
- 2012-09-11 EP EP12767153.5A patent/EP2761138A1/en not_active Withdrawn
- 2012-09-11 CA CA2848867A patent/CA2848867C/en not_active Expired - Fee Related
- 2012-09-11 JP JP2014533563A patent/JP6165740B2/ja not_active Expired - Fee Related
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