JP2013256948A5 - - Google Patents
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- Publication number
- JP2013256948A5 JP2013256948A5 JP2013120423A JP2013120423A JP2013256948A5 JP 2013256948 A5 JP2013256948 A5 JP 2013256948A5 JP 2013120423 A JP2013120423 A JP 2013120423A JP 2013120423 A JP2013120423 A JP 2013120423A JP 2013256948 A5 JP2013256948 A5 JP 2013256948A5
- Authority
- JP
- Japan
- Prior art keywords
- cavity
- temperature
- thermally responsive
- flow
- actuation assembly
- 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.)
- Granted
Links
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/494,688 US9028206B2 (en) | 2012-06-12 | 2012-06-12 | Thermally actuated assembly for a gas turbine system and method of controlling a cooling airflow path |
| US13/494,688 | 2012-06-12 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2013256948A JP2013256948A (ja) | 2013-12-26 |
| JP2013256948A5 true JP2013256948A5 (enExample) | 2016-07-14 |
| JP6132667B2 JP6132667B2 (ja) | 2017-05-24 |
Family
ID=48578876
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2013120423A Expired - Fee Related JP6132667B2 (ja) | 2012-06-12 | 2013-06-07 | ガスタービンシステム用の熱応答作動組立体および冷却空気流路を制御する方法 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9028206B2 (enExample) |
| EP (1) | EP2674594B1 (enExample) |
| JP (1) | JP6132667B2 (enExample) |
| CN (1) | CN103485894B (enExample) |
| RU (1) | RU2618791C2 (enExample) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10337343B2 (en) | 2015-08-13 | 2019-07-02 | General Electric Company | Turbine component surface cooling system with passive flow modulation |
| US20170191373A1 (en) * | 2015-12-30 | 2017-07-06 | General Electric Company | Passive flow modulation of cooling flow into a cavity |
| US10337411B2 (en) | 2015-12-30 | 2019-07-02 | General Electric Company | Auto thermal valve (ATV) for dual mode passive cooling flow modulation |
| US20170191372A1 (en) * | 2015-12-30 | 2017-07-06 | General Electric Company | Passive flow modulation of cooling flow with telemetry |
| US10335900B2 (en) | 2016-03-03 | 2019-07-02 | General Electric Company | Protective shield for liquid guided laser cutting tools |
| US10337739B2 (en) | 2016-08-16 | 2019-07-02 | General Electric Company | Combustion bypass passive valve system for a gas turbine |
| GB2553144B (en) * | 2016-08-26 | 2019-10-30 | Rolls Royce Plc | Apparatus for insertion into a cavity of an object |
| GB201615429D0 (en) * | 2016-09-12 | 2016-10-26 | Rolls Royce Plc | Apparatus for insertion into a cavity of an object |
| US20180135531A1 (en) * | 2016-11-15 | 2018-05-17 | General Electric Company | Auto-thermal valve for passively controlling fuel flow to axial fuel stage of gas turbine |
| US10712007B2 (en) | 2017-01-27 | 2020-07-14 | General Electric Company | Pneumatically-actuated fuel nozzle air flow modulator |
| US10738712B2 (en) | 2017-01-27 | 2020-08-11 | General Electric Company | Pneumatically-actuated bypass valve |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2620123A (en) * | 1946-05-31 | 1952-12-02 | Continental Aviat & Engineerin | Cooling system for combustion gas turbines |
| JPS5226040A (en) * | 1975-08-22 | 1977-02-26 | Osaka Gas Co Ltd | Heat transfer pipe |
| JPS6163572U (enExample) * | 1984-09-29 | 1986-04-30 | ||
| JPS6272975A (ja) * | 1985-09-20 | 1987-04-03 | Tlv Co Ltd | 熱感応型流量調節弁 |
| JPS6387381U (enExample) * | 1986-11-28 | 1988-06-07 | ||
| JPS63124507U (enExample) * | 1987-02-06 | 1988-08-15 | ||
| JPH02125188A (ja) * | 1988-11-02 | 1990-05-14 | Eagle Ind Co Ltd | 二重感温式遮断弁 |
| US5022817A (en) * | 1989-09-12 | 1991-06-11 | Allied-Signal Inc. | Thermostatic control of turbine cooling air |
| RU21951U1 (ru) * | 2001-10-17 | 2002-02-27 | Открытое акционерное общество "Энергомашкорпорация" | Теплообменник |
| RU2224901C1 (ru) * | 2002-05-31 | 2004-02-27 | Открытое акционерное общество "Энергомашкорпорация" | Газотурбинная установка |
| US7445424B1 (en) * | 2006-04-22 | 2008-11-04 | Florida Turbine Technologies, Inc. | Passive thermostatic bypass flow control for a brush seal application |
| US7900438B2 (en) * | 2006-07-28 | 2011-03-08 | General Electric Company | Heat transfer system and method for turbine engine using heat pipes |
| GB0722511D0 (en) * | 2007-11-19 | 2007-12-27 | Rolls Royce Plc | Turbine arrangement |
| JP5341457B2 (ja) * | 2008-01-15 | 2013-11-13 | 株式会社東芝 | 高温部品の欠陥補修方法及び高温部品 |
| US8549864B2 (en) * | 2010-01-07 | 2013-10-08 | General Electric Company | Temperature activated valves for gas turbines |
| US8684660B2 (en) * | 2011-06-20 | 2014-04-01 | General Electric Company | Pressure and temperature actuation system |
-
2012
- 2012-06-12 US US13/494,688 patent/US9028206B2/en not_active Expired - Fee Related
-
2013
- 2013-06-07 JP JP2013120423A patent/JP6132667B2/ja not_active Expired - Fee Related
- 2013-06-11 RU RU2013126595A patent/RU2618791C2/ru not_active IP Right Cessation
- 2013-06-11 EP EP13171409.9A patent/EP2674594B1/en not_active Not-in-force
- 2013-06-13 CN CN201310232346.XA patent/CN103485894B/zh not_active Expired - Fee Related
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