JP2004515703A5 - - Google Patents
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- Publication number
- JP2004515703A5 JP2004515703A5 JP2002550221A JP2002550221A JP2004515703A5 JP 2004515703 A5 JP2004515703 A5 JP 2004515703A5 JP 2002550221 A JP2002550221 A JP 2002550221A JP 2002550221 A JP2002550221 A JP 2002550221A JP 2004515703 A5 JP2004515703 A5 JP 2004515703A5
- Authority
- JP
- Japan
- 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 |
|---|---|---|---|
| IT2000MI002719A IT1319552B1 (it) | 2000-12-15 | 2000-12-15 | Sistema per adduzione di aria di raffreddamento in una turbina a gas |
| PCT/EP2001/014709 WO2002048525A2 (en) | 2000-12-15 | 2001-12-05 | System to feed cooling air into a gas turbine rotor |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2004515703A JP2004515703A (ja) | 2004-05-27 |
| JP2004515703A5 true JP2004515703A5 (ja) | 2005-12-22 |
| JP4111827B2 JP4111827B2 (ja) | 2008-07-02 |
Family
ID=11446240
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2002550221A Expired - Lifetime JP4111827B2 (ja) | 2000-12-15 | 2001-12-05 | 冷却空気をガスタービンに供給するためのシステム |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US6923005B2 (ja) |
| EP (1) | EP1343950B1 (ja) |
| JP (1) | JP4111827B2 (ja) |
| KR (1) | KR100779286B1 (ja) |
| AU (1) | AU2002234569A1 (ja) |
| CA (1) | CA2430739C (ja) |
| DE (1) | DE60104722T2 (ja) |
| IT (1) | IT1319552B1 (ja) |
| RU (1) | RU2287072C2 (ja) |
| WO (1) | WO2002048525A2 (ja) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2408548A (en) * | 2003-11-25 | 2005-06-01 | Alstom Technology Ltd | Finned seals for turbomachinery |
| US7914253B2 (en) * | 2007-05-01 | 2011-03-29 | General Electric Company | System for regulating a cooling fluid within a turbomachine |
| EP2431574A1 (en) | 2010-09-20 | 2012-03-21 | Siemens Aktiengesellschaft | Gas turbine and method for operating a gas turbine |
| US8529195B2 (en) | 2010-10-12 | 2013-09-10 | General Electric Company | Inducer for gas turbine system |
| FR2983908B1 (fr) | 2011-12-08 | 2015-02-20 | Snecma | Systeme pour assurer l’etancheite entre une enceinte d’huile et un volume exterieur attenant et turbomachine equipee d’un tel systeme d’etancheite. |
| US10107128B2 (en) * | 2015-08-20 | 2018-10-23 | United Technologies Corporation | Cooling channels for gas turbine engine component |
| PL417315A1 (pl) | 2016-05-25 | 2017-12-04 | General Electric Company | Silnik turbinowy z zawirowywaczem |
| US10316681B2 (en) | 2016-05-31 | 2019-06-11 | General Electric Company | System and method for domestic bleed circuit seals within a turbine |
| US11421597B2 (en) | 2019-10-18 | 2022-08-23 | Pratt & Whitney Canada Corp. | Tangential on-board injector (TOBI) assembly |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4296599A (en) * | 1979-03-30 | 1981-10-27 | General Electric Company | Turbine cooling air modulation apparatus |
| US4541774A (en) * | 1980-05-01 | 1985-09-17 | General Electric Company | Turbine cooling air deswirler |
| US4416111A (en) | 1981-02-25 | 1983-11-22 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Air modulation apparatus |
| US4541744A (en) * | 1984-11-15 | 1985-09-17 | General Motors Coporation | Unitized bearing assembly with moldable race members and labryinth seal |
| US4674955A (en) * | 1984-12-21 | 1987-06-23 | The Garrett Corporation | Radial inboard preswirl system |
| FR2712029B1 (fr) * | 1993-11-03 | 1995-12-08 | Snecma | Turbomachine pourvue d'un moyen de réchauffage des disques de turbines aux montées en régime. |
| US5555721A (en) * | 1994-09-28 | 1996-09-17 | General Electric Company | Gas turbine engine cooling supply circuit |
| US6540477B2 (en) * | 2001-05-21 | 2003-04-01 | General Electric Company | Turbine cooling circuit |
-
2000
- 2000-12-15 IT IT2000MI002719A patent/IT1319552B1/it active
-
2001
- 2001-12-05 RU RU2003121392/06A patent/RU2287072C2/ru active
- 2001-12-05 EP EP01985399A patent/EP1343950B1/en not_active Expired - Lifetime
- 2001-12-05 DE DE60104722T patent/DE60104722T2/de not_active Expired - Lifetime
- 2001-12-05 AU AU2002234569A patent/AU2002234569A1/en not_active Abandoned
- 2001-12-05 WO PCT/EP2001/014709 patent/WO2002048525A2/en active IP Right Grant
- 2001-12-05 KR KR1020037007885A patent/KR100779286B1/ko active IP Right Grant
- 2001-12-05 US US10/450,263 patent/US6923005B2/en not_active Expired - Lifetime
- 2001-12-05 JP JP2002550221A patent/JP4111827B2/ja not_active Expired - Lifetime
- 2001-12-05 CA CA002430739A patent/CA2430739C/en not_active Expired - Fee Related