RU2004115403A - COOLED TURBINE SHOVEL - Google Patents
COOLED TURBINE SHOVEL Download PDFInfo
- Publication number
- RU2004115403A RU2004115403A RU2004115403/06A RU2004115403A RU2004115403A RU 2004115403 A RU2004115403 A RU 2004115403A RU 2004115403/06 A RU2004115403/06 A RU 2004115403/06A RU 2004115403 A RU2004115403 A RU 2004115403A RU 2004115403 A RU2004115403 A RU 2004115403A
- Authority
- RU
- Russia
- Prior art keywords
- blade
- channels
- cavities
- cooled turbine
- blade according
- Prior art date
Links
Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2004115403/06A RU2267616C1 (en) | 2004-05-21 | 2004-05-21 | Turbine cooled blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2004115403/06A RU2267616C1 (en) | 2004-05-21 | 2004-05-21 | Turbine cooled blade |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2004115403A true RU2004115403A (en) | 2005-11-10 |
RU2267616C1 RU2267616C1 (en) | 2006-01-10 |
Family
ID=35864864
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2004115403/06A RU2267616C1 (en) | 2004-05-21 | 2004-05-21 | Turbine cooled blade |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2267616C1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2450126C2 (en) * | 2010-05-24 | 2012-05-10 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" | Gas turbine engine hollow blade |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2919897B1 (en) * | 2007-08-08 | 2014-08-22 | Snecma | TURBINE DISPENSER SECTOR |
CH700321A1 (en) * | 2009-01-30 | 2010-07-30 | Alstom Technology Ltd | Cooled vane for a gas turbine. |
EP2626519A1 (en) * | 2012-02-09 | 2013-08-14 | Siemens Aktiengesellschaft | Turbine assembly, corresponding impingement cooling tube and gas turbine engine |
US9080451B2 (en) * | 2012-06-28 | 2015-07-14 | General Electric Company | Airfoil |
EP2754856A1 (en) | 2013-01-09 | 2014-07-16 | Siemens Aktiengesellschaft | Blade for a turbomachine |
FR3020402B1 (en) * | 2014-04-24 | 2019-06-14 | Safran Aircraft Engines | DRAWER FOR TURBOMACHINE TURBINE COMPRISING AN IMPROVED HOMOGENEITY COOLING CIRCUIT |
EP2990597A1 (en) * | 2014-08-28 | 2016-03-02 | Siemens Aktiengesellschaft | Method for manufacturing a turbine assembly |
-
2004
- 2004-05-21 RU RU2004115403/06A patent/RU2267616C1/en not_active IP Right Cessation
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2450126C2 (en) * | 2010-05-24 | 2012-05-10 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" | Gas turbine engine hollow blade |
Also Published As
Publication number | Publication date |
---|---|
RU2267616C1 (en) | 2006-01-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20200522 |