JPS57153903A - Cooling structure for turbing blade - Google Patents
Cooling structure for turbing bladeInfo
- Publication number
- JPS57153903A JPS57153903A JP3937081A JP3937081A JPS57153903A JP S57153903 A JPS57153903 A JP S57153903A JP 3937081 A JP3937081 A JP 3937081A JP 3937081 A JP3937081 A JP 3937081A JP S57153903 A JPS57153903 A JP S57153903A
- Authority
- JP
- Japan
- Prior art keywords
- blade
- passages
- convection
- passage
- turbine blade
- 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.)
- Pending
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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
PURPOSE:To provide good cooling structure for the whole surface of a turbine blade of return flow type, by making the upstream part of the cooling passage of the blade of convection passages and making the downstream part of blowoff passages and a central passage connected to the convection passage. CONSTITUTION:The upstream part of the cooling passage of a turbine blade 1 is made of plural convection passages 2 located near the surface of the blade and extending in parallel with each other in the direction of the height of the blade. The convection passages 2 are connected to each other through communication passages 6 at the tip or butt of the blade 1 so that the flow of a fluid through the convection passage is turned in the communication passage. The last convection passage 2 is provided with a communication port 7 connected to a central passage 3 which extends in the direction of the height of the turbine blade 2 inside the convection passages 2 and has a relatively large cross-sectional area. An appropriate number of the convection passages 2 are connected to the central passage 3. Blowoff passages 4 are provided beside the central passage 3 so that the blowoff passages extend through the wall of the turbine blade 2 and communicate with the outside of the blade. According to this constitution, good cooling performance is attained for the whole surface of the blade 2.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3937081A JPS57153903A (en) | 1981-03-20 | 1981-03-20 | Cooling structure for turbing blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3937081A JPS57153903A (en) | 1981-03-20 | 1981-03-20 | Cooling structure for turbing blade |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS57153903A true JPS57153903A (en) | 1982-09-22 |
Family
ID=12551162
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP3937081A Pending JPS57153903A (en) | 1981-03-20 | 1981-03-20 | Cooling structure for turbing blade |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS57153903A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2678318A1 (en) * | 1991-06-25 | 1992-12-31 | Snecma | COOLED VANE OF TURBINE DISTRIBUTOR. |
US5484258A (en) * | 1994-03-01 | 1996-01-16 | General Electric Company | Turbine airfoil with convectively cooled double shell outer wall |
US6705836B2 (en) * | 2001-08-28 | 2004-03-16 | Snecma Moteurs | Gas turbine blade cooling circuits |
JP2015507129A (en) * | 2012-02-14 | 2015-03-05 | シーメンス アクティエンゲゼルシャフト | Turbine guide vane with throttle element |
JP2017115881A (en) * | 2015-12-21 | 2017-06-29 | ゼネラル・エレクトリック・カンパニイ | Platform core feed for multi-wall blade |
-
1981
- 1981-03-20 JP JP3937081A patent/JPS57153903A/en active Pending
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2678318A1 (en) * | 1991-06-25 | 1992-12-31 | Snecma | COOLED VANE OF TURBINE DISTRIBUTOR. |
US5484258A (en) * | 1994-03-01 | 1996-01-16 | General Electric Company | Turbine airfoil with convectively cooled double shell outer wall |
US6705836B2 (en) * | 2001-08-28 | 2004-03-16 | Snecma Moteurs | Gas turbine blade cooling circuits |
JP2015507129A (en) * | 2012-02-14 | 2015-03-05 | シーメンス アクティエンゲゼルシャフト | Turbine guide vane with throttle element |
US9856738B2 (en) | 2012-02-14 | 2018-01-02 | Siemens Aktiengesellschaft | Turbine guide vane with a throttle element |
JP2017115881A (en) * | 2015-12-21 | 2017-06-29 | ゼネラル・エレクトリック・カンパニイ | Platform core feed for multi-wall blade |
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