GB2067674B - Rotor blade for a gas turbine engine - Google Patents
Rotor blade for a gas turbine engineInfo
- Publication number
- GB2067674B GB2067674B GB8002281A GB8002281A GB2067674B GB 2067674 B GB2067674 B GB 2067674B GB 8002281 A GB8002281 A GB 8002281A GB 8002281 A GB8002281 A GB 8002281A GB 2067674 B GB2067674 B GB 2067674B
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- turbine engine
- rotor blade
- rotor
- 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.)
- Expired
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)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8002281A GB2067674B (en) | 1980-01-23 | 1980-01-23 | Rotor blade for a gas turbine engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8002281A GB2067674B (en) | 1980-01-23 | 1980-01-23 | Rotor blade for a gas turbine engine |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2067674A GB2067674A (en) | 1981-07-30 |
GB2067674B true GB2067674B (en) | 1983-10-19 |
Family
ID=10510840
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8002281A Expired GB2067674B (en) | 1980-01-23 | 1980-01-23 | Rotor blade for a gas turbine engine |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2067674B (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5125798A (en) * | 1990-04-13 | 1992-06-30 | General Electric Company | Method and apparatus for cooling air flow at gas turbine bucket trailing edge tip |
EP1041247B1 (en) * | 1999-04-01 | 2012-08-01 | General Electric Company | Gas turbine airfoil comprising an open cooling circuit |
US6761534B1 (en) * | 1999-04-05 | 2004-07-13 | General Electric Company | Cooling circuit for a gas turbine bucket and tip shroud |
GB2350867B (en) * | 1999-06-09 | 2003-03-19 | Rolls Royce Plc | Gas turbine airfoil internal air system |
US6966755B2 (en) | 2004-02-09 | 2005-11-22 | Siemens Westinghouse Power Corporation | Compressor airfoils with movable tips |
US7244101B2 (en) * | 2005-10-04 | 2007-07-17 | General Electric Company | Dust resistant platform blade |
-
1980
- 1980-01-23 GB GB8002281A patent/GB2067674B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB2067674A (en) | 1981-07-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |