GB2087980B - Liquid cooled aerofoil for a gas turbine engine and a method of making the aerofoil - Google Patents
Liquid cooled aerofoil for a gas turbine engine and a method of making the aerofoilInfo
- Publication number
- GB2087980B GB2087980B GB8037324A GB8037324A GB2087980B GB 2087980 B GB2087980 B GB 2087980B GB 8037324 A GB8037324 A GB 8037324A GB 8037324 A GB8037324 A GB 8037324A GB 2087980 B GB2087980 B GB 2087980B
- Authority
- GB
- United Kingdom
- Prior art keywords
- aerofoil
- making
- gas turbine
- turbine engine
- liquid cooled
- 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
- F01D5/181—Blades having a closed internal cavity containing a cooling medium, e.g. sodium
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 |
---|---|---|---|
GB8037324A GB2087980B (en) | 1980-11-20 | 1980-11-20 | Liquid cooled aerofoil for a gas turbine engine and a method of making the aerofoil |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8037324A GB2087980B (en) | 1980-11-20 | 1980-11-20 | Liquid cooled aerofoil for a gas turbine engine and a method of making the aerofoil |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2087980A GB2087980A (en) | 1982-06-03 |
GB2087980B true GB2087980B (en) | 1984-03-14 |
Family
ID=10517458
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8037324A Expired GB2087980B (en) | 1980-11-20 | 1980-11-20 | Liquid cooled aerofoil for a gas turbine engine and a method of making the aerofoil |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2087980B (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3477296B2 (en) * | 1995-11-21 | 2003-12-10 | 三菱重工業株式会社 | Gas turbine blades |
US7578652B2 (en) | 2006-10-03 | 2009-08-25 | United Technologies Corporation | Hybrid vapor and film cooled turbine blade |
EP2540970A1 (en) * | 2011-07-01 | 2013-01-02 | Siemens Aktiengesellschaft | Liquid metal cooled blade |
US10450950B2 (en) * | 2016-10-26 | 2019-10-22 | General Electric Company | Turbomachine blade with trailing edge cooling circuit |
-
1980
- 1980-11-20 GB GB8037324A patent/GB2087980B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB2087980A (en) | 1982-06-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |