GB574478A - Improvements in and relating to gas turbine cooling arrangements - Google Patents
Improvements in and relating to gas turbine cooling arrangementsInfo
- Publication number
- GB574478A GB574478A GB15202/41A GB1520241A GB574478A GB 574478 A GB574478 A GB 574478A GB 15202/41 A GB15202/41 A GB 15202/41A GB 1520241 A GB1520241 A GB 1520241A GB 574478 A GB574478 A GB 574478A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- partition
- nozzle
- relating
- box
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/085—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Supercharger (AREA)
Abstract
574,478. Gas turbines. BRITISH THOMSON-HOUSTON CO., Ltd. (General Electric Co.). Nov. 25, 1941, No. 15202. [Class 110 (iii)] The nozzle-box 12 of an exhaust gas turbine is separated from the driven air compressor 13 by a partition 17. Cooling air is admitted by a conduit 21 and part passes between the compressor and the partition. The rest is directed by a curved trough 20 to the turbine wheel disc and escapes between the nozzle-box and a curved screen 15 to the space on the nozzle-box side of the partition 17.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB15202/41A GB574478A (en) | 1941-11-25 | 1941-11-25 | Improvements in and relating to gas turbine cooling arrangements |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB15202/41A GB574478A (en) | 1941-11-25 | 1941-11-25 | Improvements in and relating to gas turbine cooling arrangements |
Publications (1)
Publication Number | Publication Date |
---|---|
GB574478A true GB574478A (en) | 1946-01-08 |
Family
ID=10054832
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15202/41A Expired GB574478A (en) | 1941-11-25 | 1941-11-25 | Improvements in and relating to gas turbine cooling arrangements |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB574478A (en) |
-
1941
- 1941-11-25 GB GB15202/41A patent/GB574478A/en not_active Expired
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