GB574545A - Improvements in and relating to cooling arrangements for gas turbines - Google Patents
Improvements in and relating to cooling arrangements for gas turbinesInfo
- Publication number
- GB574545A GB574545A GB10341/41A GB1034141A GB574545A GB 574545 A GB574545 A GB 574545A GB 10341/41 A GB10341/41 A GB 10341/41A GB 1034141 A GB1034141 A GB 1034141A GB 574545 A GB574545 A GB 574545A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbines
- relating
- cooling arrangements
- wheel
- houston
- 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)
Abstract
574,545. Gas turbines. BRITISH THOMSON-HOUSTON CO., Ltd., (General Electric Co.). Aug. 14,1941, No. 10341. [Class 110 (iii)] A turbine wheel 10 receiving the exhaust from an aircraft I.C. engine is cooled by a flow of air taken in at 23, passed through the space between the wheel and a dished disc 24 and discharged into the slip stream at 29. Specification 567,546 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB10341/41A GB574545A (en) | 1941-08-14 | 1941-08-14 | Improvements in and relating to cooling arrangements for gas turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB10341/41A GB574545A (en) | 1941-08-14 | 1941-08-14 | Improvements in and relating to cooling arrangements for gas turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB574545A true GB574545A (en) | 1946-01-10 |
Family
ID=9966070
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB10341/41A Expired GB574545A (en) | 1941-08-14 | 1941-08-14 | Improvements in and relating to cooling arrangements for gas turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB574545A (en) |
-
1941
- 1941-08-14 GB GB10341/41A patent/GB574545A/en not_active Expired
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