GB647451A - Improvements in or relating to gas turbine power plants - Google Patents
Improvements in or relating to gas turbine power plantsInfo
- Publication number
- GB647451A GB647451A GB28423/48A GB2842348A GB647451A GB 647451 A GB647451 A GB 647451A GB 28423/48 A GB28423/48 A GB 28423/48A GB 2842348 A GB2842348 A GB 2842348A GB 647451 A GB647451 A GB 647451A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- shroud ring
- welded
- gas turbine
- relating
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
647,451. Gas turbines. WESTINGHOUSE ELECTRIC INTERNATIONAL CO. Nov. 2, 1948, No. 28423. Convention date, Nov. 3, 1947. [Class 110(iii)] Stator blades 26, 27 of a gas turbine are supported by a two-piece tubular member 47, 49 bolted to a flange 38. The flange is welded to a conical piece 31 itself welded to the casing 10. The tubular part 47 is flanged at 48 to receive the outer shroud ring 41 of the blades 26. The tubular part 49 is welded to an upstanding ring 50 on the outer shroud ring 45 of the blades 27. The shroud ring 45 extends over the tips of the running blades 22, 23. The parts 47, 41 and 49, 45 are spaced apart over most of their length. The inner shroud ring 40 is secured to a main-shaft bearing support 60.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US647451XA | 1947-11-03 | 1947-11-03 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB647451A true GB647451A (en) | 1950-12-13 |
Family
ID=22058012
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB28423/48A Expired GB647451A (en) | 1947-11-03 | 1948-11-02 | Improvements in or relating to gas turbine power plants |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB647451A (en) |
-
1948
- 1948-11-02 GB GB28423/48A patent/GB647451A/en not_active Expired
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB599391A (en) | Improvements in and relating to axial flow compressors, turbines and the like machines | |
GB590420A (en) | Improvements in and relating to gas turbines | |
GB1151613A (en) | Improvements In Gas Turbine Ducted Fan Engine Assemblies | |
GB1523668A (en) | Turbomachinery stator assembly | |
GB582152A (en) | Improvements in or relating to turbine apparatus | |
GB608514A (en) | Improvements in or relating to drum structures | |
GB609220A (en) | Improvements in or relating to nozzles and stationary blades for turbines and like machines | |
GB705387A (en) | Improvements relating to radial-flow turbine or centrifugal compressors | |
GB621315A (en) | Improvements relating to compressors and turbines | |
GB618037A (en) | Improvements in turbine wheels and their method of manufacture | |
GB609446A (en) | Improvements in or relating to the rotors of gas turbines or the like | |
GB647451A (en) | Improvements in or relating to gas turbine power plants | |
GB192405A (en) | Improvements relating to wind turbines | |
GB626818A (en) | Mounting of turbine stators | |
GB624777A (en) | Improvements in or relating to stator casings for compressors and like machines | |
GB711528A (en) | Elastic fluid turbine plant | |
GB614547A (en) | Improvements in axial flow elastic fluid turbines or compressors | |
GB732920A (en) | Improvements relating to blade assemblies of turbo-machines such as compressors and turbines | |
GB844020A (en) | Stator vane assemblies for axial-flow compressors and turbines | |
GB586564A (en) | Improvements in high speed axial flow elastic fluid turbines, compressors, superchargers and like apparatus | |
GB661078A (en) | Improvements in or relating to gas turbine power plants | |
GB696558A (en) | Stator and rotor cooling means in gas turbines | |
GB636860A (en) | Improvements in or relating to stationary blading for turbines | |
GB600057A (en) | Improvements in or relating to the mounting of blades in axial flow compressors, turbines, or the like | |
GB345888A (en) | An improved method of supporting the guide blades in turbines |