CH355327A - Axial turbine, in particular gas turbine - Google Patents
Axial turbine, in particular gas turbineInfo
- Publication number
- CH355327A CH355327A CH355327DA CH355327A CH 355327 A CH355327 A CH 355327A CH 355327D A CH355327D A CH 355327DA CH 355327 A CH355327 A CH 355327A
- Authority
- CH
- Switzerland
- Prior art keywords
- turbine
- particular gas
- axial
- gas turbine
- axial turbine
- Prior art date
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
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
- F01D5/084—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades the fluid circulating at the periphery of a multistage rotor, e.g. of drum type
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2564659A GB857750A (en) | 1959-07-27 | 1959-07-27 | Axial flow machine, particularly gas turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
CH355327A true CH355327A (en) | 1961-06-30 |
Family
ID=10231048
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH355327D CH355327A (en) | 1959-07-27 | 1958-01-23 | Axial turbine, in particular gas turbine |
Country Status (2)
Country | Link |
---|---|
CH (1) | CH355327A (en) |
GB (1) | GB857750A (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1869289B1 (en) * | 2005-04-11 | 2014-12-03 | Alstom Technology Ltd | Guide vane support |
US9206693B2 (en) | 2011-02-18 | 2015-12-08 | General Electric Company | Apparatus, method, and system for separating particles from a fluid stream |
DE102013224199A1 (en) * | 2013-11-27 | 2015-05-28 | MTU Aero Engines AG | Gas turbine blade |
US9896939B2 (en) * | 2015-03-12 | 2018-02-20 | United Technologies Corporation | Integral metering feature, systems and methods |
-
1958
- 1958-01-23 CH CH355327D patent/CH355327A/en unknown
-
1959
- 1959-07-27 GB GB2564659A patent/GB857750A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB857750A (en) | 1961-01-04 |
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