CH432554A - Constant pressure turbine stage - Google Patents
Constant pressure turbine stageInfo
- Publication number
- CH432554A CH432554A CH557565A CH557565A CH432554A CH 432554 A CH432554 A CH 432554A CH 557565 A CH557565 A CH 557565A CH 557565 A CH557565 A CH 557565A CH 432554 A CH432554 A CH 432554A
- Authority
- CH
- Switzerland
- Prior art keywords
- constant pressure
- pressure turbine
- turbine stage
- stage
- constant
- 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
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
- F01D1/04—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines traversed by the working-fluid substantially axially
-
- 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
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth 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
- 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
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
- F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
-
- 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
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/145—Means for influencing boundary layers or secondary circulations
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH557565A CH432554A (en) | 1965-04-22 | 1965-04-22 | Constant pressure turbine stage |
GB17277/66A GB1149616A (en) | 1965-04-22 | 1966-04-20 | Improvements relating to impulse turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH557565A CH432554A (en) | 1965-04-22 | 1965-04-22 | Constant pressure turbine stage |
Publications (1)
Publication Number | Publication Date |
---|---|
CH432554A true CH432554A (en) | 1967-03-31 |
Family
ID=4295867
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH557565A CH432554A (en) | 1965-04-22 | 1965-04-22 | Constant pressure turbine stage |
Country Status (2)
Country | Link |
---|---|
CH (1) | CH432554A (en) |
GB (1) | GB1149616A (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4135857A (en) * | 1977-06-09 | 1979-01-23 | United Technologies Corporation | Reduced drag airfoil platforms |
DE102007027427A1 (en) * | 2007-06-14 | 2008-12-18 | Rolls-Royce Deutschland Ltd & Co Kg | Bucket cover tape with overhang |
EP2055896A1 (en) * | 2007-10-31 | 2009-05-06 | Siemens Aktiengesellschaft | Bucket for a turbine of a thermal power plant having a foot section |
FR2938642B1 (en) * | 2008-11-19 | 2010-12-31 | Faure Herman | TURBINE FOR MEASURING PETROLEUM PRODUCTS CHARGED WITH A FRICTION REDUCING AGENT |
-
1965
- 1965-04-22 CH CH557565A patent/CH432554A/en unknown
-
1966
- 1966-04-20 GB GB17277/66A patent/GB1149616A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB1149616A (en) | 1969-04-23 |
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