GB490501A - Improvements in or relating to the blading of steam or gas turbines - Google Patents
Improvements in or relating to the blading of steam or gas turbinesInfo
- Publication number
- GB490501A GB490501A GB6688/38A GB668838A GB490501A GB 490501 A GB490501 A GB 490501A GB 6688/38 A GB6688/38 A GB 6688/38A GB 668838 A GB668838 A GB 668838A GB 490501 A GB490501 A GB 490501A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- steam
- blading
- relating
- gas turbines
- 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
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
- E05D15/00—Suspension arrangements for wings
- E05D15/40—Suspension arrangements for wings supported on arms movable in vertical planes
- E05D15/403—Suspension arrangements for wings supported on arms movable in vertical planes with arms fixed on the wing pivoting about an axis outside the wing
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/31—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor with roughened surfaces
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
490,501. Elastic - fluid turbines. ESCHER WYSS MASCHINENFABRIKEN AKT.-GES. March 3, 1938, No. 6688. Convention date, March 4, 1937. [Class 110 (iii)] A guide blade 1 for a steam or gas turbine with a bevelled outlet edge 5 has the portion 6 of the blade adjacent the bevelled edge made rougher than the rest of the surface. The blade may be roughened on one or both sides, and the roughness may be formed by fixing raised surfaces to the blade.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH490501X | 1937-03-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB490501A true GB490501A (en) | 1938-08-16 |
Family
ID=4516592
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB6688/38A Expired GB490501A (en) | 1937-03-04 | 1938-03-03 | Improvements in or relating to the blading of steam or gas turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB490501A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2788172A (en) * | 1951-12-06 | 1957-04-09 | Stalker Dev Company | Bladed structures for axial flow compressors |
US2819837A (en) * | 1952-06-19 | 1958-01-14 | Laval Steam Turbine Co | Compressor |
US2934952A (en) * | 1952-06-07 | 1960-05-03 | Gehre Hans | Orifice plate throttling device for axial flow measuring wheel meters |
US3014640A (en) * | 1958-06-09 | 1961-12-26 | Gen Motors Corp | Axial flow compressor |
US3161167A (en) * | 1963-02-14 | 1964-12-15 | Murray H Silverman | Method and means for reducing hydrodynamic noise |
US5228833A (en) * | 1991-06-28 | 1993-07-20 | Asea Brown Boveri Ltd. | Turbomachine blade/vane for subsonic conditions |
-
1938
- 1938-03-03 GB GB6688/38A patent/GB490501A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2788172A (en) * | 1951-12-06 | 1957-04-09 | Stalker Dev Company | Bladed structures for axial flow compressors |
US2934952A (en) * | 1952-06-07 | 1960-05-03 | Gehre Hans | Orifice plate throttling device for axial flow measuring wheel meters |
US2819837A (en) * | 1952-06-19 | 1958-01-14 | Laval Steam Turbine Co | Compressor |
US3014640A (en) * | 1958-06-09 | 1961-12-26 | Gen Motors Corp | Axial flow compressor |
US3161167A (en) * | 1963-02-14 | 1964-12-15 | Murray H Silverman | Method and means for reducing hydrodynamic noise |
US5228833A (en) * | 1991-06-28 | 1993-07-20 | Asea Brown Boveri Ltd. | Turbomachine blade/vane for subsonic conditions |
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