GB191128314A - Improvements in and relating to Turbines. - Google Patents
Improvements in and relating to Turbines.Info
- Publication number
- GB191128314A GB191128314A GB191128314DA GB191128314A GB 191128314 A GB191128314 A GB 191128314A GB 191128314D A GB191128314D A GB 191128314DA GB 191128314 A GB191128314 A GB 191128314A
- Authority
- GB
- United Kingdom
- Prior art keywords
- jet
- blades
- turbine
- rotor
- reversing
- 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
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/30—Non-positive-displacement machines or engines, e.g. steam turbines characterised by having a single rotor operable in either direction of rotation, e.g. by reversing of blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
Abstract
28,314. Anderson, H. P. H., and Ward, J. C. A. Dec. 16. Working-fluid supply; reversing; blades. - A turbine provided with blades modified for reversing is driven by an air current induced by a jet of steam or gas which may be arranged to operate on the inlet or on the exhaust side of the turbine for either direction of working. A jet 20 is provided at each end of a casing 6, which houses a rotor 1 having sets of blades co-operating with stator blades 7 and so disposed that the rotor is driven in either direction, according to the direction in which the flow of air is induced through the casing, i.e. according to which jet 20 is put in operation. Steam or gas is admitted by a valve 19 to either jet 20, the spindle 21 of which may be governor-controlled. Condensers 10, 11 may be provided. By reversing the direction of the jet 20, a forced current of air may be driven through the turbine, and the condenser may be arranged so that the steam &c. is condensed either before or after passing through the turbine. The rotor blades may be formed from a solid disk, which may be secured between the bolted rings 2 of the rotor.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB191128314T | 1911-12-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB191128314A true GB191128314A (en) | 1912-11-21 |
Family
ID=32366536
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB191128314D Expired GB191128314A (en) | 1911-12-16 | 1911-12-16 | Improvements in and relating to Turbines. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB191128314A (en) |
-
1911
- 1911-12-16 GB GB191128314D patent/GB191128314A/en not_active Expired
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