GB191318865A - Improvements in Turbines. - Google Patents
Improvements in Turbines.Info
- Publication number
- GB191318865A GB191318865A GB191318865DA GB191318865A GB 191318865 A GB191318865 A GB 191318865A GB 191318865D A GB191318865D A GB 191318865DA GB 191318865 A GB191318865 A GB 191318865A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- ports
- steam
- stages
- exhaust ports
- 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
- F01D9/06—Fluid supply conduits to nozzles or the like
-
- 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
18,865. Owens, C. T. Aug. 19. Combined-flow type.-The rotor is provided with a number of rows of blades 30, Figs. 4 and 5, parallel to the axis of the turbine; the stator being provided with similar blades 32, Fig. 5, inclined to the axis of the turbine. Ports 11, 12 are provided in the casing and perform the functions of inlet and exhaust ports alternatively. Assuming that the steam is admitted by way of ports 11, the first row of blades a operate as a jet-wheel. The steam is subsequently successively re-directed axially by the blades 32 upon the succeeding stages, which thereby act as axial-flow stages. When running in the reverse direction the row of blades g have a jet-wheel action and the remaining stages an axial-flow action. The casing may be provided with by-passes 35, Fig. 4, in which case the first row of blades act as a circular-flow. stage. Plant.-A number of turbines 2, 3, 4, Figs. 1 and 2, in axial alinement, drive a common shaft 5. The steam passes through the turbines in series. Reversing.-Each turbine is provided with a cylindrical valve chamber 6, provided with an inlet port 7 and two exhaust ports 8. A piston valve 13 places the ports 12, 11 in communication with the inlet port 7 and one of the exhaust ports 8 respectively, or vice versa. The three reversing-valves are simultaneously operated by a rock-shaft 19, Figs. 1 and 2, actuated by a fluid-relay 24. Each pair of exhaust ports are connected to the succeeding inlet port by a Y-connexion such as 9, 10, Fig. 2. Regulating.-An auxiliary supply of live steam may be supplied to the intermediate and low-pressure stages to facilitate starting by a pipe 37, Fig. 4.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB191318865T | 1913-08-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB191318865A true GB191318865A (en) | 1914-01-22 |
Family
ID=32579120
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB191318865D Expired GB191318865A (en) | 1913-08-19 | 1913-08-19 | Improvements in Turbines. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB191318865A (en) |
-
1913
- 1913-08-19 GB GB191318865D patent/GB191318865A/en not_active Expired
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