GB128584A - Improvements in Multi-stage Turbines. - Google Patents
Improvements in Multi-stage Turbines.Info
- Publication number
- GB128584A GB128584A GB15569/19A GB1556919A GB128584A GB 128584 A GB128584 A GB 128584A GB 15569/19 A GB15569/19 A GB 15569/19A GB 1556919 A GB1556919 A GB 1556919A GB 128584 A GB128584 A GB 128584A
- Authority
- GB
- United Kingdom
- Prior art keywords
- recesses
- rotor
- motor
- circular
- turbine
- 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
- F01D1/02—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
- F01D1/026—Impact turbines with buckets, i.e. impulse turbines, e.g. Pelton turbines
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
128,584. Pidwell, A. W., and Du Saussois, A. M. J. M. June 18, 1918, [Convention date]. Circular-flow type; reversing; motor power plant.-A reversible circular-flow turbine having a number of concentric stages comprises a onepiece rotor c formed with concentric rings of budgets d<1>, d<2>, d<3> located between two casing parts a, b having recesses o<1>, o<2>, 0<o>. The rotor c and casing members a, b are formed as shown in Fig. 3, one side being used for forward working and the other for reverse working. Motive fluid is admitted by inlets g to and round the innermost ring of buckets d' and recesses o<1>, and passes to the outer rings successively. The turbine may be used as a silencer and an auxiliary motor on motor-cars by discharging the exhaust gases therethrough. The Specification as open to inspection under Sect. 91 (3) (a) comprises also the non-reversible modification shown in Fig. 3 (Cancelled). This subject-matter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR128584X | 1918-06-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB128584A true GB128584A (en) | 1920-04-22 |
Family
ID=32339389
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15569/19A Expired GB128584A (en) | 1918-06-18 | 1919-06-20 | Improvements in Multi-stage Turbines. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB128584A (en) |
-
1919
- 1919-06-20 GB GB15569/19A patent/GB128584A/en not_active Expired
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