GB237611A - - Google Patents
Info
- Publication number
- GB237611A GB237611A GB18680/25A GB1868025A GB237611A GB 237611 A GB237611 A GB 237611A GB 18680/25 A GB18680/25 A GB 18680/25A GB 1868025 A GB1868025 A GB 1868025A GB 237611 A GB237611 A GB 237611A
- Authority
- GB
- United Kingdom
- Prior art keywords
- stage
- point
- abrupt change
- radialflow
- assignees
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
237,611. International General Electric Co., Inc., (Assignees of Allgemeine Elektricitõts Ges.). July 24, 1924, [Convention date]. Combined-flow type. - In turbines with an abrupt change of diameter of the rotor, a radialflow stage e is arranged in the steam passage at the point of the abrupt change. The stator blades of the stage e are mounted on insertions f introduced into openings in the disc-shaped wall at the point of transition.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE237611X | 1924-07-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB237611A true GB237611A (en) | 1925-10-15 |
Family
ID=5903187
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB18680/25A Expired GB237611A (en) | 1924-07-24 | 1925-07-22 |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB237611A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1027530A1 (en) * | 1997-10-27 | 2000-08-16 | Kenneth Douglas Horner | An air turbine motor |
-
1925
- 1925-07-22 GB GB18680/25A patent/GB237611A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1027530A1 (en) * | 1997-10-27 | 2000-08-16 | Kenneth Douglas Horner | An air turbine motor |
EP1027530A4 (en) * | 1997-10-27 | 2004-05-12 | Kenneth Douglas Horner | An air turbine motor |
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