GB639311A - Improvements in and relating to steam or gas turbines with more than two cylinders - Google Patents
Improvements in and relating to steam or gas turbines with more than two cylindersInfo
- Publication number
- GB639311A GB639311A GB14227/48A GB1422748A GB639311A GB 639311 A GB639311 A GB 639311A GB 14227/48 A GB14227/48 A GB 14227/48A GB 1422748 A GB1422748 A GB 1422748A GB 639311 A GB639311 A GB 639311A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pressure
- cylinders
- low
- cylinder
- steam
- 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
- F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
- F01D3/02—Machines or engines with axial-thrust balancing effected by working-fluid characterised by having one fluid flow in one axial direction and another fluid flow in the opposite direction
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
639,311. Elastic fluid turbines. BRITISH THOMSON-HOUSTON CO., Ltd. May 26, 1948, No. 14227. Convention date, May 29, 1947. [Class 110(iii)] In a turbine having, at least, high-pressure, intermediate and low-pressure cylinders. 1, 2, 3, the high and low-pressure cylinders are adjacent and the only thrust bearing 5 is between them. The intermediate pressure cylinder 2 and the generator 4 are beyond the low-pressure cylinder and all the shafts are coupled without relative axial freedom. The fluid flows through the high and intermediate-pressure cylinders are in directions away from the thrust bearing. The low-pressure turbine may comprise one or two cylinders of the double flow type, or, one such cylinder in parallel with a low-pressure stage constructed with the intermediate pressure stage.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR639311X | 1947-05-29 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB639311A true GB639311A (en) | 1950-06-28 |
Family
ID=8996661
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB14227/48A Expired GB639311A (en) | 1947-05-29 | 1948-05-26 | Improvements in and relating to steam or gas turbines with more than two cylinders |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB639311A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108979761A (en) * | 2018-07-24 | 2018-12-11 | 哈尔滨汽轮机厂有限责任公司 | A kind of large capacity combination circulation steam turbine |
-
1948
- 1948-05-26 GB GB14227/48A patent/GB639311A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108979761A (en) * | 2018-07-24 | 2018-12-11 | 哈尔滨汽轮机厂有限责任公司 | A kind of large capacity combination circulation steam turbine |
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