GB190804157A - Multistage Re-action Steam Turbines. - Google Patents
Multistage Re-action Steam Turbines.Info
- Publication number
- GB190804157A GB190804157A GB190804157DA GB190804157A GB 190804157 A GB190804157 A GB 190804157A GB 190804157D A GB190804157D A GB 190804157DA GB 190804157 A GB190804157 A GB 190804157A
- Authority
- GB
- United Kingdom
- Prior art keywords
- steam
- shaft
- casing
- centre
- annular chamber
- 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
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
4157. Brown, Boveri, et Cie, Akt.-Ges. March 26, 1907, [date applied for under Section 91 of Patents &c. Act, 1907]. Elastic-fluid turbines.-To prevent deformation by bending &c. of the cylinder or shaft of a multiple - stage reaction steam turbine of the Parsons type, due to the high temperature of the entering superheated steam, a separate annular chamber is provided within the casing to isolate the steam until it has sufficiently cooled. The annular chamber b is fixed and has a bladed portion d. A rotating bladed drum e is thermally insulated from the shaft, but is connected to it for driving purposes. Pieces i centre the portion e relatively to the shaft, and projections l centre the fixed part d. The flanged steam inlet m may be formed in one piece with the part d or may be attached to it. Steam-tight packing o is provided for the steam inlet. The superheated steam passes into the annular space b and between the portions d, e before coming into contact with either the turbine shaft or casing when it is at a sufficiently low temperature. The passage between the part d and the casing leads to the dummy piston h for balancing purposes.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE190804157X | 1907-03-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB190804157A true GB190804157A (en) | 1908-07-09 |
Family
ID=32186885
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB190804157D Expired GB190804157A (en) | 1907-03-26 | 1908-02-24 | Multistage Re-action Steam Turbines. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB190804157A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2425177A (en) * | 1943-05-11 | 1947-08-05 | United Aircraft Corp | Turbine construction |
-
1908
- 1908-02-24 GB GB190804157D patent/GB190804157A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2425177A (en) * | 1943-05-11 | 1947-08-05 | United Aircraft Corp | Turbine construction |
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Drewry | Closure to “Discussions of ‘Reheat Experiences at Port Washington’”(1952, Trans. ASME, 74, pp. 555–556) |