GB173365A - Improvements in and relating to elastic fluid turbines - Google Patents
Improvements in and relating to elastic fluid turbinesInfo
- Publication number
- GB173365A GB173365A GB2938520A GB2938520A GB173365A GB 173365 A GB173365 A GB 173365A GB 2938520 A GB2938520 A GB 2938520A GB 2938520 A GB2938520 A GB 2938520A GB 173365 A GB173365 A GB 173365A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chest
- chambers
- turbine
- blades
- motive fluid
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
173,365. British Thomson - Houston Co., Ltd., (General Electric Co.). Oct. 18, 1920. Axial-flow type; casings.-The motive fluid for a turbine 11 is supplied through nozzles carried by an annular chest 14 which is mounted between the casing walls 6, 7 so that it may expand and contract independently of said walls. For this purpose the chest is slidably mounted on fixed radial tubes 17 which together with conduits 19 may be used to admit motive fluid from the valve chest 20 to one or more of the chambers 31, 32, 33, 34 of the chest 14. Each of these chambers feeds a definite arc of nozzles. The first stage wheel 11 has two rows of blades 12, 13, with fixed intermediate blades 35, the latter being preferably provided only in front of those portions of the nozzle ring which are used in operating the turbine up to normal load. For example, the intermediate blades may be omitted in front of chamber 34 or in front of both chambers 33, 34.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2938520A GB173365A (en) | 1920-10-18 | 1920-10-18 | Improvements in and relating to elastic fluid turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2938520A GB173365A (en) | 1920-10-18 | 1920-10-18 | Improvements in and relating to elastic fluid turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB173365A true GB173365A (en) | 1922-01-05 |
Family
ID=10290714
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2938520A Expired GB173365A (en) | 1920-10-18 | 1920-10-18 | Improvements in and relating to elastic fluid turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB173365A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1032272B (en) * | 1954-07-14 | 1958-06-19 | Vickers Armstrongs Ltd | Hot steam turbine |
-
1920
- 1920-10-18 GB GB2938520A patent/GB173365A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1032272B (en) * | 1954-07-14 | 1958-06-19 | Vickers Armstrongs Ltd | Hot steam turbine |
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