GB200796A - Improvements in and relating to elastic fluid turbines - Google Patents
Improvements in and relating to elastic fluid turbinesInfo
- Publication number
- GB200796A GB200796A GB13948/23A GB1394823A GB200796A GB 200796 A GB200796 A GB 200796A GB 13948/23 A GB13948/23 A GB 13948/23A GB 1394823 A GB1394823 A GB 1394823A GB 200796 A GB200796 A GB 200796A
- Authority
- GB
- United Kingdom
- Prior art keywords
- nozzle
- fluid turbines
- relating
- throat
- elastic 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
- 239000012530 fluid Substances 0.000 title abstract 2
- 230000004323 axial length Effects 0.000 abstract 1
- 238000005192 partition Methods 0.000 abstract 1
- 230000000717 retained effect Effects 0.000 abstract 1
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
- F01D1/04—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 traversed by the working-fluid substantially axially
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
200,796. British Thomson - Houston Co., Ltd., (Assignees of Warren, G. B., and Wirt, H. L.). July 12, 1922, [Convention date]. Axial-flow type ; nozzles.-In elastic-fluid turbines of the impulse type wherein the nozzle passages flare radially outwards, the nozzle sidewalls or partitions 6 at the throat and/or at the exit edges 8 are given a small forward inclination b to the radius a, the concentric form of the radially flared inner and outer walls of the nozzle passages being retained throughout the axial length of the nozzle. The nozzle throat may be positioned at the exit edges.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US200796XA | 1922-07-12 | 1922-07-12 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB200796A true GB200796A (en) | 1924-01-10 |
Family
ID=21796634
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB13948/23A Expired GB200796A (en) | 1922-07-12 | 1923-05-26 | Improvements in and relating to elastic fluid turbines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB200796A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2266931A (en) * | 1992-05-15 | 1993-11-17 | Gec Alsthom Ltd | Turbine guide blade assembly. |
| RU2187659C1 (en) * | 2000-12-07 | 2002-08-20 | Ревзин Борис Соломонович | Axial flow turbine nozzle assembly |
-
1923
- 1923-05-26 GB GB13948/23A patent/GB200796A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2266931A (en) * | 1992-05-15 | 1993-11-17 | Gec Alsthom Ltd | Turbine guide blade assembly. |
| GB2266931B (en) * | 1992-05-15 | 1995-08-30 | Gec Alsthom Ltd | Turbine blade assembly |
| US5575620A (en) * | 1992-05-15 | 1996-11-19 | Gec Alsthom Limited | Turbine blade assembly |
| RU2187659C1 (en) * | 2000-12-07 | 2002-08-20 | Ревзин Борис Соломонович | Axial flow turbine nozzle assembly |
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