GB191714A - Improvements relating to elastic fluid turbines - Google Patents
Improvements relating to elastic fluid turbinesInfo
- Publication number
- GB191714A GB191714A GB34722/22A GB3472222A GB191714A GB 191714 A GB191714 A GB 191714A GB 34722/22 A GB34722/22 A GB 34722/22A GB 3472222 A GB3472222 A GB 3472222A GB 191714 A GB191714 A GB 191714A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flow
- fluid
- axial
- blades
- stage
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
191,714. Metropolitan-Vickers Electrical Co., Ltd., (Assignees of Allen, R. C.). Jan. 13, 1922, [Convention date]. Combined-flow type; axial-flow type; blades.- In an elastic fluid turbine the blade space between the rotor and casing is shaped to change the mean direction of fluid flow gradually from an axial to a radial direction. The fluid passes through a velocity stage 14 and an axial-flow stage 12 having blades of gradually increasing length to an axial radial stage comprising wide rotor blades 19, 21 of substantially triangular form separated by stator blades 20 also of triangular form. The exit edges 23, 24 of the rotor blades are normal to the mean direction of flow of the fluid. Guiding-ribs 31 assist in changing the direction of flow of the fluid and prevent eddies.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US191714XA | 1922-01-13 | 1922-01-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB191714A true GB191714A (en) | 1923-02-15 |
Family
ID=21791800
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB34722/22A Expired GB191714A (en) | 1922-01-13 | 1922-12-20 | Improvements relating to elastic fluid turbines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB191714A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0336064A1 (en) * | 1988-03-31 | 1989-10-11 | Daimler-Benz Aktiengesellschaft | Exhaust gas turbocharger for combustion engine |
-
1922
- 1922-12-20 GB GB34722/22A patent/GB191714A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0336064A1 (en) * | 1988-03-31 | 1989-10-11 | Daimler-Benz Aktiengesellschaft | Exhaust gas turbocharger for combustion engine |
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