GB434363A - Improvements in or relating to turbines - Google Patents
Improvements in or relating to turbinesInfo
- Publication number
- GB434363A GB434363A GB6847/34A GB684734A GB434363A GB 434363 A GB434363 A GB 434363A GB 6847/34 A GB6847/34 A GB 6847/34A GB 684734 A GB684734 A GB 684734A GB 434363 A GB434363 A GB 434363A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbines
- march
- arc
- fluid
- blade ring
- 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
- 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
- F01D1/12—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 with repeated action on same blade ring
- F01D1/14—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 with repeated action on same blade ring traversed by the working-fluid substantially radially
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
434,363. Elastic - fluid turbines. ZERKOWITZ, G., 8, Giselastrasse, Munich, Germany. March 3, 1934, No. 6847. Convention date, March 31, 1933. [A Specification was laid open to inspection under Sect. 91 of the Acts, Sept. 25, 1934.] [Class 110 (iii)] The turbine has a single wheel of blades 17, supplied with working fluid by nozzles 16, and the fluid leaving the blade ring through an arc b1 passes by way of a channel 18 to two or more channels between guide vanes 19 and re-enters the blade ring over an arc b2. Between the arcs b1, b2, the guide channel tapers in depth from h1 to h2. The rotor 20 may be shaped as shown in Fig. 2. The invention may be applied to axial-flow turbines, and to turbines used in the cold-generation art.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE434363X | 1933-03-31 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB434363A true GB434363A (en) | 1935-08-30 |
Family
ID=6505631
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB6847/34A Expired GB434363A (en) | 1933-03-31 | 1934-03-03 | Improvements in or relating to turbines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB434363A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2466568A (en) * | 1944-05-02 | 1949-04-05 | Harold T Bean | Aircraft landing wheel rotating means |
-
1934
- 1934-03-03 GB GB6847/34A patent/GB434363A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2466568A (en) * | 1944-05-02 | 1949-04-05 | Harold T Bean | Aircraft landing wheel rotating means |
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