GB419082A - Improvements in blading arrangements for radially traversed turbomachines - Google Patents
Improvements in blading arrangements for radially traversed turbomachinesInfo
- Publication number
- GB419082A GB419082A GB1513133A GB1513133A GB419082A GB 419082 A GB419082 A GB 419082A GB 1513133 A GB1513133 A GB 1513133A GB 1513133 A GB1513133 A GB 1513133A GB 419082 A GB419082 A GB 419082A
- Authority
- GB
- United Kingdom
- Prior art keywords
- discs
- turbine
- blading
- arrangements
- thrust
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
419,082. Steam turbines. MEINING- HAUS, U., 4, Margaretenplatz, M³lheim, Ruhr, Germany. May 25, 1933, No. 15131. [A Specification was laid open to inspection under Sect. 91 of the Acts, Dec. 2, 1933.] [Class 110 (iii).] In a multiple-disc reaction turbine of the radial-flow type, the discs of which are bladed on one side only, the blades are distributed over a larger number of discs than the minimum number determined by a consideration of centrifugal forces. The object is to reduce the amount of unbalanced end thrust, and a number of arrangements are described in which the discs are mounted in overhung fashion on one or both ends of the shaft of a driven machine. In the Figure steam is admitted to an inwardflow impulse stage 22 by a coiled flexible pipe 19, which passes through a low pressure conduit of the turbine, and is then used in outward-flow blading a<2>, a<3>, a<4>, and finally in axial-flow blading 8. An end-thrust device 18 is positioned as shown. A dummy piston may be arranged on the other end of the shaft to take up end thrust. The turbine is arranged for dismantling in an axial direction, the discs being undivided. Specification 412,073 is referred to. 419,082.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1513133A GB419082A (en) | 1933-05-25 | 1933-05-25 | Improvements in blading arrangements for radially traversed turbomachines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1513133A GB419082A (en) | 1933-05-25 | 1933-05-25 | Improvements in blading arrangements for radially traversed turbomachines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB419082A true GB419082A (en) | 1934-11-06 |
Family
ID=10053585
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1513133A Expired GB419082A (en) | 1933-05-25 | 1933-05-25 | Improvements in blading arrangements for radially traversed turbomachines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB419082A (en) |
-
1933
- 1933-05-25 GB GB1513133A patent/GB419082A/en not_active Expired
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