GB633022A - Guide blade system for rotary elastic fluid machines - Google Patents
Guide blade system for rotary elastic fluid machinesInfo
- Publication number
- GB633022A GB633022A GB22903/47A GB2290347A GB633022A GB 633022 A GB633022 A GB 633022A GB 22903/47 A GB22903/47 A GB 22903/47A GB 2290347 A GB2290347 A GB 2290347A GB 633022 A GB633022 A GB 633022A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- distance pieces
- disc
- pins
- guide blade
- 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
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Hydraulic Turbines (AREA)
Abstract
633,022. Turbine blading. SVENSKA TURBINFABRIKS AKTIEBOLAGET LJUNGSTROM, Aug. 18, 1947, No. 22903. Convention date, Sept. 19, 1946. [Class 110(iii)] A guide vane assembly for an axial flow turbine or similar machine having annular sets of blades supported by a disc-shaped member comprises blades 1 formed at both ends with integral distance pieces 2, the distance pieces at the root being provided with radial pins 3, a disc-shaped member 5 with an annular slot 6 formed in its peripheral surface and a bond ring 7. The blades 1 are assembled to the disc 5 by placing the pins 3 in immediate proximity to one another in the slot 6 and shrinking the ring 7 over the distance pieces at the tips of the blades. Short pins 4 may be provided on the tip distance pieces.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE261192X | 1946-09-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB633022A true GB633022A (en) | 1949-12-05 |
Family
ID=20306449
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB22903/47A Expired GB633022A (en) | 1946-09-19 | 1947-08-18 | Guide blade system for rotary elastic fluid machines |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH261192A (en) |
FR (1) | FR952478A (en) |
GB (1) | GB633022A (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3066911A (en) * | 1959-05-12 | 1962-12-04 | Thompson Ramo Wooldridge Inc | Nozzle and turbine wheel shroud support |
US3300180A (en) * | 1964-11-17 | 1967-01-24 | Worthington Corp | Segmented diaphragm assembly |
-
1947
- 1947-08-18 GB GB22903/47A patent/GB633022A/en not_active Expired
- 1947-08-19 CH CH261192D patent/CH261192A/en unknown
- 1947-08-26 FR FR952478D patent/FR952478A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
CH261192A (en) | 1949-04-30 |
FR952478A (en) | 1949-11-17 |
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