GB646491A - Improvements in blade rings for radial flow elastic fluid turbines - Google Patents
Improvements in blade rings for radial flow elastic fluid turbinesInfo
- Publication number
- GB646491A GB646491A GB1372944A GB1372944A GB646491A GB 646491 A GB646491 A GB 646491A GB 1372944 A GB1372944 A GB 1372944A GB 1372944 A GB1372944 A GB 1372944A GB 646491 A GB646491 A GB 646491A
- Authority
- GB
- United Kingdom
- Prior art keywords
- welding
- roots
- blades
- rib
- 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
- 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
- F01D5/021—Blade-carrying members, e.g. rotors for flow machines or engines with only one axial stage
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
646,491. Turbine blades. FAIRWEATHER, H. G. C. (Svenska Turbinfabriks Aktiebolaget Ljungstrom.). July 18, 1944, No. 13729. [A Specification was laid open to inspection under Sect. 91 of the Acts, Jan. 18, 1946.]. [Class 110(iii)] '[Also in Group XXII] Blade rings for radial flow elastic fluid turbines are manufactured by connecting together the roots of adjacent blades, preferably in groups, by welding, the roots being further connected to the supporting ring or rings by welding. A rib 7, Fig. 3, is formed on one or both faces of a blade root 2 by pressing or machining. During welding, the rib or ribs flow outwards to seal the joint, the surfaces 5 of adjacent roots consequently abutting. After a number of blades have been welded together, the blade roots are shaped by turning or other means. Instead of a rib, a wire 8, Fig. 4, may be fastened to the root, which, in this case, may be finished to shape before welding. In welding together a group of blades an electrical short-circuiting bar 10, Fig. 7, controls the length of the group- Specifications 560,620 and 582,563 are referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1372944A GB646491A (en) | 1944-07-18 | 1944-07-18 | Improvements in blade rings for radial flow elastic fluid turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1372944A GB646491A (en) | 1944-07-18 | 1944-07-18 | Improvements in blade rings for radial flow elastic fluid turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB646491A true GB646491A (en) | 1950-11-22 |
Family
ID=10028310
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1372944A Expired GB646491A (en) | 1944-07-18 | 1944-07-18 | Improvements in blade rings for radial flow elastic fluid turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB646491A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3003745A (en) * | 1957-10-31 | 1961-10-10 | Bendix Corp | Turbine wheel containment |
GB2142985A (en) * | 1983-07-05 | 1985-01-30 | Howden James & Co Ltd | Impeller for a double inlet centrifugal fan |
-
1944
- 1944-07-18 GB GB1372944A patent/GB646491A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3003745A (en) * | 1957-10-31 | 1961-10-10 | Bendix Corp | Turbine wheel containment |
GB2142985A (en) * | 1983-07-05 | 1985-01-30 | Howden James & Co Ltd | Impeller for a double inlet centrifugal fan |
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