GB758407A - Method of manufacturing blade rings for radial flow turbines or radial flow compressors - Google Patents
Method of manufacturing blade rings for radial flow turbines or radial flow compressorsInfo
- Publication number
- GB758407A GB758407A GB1963254A GB1963254A GB758407A GB 758407 A GB758407 A GB 758407A GB 1963254 A GB1963254 A GB 1963254A GB 1963254 A GB1963254 A GB 1963254A GB 758407 A GB758407 A GB 758407A
- Authority
- GB
- United Kingdom
- Prior art keywords
- radial flow
- blades
- weak
- strengthening ring
- hooked
- 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
- F01D5/041—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the Ljungström type
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
758,407. Radial flow turbines and compressors. SVENSKA TURBINFABRIKS AKTIEBOLAGET LJUNGSTROM. July 5, 1954, No. 19632/54. Class 110(3) The invention relates to a divided strengthening ring for supporting an annular set of blades of a radial flow turbine or compressor in which the blades 1 are formed with radially-outwardly projecting hookshaped ends 3 for engaging a corresponding groove of the strengthening ring. The strengthening ring comprises a comparatively weak annular member 4 which surrounds and engages the hooked ends of the blades, and a stronger member 5 formed at its side facing the hooked blade ends with two concentric flanges 6, 7 for engaging those portions of the blade ends not engaged by the weak annular member, the outer flange 6 being joined by welding 8 to the weak member. The weak member 4, of the strengthening ring may be mounted by heating it and allowing it to shrink around the hooked blade ends, the blades being held in the clamping device in which they were held during the shaping of the blade roots by a turning operation. Specification 594,204 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1963254A GB758407A (en) | 1954-07-05 | 1954-07-05 | Method of manufacturing blade rings for radial flow turbines or radial flow compressors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1963254A GB758407A (en) | 1954-07-05 | 1954-07-05 | Method of manufacturing blade rings for radial flow turbines or radial flow compressors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB758407A true GB758407A (en) | 1956-10-03 |
Family
ID=10132601
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1963254A Expired GB758407A (en) | 1954-07-05 | 1954-07-05 | Method of manufacturing blade rings for radial flow turbines or radial flow compressors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB758407A (en) |
-
1954
- 1954-07-05 GB GB1963254A patent/GB758407A/en not_active Expired
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