GB592956A - Improvements in or relating to the securing of blades to blade rings of radial flow turbines - Google Patents
Improvements in or relating to the securing of blades to blade rings of radial flow turbinesInfo
- Publication number
- GB592956A GB592956A GB5230/45A GB523045A GB592956A GB 592956 A GB592956 A GB 592956A GB 5230/45 A GB5230/45 A GB 5230/45A GB 523045 A GB523045 A GB 523045A GB 592956 A GB592956 A GB 592956A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- securing
- relating
- radial flow
- blade rings
- 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
Abstract
592,956. Turbine blades. AKTIEBOLAGET LJUNGSTROMS ANGTURBIN. March 2, 1945, No. 5230. Convention date, March 2, 1944. [Class 110 (iii)] The roots of a ring of blades are formed with teeth 24 and the ring bond 14 with corresponding grooves 34. After assembly, as shown, the parts are brought together by a rolling operation applied to the ring bond. In the circular assembly of blades, the teeth 24 may form annular or helical projections. The projections may be of equal height as shown in the upper part of the Figure or, of a height increasing towards the blade as shown in the lower part.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE592956X | 1944-03-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB592956A true GB592956A (en) | 1947-10-03 |
Family
ID=20312661
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5230/45A Expired GB592956A (en) | 1944-03-02 | 1945-03-02 | Improvements in or relating to the securing of blades to blade rings of radial flow turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB592956A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3047936A (en) * | 1959-03-11 | 1962-08-07 | Curtiss Wright Corp | Gas turbine rotor |
US5363554A (en) * | 1991-06-05 | 1994-11-15 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Titanium compressor blade having a wear-resistant portion |
-
1945
- 1945-03-02 GB GB5230/45A patent/GB592956A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3047936A (en) * | 1959-03-11 | 1962-08-07 | Curtiss Wright Corp | Gas turbine rotor |
US5363554A (en) * | 1991-06-05 | 1994-11-15 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Titanium compressor blade having a wear-resistant portion |
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