GB599698A - Improvements in or relating to blade rings of radial flow turbines - Google Patents
Improvements in or relating to blade rings of radial flow turbinesInfo
- Publication number
- GB599698A GB599698A GB5229/45A GB522945A GB599698A GB 599698 A GB599698 A GB 599698A GB 5229/45 A GB5229/45 A GB 5229/45A GB 522945 A GB522945 A GB 522945A GB 599698 A GB599698 A GB 599698A
- Authority
- GB
- United Kingdom
- Prior art keywords
- carrying ring
- blade
- projections
- blades
- ring
- 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
599,698. Turbine blades. AKTIEBOLAGET LJUNGSTROMS ANGTURBIN. March 2, 1945, No. 5229. Convention date, March 2, 1944. [Class 110 (iii)] In a blade ring for a radial flow turbine of the kind in which axially extending blades 24, Fig. 5, are secured to a carrying ring 28 by projections extending from the blade roots and interlocked with both the radially inner and outer edges of the carrying ring, that face of each blade root adjacent the carrying ring is cut away to provide two radially spaced projections 44, 48, each positively locked to the carrying ring against bending stresses, the recess between the projections receiving a projecting portion 40 of the carrying ring. The projection 44 is serrated or threaded, but may instead be identical with the dovetail projection 48. The sides 42 of the carrying ring may be outwardly bent prior to insertion of the blades and subsequently rolled in. The blade roots may be welded together. The projections may each be in the form of a halfdovelail 34, Fig. 6. The inner projection 50 may be threaded in the case where the radial depth of the blade is so much less than that of the carrying ring that a rolling operation cannot be applied.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE599698X | 1944-03-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB599698A true GB599698A (en) | 1948-03-18 |
Family
ID=20312795
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5229/45A Expired GB599698A (en) | 1944-03-02 | 1945-03-02 | Improvements in or relating to blade rings of radial flow turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB599698A (en) |
-
1945
- 1945-03-02 GB GB5229/45A patent/GB599698A/en not_active Expired
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB478104A (en) | Improvements in and relating to elastic fluid turbines | |
GB1349170A (en) | Rotor for a gas turbine engine | |
GB611405A (en) | Improvements in or relating to rotors for multi-stage axial flow compressors and turbines | |
GB574759A (en) | Improvements in or relating to turbine blades | |
GB1326122A (en) | Blade securing arrangement for compressors and or turbines | |
GB614678A (en) | Improvements in or relating to turbine blading or the like | |
GB748903A (en) | Blades for compressors, turbines and like bladed rotary machines | |
GB1148339A (en) | Compressors or turbines for gas turbine engines | |
GB622626A (en) | Manufacture of a bladed turbine disc | |
GB599698A (en) | Improvements in or relating to blade rings of radial flow turbines | |
GB1527074A (en) | Bladed rotors | |
GB307832A (en) | Blade ring for radial steam- or gas-turbines and method of manufacturing the same | |
GB473714A (en) | Improvements in or relating to turbines | |
GB532357A (en) | Improvements in and relating to elastic fluid turbines | |
GB728754A (en) | Improvements in or relating to bladed rotors for compressors, turbines and like fluid flow machines | |
GB728710A (en) | Improvements in and relating to axial-flow turbines and the like | |
GB210288A (en) | Improvements in the construction of the rotors of elastic fluid turbines | |
GB590433A (en) | Improvements in and relating to the manufacture of turbine rotors | |
GB924808A (en) | Improvements relating to rotors for turbines or compressors | |
GB647143A (en) | Improvements in or relating to turbine blades | |
US2573621A (en) | Elastic fluid turbine | |
GB156559A (en) | Improvements in and relating to the blading of turbines of the type wherein the blades are held by their root ends in a groove in the turbine wheel | |
GB123737A (en) | An Improved Blade Foot for the Blades of Gas and Steam Turbines. | |
GB724123A (en) | Improvements in or relating to blades for compressors, turbines and the like | |
GB1100384A (en) | Stator blade assemblies for axial flow compressors or turbines |