GB682546A - Improvements in or relating to rotors for turbines and compressors and to the manufacture thereof - Google Patents
Improvements in or relating to rotors for turbines and compressors and to the manufacture thereofInfo
- Publication number
- GB682546A GB682546A GB1098450A GB1098450A GB682546A GB 682546 A GB682546 A GB 682546A GB 1098450 A GB1098450 A GB 1098450A GB 1098450 A GB1098450 A GB 1098450A GB 682546 A GB682546 A GB 682546A
- Authority
- GB
- United Kingdom
- Prior art keywords
- arcs
- tool
- rotor
- turbines
- compressors
- 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
- F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
- F01D5/048—Form or construction
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
682,546. Turning; making turbines &c. ROLLS-ROYCE, Ltd. April 6, 1951 [May 3, 1950], No. 10984/50. Classes 83 (ii) and 83 (iii). [Also in Group XXVI] A turbine or compressor rotor is lightened by providing an annular recess 14 extending from an axial bore 11 in the hub 10 and formed by a turning tool 21 with a convex cutting edge 21a, the tool being swung about a centre 17 while the rotor is rotated to cut the arcs 15, 16 and the rotor then being reversed in position and the operation repeated to cut the arcs 18, 19. Alternatively, straight tapers 22 may be formed in the bore before machining the arcs 16, 19 with the tool 21.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1098450A GB682546A (en) | 1950-05-03 | 1950-05-03 | Improvements in or relating to rotors for turbines and compressors and to the manufacture thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1098450A GB682546A (en) | 1950-05-03 | 1950-05-03 | Improvements in or relating to rotors for turbines and compressors and to the manufacture thereof |
Publications (1)
Publication Number | Publication Date |
---|---|
GB682546A true GB682546A (en) | 1952-11-12 |
Family
ID=9977905
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1098450A Expired GB682546A (en) | 1950-05-03 | 1950-05-03 | Improvements in or relating to rotors for turbines and compressors and to the manufacture thereof |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB682546A (en) |
-
1950
- 1950-05-03 GB GB1098450A patent/GB682546A/en not_active Expired
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