GB757759A - Production of turbine or compressor blades - Google Patents
Production of turbine or compressor bladesInfo
- Publication number
- GB757759A GB757759A GB17872/54A GB1787254A GB757759A GB 757759 A GB757759 A GB 757759A GB 17872/54 A GB17872/54 A GB 17872/54A GB 1787254 A GB1787254 A GB 1787254A GB 757759 A GB757759 A GB 757759A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blank
- beads
- rolling
- turbine
- june
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
- B21K3/00—Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like
- B21K3/04—Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like blades, e.g. for turbines; Upsetting of blade roots
-
- 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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Architecture (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
757,759. Making turbine &c. blades; rolling. WURTTEMBERGISCHE METALLWARENFABRIK. June 17, 1954 [June 19, 1953], No. 17872/54. Classes 83 (2) and 83 (4). In a method of making turbine or compressor blades a blank 2, Fig. 2, to be rolled in successive stages is initially formed with one or more grooves 6 or beads by the first roll pair 3, 4 to act as guides to prevent the blank becoming displaced during the following rolling stages. The blank may be rolled between segmental rolls, the bead or groove being gradually reduced until it is finally removed in the last rolling stage. In a modification beads 16, Fig. 12, are formed along each-longitudinal edge and these remain during the final rolling stage after which the beads are removed. The blank is finally upset at one end to form the root and is then stamped in dies to the final cross-section and twist.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE757759X | 1953-06-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB757759A true GB757759A (en) | 1956-09-26 |
Family
ID=6660103
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB17872/54A Expired GB757759A (en) | 1953-06-19 | 1954-06-17 | Production of turbine or compressor blades |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB757759A (en) |
-
1954
- 1954-06-17 GB GB17872/54A patent/GB757759A/en not_active Expired
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