GB173129A - Improvements in and relating to methods of making blade rings for elastic fluid turbines and the like - Google Patents
Improvements in and relating to methods of making blade rings for elastic fluid turbines and the likeInfo
- Publication number
- GB173129A GB173129A GB3095320A GB3095320A GB173129A GB 173129 A GB173129 A GB 173129A GB 3095320 A GB3095320 A GB 3095320A GB 3095320 A GB3095320 A GB 3095320A GB 173129 A GB173129 A GB 173129A
- Authority
- GB
- United Kingdom
- Prior art keywords
- metal
- relating
- methods
- built
- pieces
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
173,129. British Thomson - Houston Co., Ltd., (General Electric Co.). Nov. 2, 1920. Turbines.-Turbine blade segments are formed by assembling blade lengths and distance-pieces in a holder, welding them together, building up metal at the ends of the blades and machining the built-up metal. For a radial-flow segment, distance-pieces, shaped as shown in Fig. 1, are placed with lugs 24 in notches in two rings 27, Fig. 4, the blades being placed between the distance-pieces and the whole secured by plates 30 and metal 32 is built up at the ends. The segment is removed by cutting through the lugs 24, and the built-up metal is machined to the form shown in dotted lines. A similar method for axial-flow segments is described.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3095320A GB173129A (en) | 1920-11-02 | 1920-11-02 | Improvements in and relating to methods of making blade rings for elastic fluid turbines and the like |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3095320A GB173129A (en) | 1920-11-02 | 1920-11-02 | Improvements in and relating to methods of making blade rings for elastic fluid turbines and the like |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB173129A true GB173129A (en) | 1921-12-29 |
Family
ID=10315678
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3095320A Expired GB173129A (en) | 1920-11-02 | 1920-11-02 | Improvements in and relating to methods of making blade rings for elastic fluid turbines and the like |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB173129A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3038699A (en) * | 1958-11-04 | 1962-06-12 | Poly Ind Inc | Nozzle ring assembly |
-
1920
- 1920-11-02 GB GB3095320A patent/GB173129A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3038699A (en) * | 1958-11-04 | 1962-06-12 | Poly Ind Inc | Nozzle ring assembly |
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