GB197873A - Improvements relating to elastic fluid turbines - Google Patents
Improvements relating to elastic fluid turbinesInfo
- Publication number
- GB197873A GB197873A GB1971422A GB1971422A GB197873A GB 197873 A GB197873 A GB 197873A GB 1971422 A GB1971422 A GB 1971422A GB 1971422 A GB1971422 A GB 1971422A GB 197873 A GB197873 A GB 197873A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- blades
- sections
- slot
- wide
- 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
197,873. Metropolitan - Vickers Electrical Co., Ltd., (Westinghouse Electric & Manufacturing Co.). July 18, 1922. Blades. -The wide low-pressure reaction blading described in Specifications 182,775 and 183,429 which receives elastic fluid axially and discharges it peripherally, or peripherally and laterally at a small angle, is formed with curved ribs or other deflector surfaces which extend from blade to blade. When the wide blading comprises a series of sections suitably assembled the deflectors are secured to the sections before being assembled. In Fig. 6, deflector plates 30, made as single pieces or in sections are shaped to fit grooved supports 31 on the blade sections 28. The plates 30 may be bowed so that when forced into the supports 31 they will brace the blades and permit of differential expansion. Fig. 2 shows a single guide member 32 for each blade section 22, the members 32 being arranged successively lower from the inlet edge of the first blade section to the rear edge of the last section. To reduce vibration, the wide blades 22, Fig. 12, are secured to reinforcing members 35 which consist of flat annular strips fitting slots in the blade tips and arranged radially of the blades. Fig. 14 shows a method of connecting the blades 22 to the rotor 18. The 'blade 22 has a dovetail root 26 fitting a slot in the rotor. A groove 37 at the base of the slot receives wedges 38, 39 which force together the inclined surfaces of the blade root and of the slot. An end plate 42 contacts with the last wedge 38 of each series and holds the wedges in position.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1971422A GB197873A (en) | 1922-07-18 | 1922-07-18 | Improvements relating to elastic fluid turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1971422A GB197873A (en) | 1922-07-18 | 1922-07-18 | Improvements relating to elastic fluid turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB197873A true GB197873A (en) | 1923-05-24 |
Family
ID=10133980
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1971422A Expired GB197873A (en) | 1922-07-18 | 1922-07-18 | Improvements relating to elastic fluid turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB197873A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3677658A (en) * | 1970-12-08 | 1972-07-18 | Westinghouse Electric Corp | Split casting steam chest, nozzle chamber and casing assembly for turbines |
US4013378A (en) * | 1976-03-26 | 1977-03-22 | General Electric Company | Axial flow turbine exhaust hood |
US5338155A (en) * | 1992-08-03 | 1994-08-16 | Asea Brown Boveri Ltd. | Multi-zone diffuser for turbomachine |
-
1922
- 1922-07-18 GB GB1971422A patent/GB197873A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3677658A (en) * | 1970-12-08 | 1972-07-18 | Westinghouse Electric Corp | Split casting steam chest, nozzle chamber and casing assembly for turbines |
US4013378A (en) * | 1976-03-26 | 1977-03-22 | General Electric Company | Axial flow turbine exhaust hood |
US5338155A (en) * | 1992-08-03 | 1994-08-16 | Asea Brown Boveri Ltd. | Multi-zone diffuser for turbomachine |
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