GB189131A - Improvements in or relating to turbine blades - Google Patents
Improvements in or relating to turbine bladesInfo
- Publication number
- GB189131A GB189131A GB31165/22A GB3116522A GB189131A GB 189131 A GB189131 A GB 189131A GB 31165/22 A GB31165/22 A GB 31165/22A GB 3116522 A GB3116522 A GB 3116522A GB 189131 A GB189131 A GB 189131A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- relating
- turbine blades
- crowns
- pressure
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
189,131. Soc. Rateau. Nov. 16, 1921, [Convention date]. Blades; axial-flow type.- The low-pressure blading of large turbines is divided into two or more concentric crowns of blades a, f, through which the steam flows in the same direction and at the same pressure. The number of blades in the outer crowns is a multiple of the number of blades in the inner crown. The outer blades are secured to the extremities of the inner blades. The bladefixing means described in Specifications 607/09 and 112,934 may be used.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR189131X | 1921-11-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB189131A true GB189131A (en) | 1923-03-01 |
Family
ID=8878876
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB31165/22A Expired GB189131A (en) | 1921-11-16 | 1922-11-14 | Improvements in or relating to turbine blades |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB189131A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2948506A (en) * | 1958-09-18 | 1960-08-09 | Gen Electric | Damping turbine buckets |
US2999668A (en) * | 1958-08-28 | 1961-09-12 | Curtiss Wright Corp | Self-balanced rotor blade |
US3002675A (en) * | 1957-11-07 | 1961-10-03 | Power Jets Res & Dev Ltd | Blade elements for turbo machines |
US3610776A (en) * | 1970-03-02 | 1971-10-05 | Rolls Royce | Compressor blade for a gas turbine engine |
US3751182A (en) * | 1971-08-20 | 1973-08-07 | Westinghouse Electric Corp | Guide vanes for supersonic turbine blades |
US4032258A (en) * | 1974-06-26 | 1977-06-28 | Rolls-Royce (1971) Limited | Bladed rotor for fluid flow machines |
US4084922A (en) * | 1976-12-27 | 1978-04-18 | Electric Power Research Institute, Inc. | Turbine rotor with pin mounted ceramic turbine blades |
US4094615A (en) * | 1976-12-27 | 1978-06-13 | Electric Power Research Institute, Inc. | Blade attachment structure for gas turbine rotor |
US4142836A (en) * | 1976-12-27 | 1979-03-06 | Electric Power Research Institute, Inc. | Multiple-piece ceramic turbine blade |
RU2486346C2 (en) * | 2007-04-13 | 2013-06-27 | Снекма | Fan blade, fan and jet turbine engine |
-
1922
- 1922-11-14 GB GB31165/22A patent/GB189131A/en not_active Expired
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3002675A (en) * | 1957-11-07 | 1961-10-03 | Power Jets Res & Dev Ltd | Blade elements for turbo machines |
US2999668A (en) * | 1958-08-28 | 1961-09-12 | Curtiss Wright Corp | Self-balanced rotor blade |
US2948506A (en) * | 1958-09-18 | 1960-08-09 | Gen Electric | Damping turbine buckets |
US3610776A (en) * | 1970-03-02 | 1971-10-05 | Rolls Royce | Compressor blade for a gas turbine engine |
US3751182A (en) * | 1971-08-20 | 1973-08-07 | Westinghouse Electric Corp | Guide vanes for supersonic turbine blades |
US4032258A (en) * | 1974-06-26 | 1977-06-28 | Rolls-Royce (1971) Limited | Bladed rotor for fluid flow machines |
US4084922A (en) * | 1976-12-27 | 1978-04-18 | Electric Power Research Institute, Inc. | Turbine rotor with pin mounted ceramic turbine blades |
US4094615A (en) * | 1976-12-27 | 1978-06-13 | Electric Power Research Institute, Inc. | Blade attachment structure for gas turbine rotor |
US4142836A (en) * | 1976-12-27 | 1979-03-06 | Electric Power Research Institute, Inc. | Multiple-piece ceramic turbine blade |
RU2486346C2 (en) * | 2007-04-13 | 2013-06-27 | Снекма | Fan blade, fan and jet turbine engine |
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