GB284312A - Improvements in or relating to the rotor blading of axial-now turbines - Google Patents
Improvements in or relating to the rotor blading of axial-now turbinesInfo
- Publication number
- GB284312A GB284312A GB34384/27A GB3438427A GB284312A GB 284312 A GB284312 A GB 284312A GB 34384/27 A GB34384/27 A GB 34384/27A GB 3438427 A GB3438427 A GB 3438427A GB 284312 A GB284312 A GB 284312A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- axial
- turbines
- relating
- now
- 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
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
-
- 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
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/24—Blade-to-blade connections, e.g. for damping vibrations using wire or the like
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
284,312. Akt.-Ges. der Maschinenfabriken Escher, Wyss, et Cie. Jan. 29, 1927, [Convention date]. Axial - flow type; blades.-Between every two of the main blades 4 of the rotor 1 of an axial-flow steam turbine, one or more intermediate blades 5 are secured to the shroudring 6 and extend to within a certain distance of the blade roots where they are rigidly secured to the blading by suitable means. These means may be a wire 7, soldered or welded to the blades, or a wire 8 with distance sleeves 9, soldered or welded to the blades. T h e s e intermediate blades assist in guiding the steam at the parts where the pitch t1 of the blades is considerably greater than the pitch t2 at the blade roots.
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH111452X | 1927-01-29 | ||
CH284312X | 1927-01-29 | ||
CH477319X | 1927-01-29 | ||
DE646373X | 1927-01-29 | ||
CH124599T | 1927-01-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB284312A true GB284312A (en) | 1928-05-03 |
Family
ID=40350196
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB34384/27A Expired GB284312A (en) | 1927-01-29 | 1927-12-19 | Improvements in or relating to the rotor blading of axial-now turbines |
Country Status (5)
Country | Link |
---|---|
AT (1) | AT111452B (en) |
CH (1) | CH124599A (en) |
DE (1) | DE477319C (en) |
FR (1) | FR646373A (en) |
GB (1) | GB284312A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2920864A (en) * | 1956-05-14 | 1960-01-12 | United Aircraft Corp | Secondary flow reducer |
US3282032A (en) * | 1962-01-29 | 1966-11-01 | Bahnson Co | Rotating eliminator |
US3837761A (en) * | 1971-08-20 | 1974-09-24 | Westinghouse Electric Corp | Guide vanes for supersonic turbine blades |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3751182A (en) * | 1971-08-20 | 1973-08-07 | Westinghouse Electric Corp | Guide vanes for supersonic turbine blades |
EP2019188A1 (en) * | 2007-07-25 | 2009-01-28 | Siemens Aktiengesellschaft | Rotor stage with damping element |
-
1927
- 1927-01-29 CH CH124599D patent/CH124599A/en unknown
- 1927-02-08 DE DEA49972D patent/DE477319C/en not_active Expired
- 1927-12-09 AT AT111452D patent/AT111452B/en active
- 1927-12-19 GB GB34384/27A patent/GB284312A/en not_active Expired
- 1927-12-27 FR FR646373D patent/FR646373A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2920864A (en) * | 1956-05-14 | 1960-01-12 | United Aircraft Corp | Secondary flow reducer |
US3282032A (en) * | 1962-01-29 | 1966-11-01 | Bahnson Co | Rotating eliminator |
US3837761A (en) * | 1971-08-20 | 1974-09-24 | Westinghouse Electric Corp | Guide vanes for supersonic turbine blades |
Also Published As
Publication number | Publication date |
---|---|
FR646373A (en) | 1928-11-10 |
AT111452B (en) | 1928-11-26 |
CH124599A (en) | 1928-03-01 |
DE477319C (en) | 1929-06-05 |
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