GB895837A - An improvement in or relating to turbines - Google Patents
An improvement in or relating to turbinesInfo
- Publication number
- GB895837A GB895837A GB4434959A GB4434959A GB895837A GB 895837 A GB895837 A GB 895837A GB 4434959 A GB4434959 A GB 4434959A GB 4434959 A GB4434959 A GB 4434959A GB 895837 A GB895837 A GB 895837A
- Authority
- GB
- United Kingdom
- Prior art keywords
- bearing
- rotor
- turbines
- pinions
- dec
- 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
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/12—Combinations with mechanical gearing
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
895,837. Turbines. BROWN INDUSTRIES Ltd., DAVID. Dec. 29, 1960 [Dec. 31, 1959], No. 44349/59. Class 110 (3). In a radial flow turbine the rotor shaft 12 is supported, in or near a plane perpendicular to its axis containing the rotor 13, by bearing means 11 and, in a plane spaced axially from the rotor 13, by the centralizing action exerted on one member 15 of a gear arrangement by three or more pinions 17. The member 15 may be formed on or carried by the rotor shaft 12 and three pinions 17 are mounted in a planet carrier 16 engaging an annulus 19. A gland 20 seals off the gear arrangement and secures the bearing 11 in the casing. The bearing 11 may be of ball, roller or plain type and may be augmented by a separate thrust bearing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4434959A GB895837A (en) | 1959-12-31 | 1959-12-31 | An improvement in or relating to turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4434959A GB895837A (en) | 1959-12-31 | 1959-12-31 | An improvement in or relating to turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB895837A true GB895837A (en) | 1962-05-09 |
Family
ID=10432858
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4434959A Expired GB895837A (en) | 1959-12-31 | 1959-12-31 | An improvement in or relating to turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB895837A (en) |
-
1959
- 1959-12-31 GB GB4434959A patent/GB895837A/en not_active Expired
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