GB236207A - Improvements in and relating to elastic fluid turbines - Google Patents
Improvements in and relating to elastic fluid turbinesInfo
- Publication number
- GB236207A GB236207A GB15892/25A GB1589225A GB236207A GB 236207 A GB236207 A GB 236207A GB 15892/25 A GB15892/25 A GB 15892/25A GB 1589225 A GB1589225 A GB 1589225A GB 236207 A GB236207 A GB 236207A
- Authority
- GB
- United Kingdom
- Prior art keywords
- diaphragm
- packing
- teeth
- relating
- elastic fluid
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Diaphragms And Bellows (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
236,207. British Thomson-Houston Co., Ltd., (Assignees of Warren, G. B.). June 24, 1924, [Convention date]. Stuffing-boxes, substitutes for.-Turbine packing is so arranged that increased load decreases the packing clearance. Packing for a turbine diaphragm may comprise inclined teeth 14 on a tapered element 20 on the shaft cooperating with radial teeth 16 in a tapered aperture in an element 18 secured to the diaphragm 17. Increased pressure on increased load causes deflection of the diaphragm and consequent approach of the teeth 14 and 16. Specification 111,897 is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US236207XA | 1924-06-24 | 1924-06-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB236207A true GB236207A (en) | 1926-04-08 |
Family
ID=21816244
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15892/25A Expired GB236207A (en) | 1924-06-24 | 1925-06-19 | Improvements in and relating to elastic fluid turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB236207A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2851245A (en) * | 1953-02-11 | 1958-09-09 | Alan Muntz & Co Ltd | Radial flow exhaust turbines for use with diesel engines |
US2977142A (en) * | 1955-10-18 | 1961-03-28 | Gen Electric | Supporting means to maintain concentricity between two members |
US4148494A (en) * | 1977-12-21 | 1979-04-10 | General Electric Company | Rotary labyrinth seal member |
-
1925
- 1925-06-19 GB GB15892/25A patent/GB236207A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2851245A (en) * | 1953-02-11 | 1958-09-09 | Alan Muntz & Co Ltd | Radial flow exhaust turbines for use with diesel engines |
US2977142A (en) * | 1955-10-18 | 1961-03-28 | Gen Electric | Supporting means to maintain concentricity between two members |
US4148494A (en) * | 1977-12-21 | 1979-04-10 | General Electric Company | Rotary labyrinth seal member |
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