GB746416A - Improvements in or relating to sealing arrangements for relatively rotating parts - Google Patents
Improvements in or relating to sealing arrangements for relatively rotating partsInfo
- Publication number
- GB746416A GB746416A GB4996/54A GB499654A GB746416A GB 746416 A GB746416 A GB 746416A GB 4996/54 A GB4996/54 A GB 4996/54A GB 499654 A GB499654 A GB 499654A GB 746416 A GB746416 A GB 746416A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ring
- sealing
- rings
- grooves
- thrust
- 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
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/34—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
- F16J15/3436—Pressing means
- F16J15/3448—Pressing means the pressing force resulting from fluid pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B11/00—Parts or details not provided for in, or of interest apart from, the preceding groups, e.g. wear-protection couplings, between turbine and generator
- F03B11/006—Sealing arrangements
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/20—Hydro energy
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Sealing Devices (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Hydraulic Turbines (AREA)
Abstract
746,416. Stuffing-box substitutes. SOLITAIR, C. A., [trading as MASKINFIRMA C. RONDORF]. Feb. 19, 1954 [Feb. 20, 1953], No. 4996/54. Class 122(5) A sealing arrangement for relatively rotating parts, such as a water-turbine shaft 1 and its housing, comprises at least one radially split sealing ring 12 slidably housed in a groove 8 formed in one of the parts and resiliently urged into sealing contact both with one side wall 4c of the groove 8 and a plane or conical surface 3a on the other part. The sealing rings are expanded to contact the wall 4c and urged towards the surface 3a on a ring 3 attached to the shaft 1 by means of springs 9 compressed between the bottom of the grooves 8 and split thrust rings 11 housed in the grooves and contacting the sealing rings 12 on a conical surface. The rings 11 and 12 may be of bronze and graphite respectively. Drainage passages 14a, 14b, 14c, 15, 15a and 15b lead from the walls 4c of the grooves to a common passage 16 and then via a pipe 17 to the turbine inlet duct or other low pressure point. Alternatively, two passages such as 14b, 14c may be associated with the grooves and one passage 14c connected to drain while the other is supplied with pressure fluid to counteract leakage. The ungrooved face of the seal housing is provided with ribs 4a which co-operate with ribs 2a on a ring 2 on the shaft 1 to form a labyrinth seal to reduce the pressure of water reaching the inner sealing ring 12 through clearances 7 and 13 between the seal housing and the shaft and the ring 3 respectively. In a modification the thrust ring 11 is replaced by a second graphite split sealing ring protected on its inner periphery by a thrust liner. In a further modification the thrust and sealing rings 11 and 12 are replaced by a single sealing ring'having a conical sealing face urged into contact with a conical face on the ring 3.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE746416X | 1953-02-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB746416A true GB746416A (en) | 1956-03-14 |
Family
ID=20323238
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4996/54A Expired GB746416A (en) | 1953-02-20 | 1954-02-19 | Improvements in or relating to sealing arrangements for relatively rotating parts |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB746416A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3024027A (en) * | 1958-02-17 | 1962-03-06 | Borg Warner | Pressure loadable fluid seal device |
GB2125492A (en) * | 1982-08-16 | 1984-03-07 | Ae Plc | Fluid seals for marine propulsion shafting |
EP2687715A4 (en) * | 2011-03-16 | 2015-09-09 | Eagle Ind Co Ltd | Underwater hydro turbine generator |
CN114458454A (en) * | 2021-11-29 | 2022-05-10 | 中国航发沈阳发动机研究所 | Graphite piston ring sealing structure for aircraft engine |
-
1954
- 1954-02-19 GB GB4996/54A patent/GB746416A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3024027A (en) * | 1958-02-17 | 1962-03-06 | Borg Warner | Pressure loadable fluid seal device |
GB2125492A (en) * | 1982-08-16 | 1984-03-07 | Ae Plc | Fluid seals for marine propulsion shafting |
EP2687715A4 (en) * | 2011-03-16 | 2015-09-09 | Eagle Ind Co Ltd | Underwater hydro turbine generator |
CN114458454A (en) * | 2021-11-29 | 2022-05-10 | 中国航发沈阳发动机研究所 | Graphite piston ring sealing structure for aircraft engine |
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