GB989477A - Bearing assembly - Google Patents
Bearing assemblyInfo
- Publication number
- GB989477A GB989477A GB407964A GB407964A GB989477A GB 989477 A GB989477 A GB 989477A GB 407964 A GB407964 A GB 407964A GB 407964 A GB407964 A GB 407964A GB 989477 A GB989477 A GB 989477A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- passage
- reservoir
- lubricator
- shaft
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/18—Lubricating arrangements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
- Rolling Contact Bearings (AREA)
- Sliding-Contact Bearings (AREA)
Abstract
989,477. Gas turbine plant. ROLLS-ROYCE Ltd. Jan. 30, 1964, No. 4079/64. Heading F1G. [Also in Division F2] A lubricator for a bearing comprises a rotor 35 having a passage 70,71 with an inlet from a stationary reservoir 55 and an outlet which at one angular position of the rotor communicates with a passage 76 leading by ducts 81, 83 to bearings 21, 23 within which the lubricator lies. As described, the lubricator is mounted inside the shafts 16, 17 of a twin-shaft vertically mounted jet lift engine, the rotor being driven by the L.P. shaft 17 through a member 50. The reservoir contains a piston 37 pressed against the rotor by a spring 42 and having an opening 74 by which the inlet of the passage 71 communicates with the reservoir at one angular position of the rotor. The reservoir is filled through a tube 60, has an overflow provided by passages 66, 67 in the rotor shaft 34, and is mounted on a torque tube 33 convoluted to allow for thermal expansion. A non-return valve (Fig. 2, not shown) is located in the passage 70 and is opened by centrifugal force when the rotor rotates to allow lubricant to be centrifuged by the rotor on to the bearings. The flow of oil is shown by arrows in the Figure.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB407964A GB989477A (en) | 1964-01-30 | 1964-01-30 | Bearing assembly |
DE19651475552 DE1475552B2 (en) | 1964-01-30 | 1965-01-28 | Lubricating device for bearings in gas turbine lift engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB407964A GB989477A (en) | 1964-01-30 | 1964-01-30 | Bearing assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
GB989477A true GB989477A (en) | 1965-04-22 |
Family
ID=9770339
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB407964A Expired GB989477A (en) | 1964-01-30 | 1964-01-30 | Bearing assembly |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE1475552B2 (en) |
GB (1) | GB989477A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0408454A1 (en) * | 1989-07-12 | 1991-01-16 | HISPANO-SUIZA Société anonyme dite: | Device for restricting the oil flow in a rotating shaft |
WO2011104477A1 (en) * | 2010-02-25 | 2011-09-01 | Turbomeca | Turbomachine comprising a vertical shaft |
-
1964
- 1964-01-30 GB GB407964A patent/GB989477A/en not_active Expired
-
1965
- 1965-01-28 DE DE19651475552 patent/DE1475552B2/en active Pending
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0408454A1 (en) * | 1989-07-12 | 1991-01-16 | HISPANO-SUIZA Société anonyme dite: | Device for restricting the oil flow in a rotating shaft |
FR2649754A1 (en) * | 1989-07-12 | 1991-01-18 | Hispano Suiza Sa | DEVICE FOR LIMITING LUBRICANT FLOW THROUGH A ROTATING SHAFT |
WO1991000977A1 (en) * | 1989-07-12 | 1991-01-24 | Hispano Suiza | Device to limit the flow of lubricant through a rotating shaft |
WO2011104477A1 (en) * | 2010-02-25 | 2011-09-01 | Turbomeca | Turbomachine comprising a vertical shaft |
CN102782261A (en) * | 2010-02-25 | 2012-11-14 | 涡轮梅坎公司 | Turbomachine comprising a vertical shaft |
US20120321460A1 (en) * | 2010-02-25 | 2012-12-20 | Turbomeca | Vertical shaft turbomachine |
KR20130004292A (en) * | 2010-02-25 | 2013-01-09 | 터보메카 | A vertical shaft turbomachine |
CN102782261B (en) * | 2010-02-25 | 2015-02-18 | 涡轮梅坎公司 | Turbomachine comprising a vertical shaft |
US9163526B2 (en) | 2010-02-25 | 2015-10-20 | Turbomeca | Vertical shaft turbomachine |
Also Published As
Publication number | Publication date |
---|---|
DE1475552A1 (en) | 1969-10-23 |
DE1475552B2 (en) | 1971-02-04 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3969804A (en) | Bearing housing assembly method for high speed rotating shafts | |
EP0105686B1 (en) | Supercharger | |
GB1248437A (en) | Lubrication system | |
US3090544A (en) | Air lubricated bearing | |
GB1517667A (en) | Variable v-belt transmission | |
US2604188A (en) | Oil supply and scavenge system | |
US3089304A (en) | Turbocharger waste gate system | |
US2847186A (en) | Fluid driven power unit | |
GB1129419A (en) | Gas turbine engine | |
GB939704A (en) | Rotor and bearing construction for rotary internal combustion engines, fluid motors, pumps, compressors and the like | |
US2775400A (en) | Turbine driven fan unit | |
US3382809A (en) | Control for fluid pump bypass | |
US3147913A (en) | Gas turbine engine | |
GB1219171A (en) | Improvements in or relating to gas turbine engine accessory drive systems | |
GB989477A (en) | Bearing assembly | |
GB1256486A (en) | ||
GB839344A (en) | Improvements in or relating to gas-turbine engines | |
US3285004A (en) | Bearing assembly | |
US2581172A (en) | Vane type hydraulic transmission | |
US2642155A (en) | Lubrication apparatus | |
US2615533A (en) | Self-lubricated turbine drive and gear reduction unit | |
GB1281842A (en) | Gas turbine engines | |
US4194360A (en) | Power take-off arrangements | |
US1843122A (en) | Lubricating, sealing and thrust balancing means for compressors and the like | |
US1189697A (en) | Motor control. |