GB942842A - Gas turbine engine - Google Patents
Gas turbine engineInfo
- Publication number
- GB942842A GB942842A GB1710061A GB1710061A GB942842A GB 942842 A GB942842 A GB 942842A GB 1710061 A GB1710061 A GB 1710061A GB 1710061 A GB1710061 A GB 1710061A GB 942842 A GB942842 A GB 942842A
- Authority
- GB
- United Kingdom
- Prior art keywords
- bearing
- shaft
- chamber
- sump
- splined
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/60—Fluid transfer
- F05D2260/601—Fluid transfer using an ejector or a jet pump
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/60—Fluid transfer
- F05D2260/602—Drainage
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Lubrication Of Internal Combustion Engines (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
942,842. Lubricating. ROLLS-ROYCE Ltd. May 4, 1962 [May 10, 1961], No. 17100/61. Heading F2A. [Also in Division F1] A gas turbine engine has a shaft which carries the compressor and the turbine of the engine, a bearing in which the shaft is rotatably mounted, and means for supplying lubricant to the bearing. A bearing housing chamber in which the bearing is housed is provided also a sump chamber to which may drain lubricant which has passed through the bearing, there being also at least one ejector pump for pumping lubricant out of the sump chamber and for maintaining a low pressure within the bearing housing chamber. By the term "ejector pump " is meant a known kind of pump which has no moving parts but which aspirates the " pumped " medium at the throat of a Venturi through which a fluid such as compressed air flows. The invention is described with reference to a gas turbine engine of the vertical lift type comprising an air compressor 13 and a turbine 15 mounted on a common shaft 17, the upstream end of which is supported in a bearing 19. The upstream end of the shaft 17 is formed with an extension 18 on which the inner race 21 of the bearing 19 is mounted, the outer race 20 of the bearing being in splined engagement with an inner housing member 22 which is secured within an outer housing member 23, the member 23 being supported from the outer casing 11 by the inlet guide vanes 12. The upper face of the outer race 20 is engaged by a ring member 24 which is also in splined engagement with the housing member 22 and is acted on by springs 25. The action of the springs 25 tends to counteract the thrust exerted on the shaft 17 by the compressor. An annular member 27 is secured to the shaft extension 18 adjacent the lower face of the inner race 21 of the bearing, the member 27 having an axial portion 30 and a radially-extending flange 31. A flange member 32 secured to the outer housing member 23 has an axially-extending flange 34 to form a seal with the axially-extending portion 30. The flange 31 forms with adjacent parts a sump chamber 35 and a chamber 36. The chambers 35, 36 are connected respectively by lines 37, 38 which extend through a hollow guide vane 12 to ejector pumps 39 disposed externally of the casing 11, the pumps acting to pump oil from the sump chamber 35 and air from the chamber 36, thereby maintaining the pressure within the chamber 36 lower than the pressure within the working fluid duct of the engine. A line 40 also passes through the hollow guide vane 12 and provides a means by which a single shot of oil may be introduced to the upstream side of the member 24, the oil passing through orifices 41 to the bearing 19 and thence to the sump chamber 35. A sleeve 42 is splined internally within the shaft extension 18 and the flange 44 of a quill shaft 43 is splined within the sleeve, the quill shaft in turn being splined to the drive shaft 47 of a fuel pump 46. A sump 51 is formed in the wall member 52 which is secured to the shaft extension 18, lubricating oil supplied to the fuel pump draining back to the sump 51 and being centrifuged through ports 50 to the sump chamber 35.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1710061A GB942842A (en) | 1961-05-10 | 1961-05-10 | Gas turbine engine |
DE1966R0032648 DE1299940B (en) | 1961-05-10 | 1966-04-19 | Extraction device at the oil sump of a shaft bearing of gas turbine engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1710061A GB942842A (en) | 1961-05-10 | 1961-05-10 | Gas turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
GB942842A true GB942842A (en) | 1963-11-27 |
Family
ID=10089254
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1710061A Expired GB942842A (en) | 1961-05-10 | 1961-05-10 | Gas turbine engine |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE1299940B (en) |
GB (1) | GB942842A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030097872A1 (en) * | 2001-11-29 | 2003-05-29 | Granitz Charles Robert | System for reducing oil consumption in gas turbine engines |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB623615A (en) * | 1947-05-06 | 1949-05-19 | Frederick William Walton Morle | Improvements in or relating to gas-turbine-engines |
DE901017C (en) * | 1949-02-04 | 1954-01-07 | English Electric Co Ltd | Gas turbine with lubricating and sealing device on the bearing |
DE872136C (en) * | 1949-09-17 | 1953-03-30 | Basf Ag | Storage for single and multi-stage flow machines with upright, approximately vertically arranged rotor shaft |
DE1018187B (en) * | 1953-11-07 | 1957-10-24 | Allis Chalmers Mfg Co | Compressor shaft seal |
CH329862A (en) * | 1954-05-01 | 1958-05-15 | Ruston & Hornsby Ltd | Turbo machine for gaseous medium |
DE1048932B (en) * | 1957-06-28 | 1959-01-22 | Sulzer Ag | Relaxation turbine |
-
1961
- 1961-05-10 GB GB1710061A patent/GB942842A/en not_active Expired
-
1966
- 1966-04-19 DE DE1966R0032648 patent/DE1299940B/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
DE1299940B (en) | 1969-07-24 |
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