GB610010A - Improvements relating to lubrication systems of gas turbine engines - Google Patents
Improvements relating to lubrication systems of gas turbine enginesInfo
- Publication number
- GB610010A GB610010A GB1103044A GB1103044A GB610010A GB 610010 A GB610010 A GB 610010A GB 1103044 A GB1103044 A GB 1103044A GB 1103044 A GB1103044 A GB 1103044A GB 610010 A GB610010 A GB 610010A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lubricant
- bore
- oil
- shafting
- rearwardly
- 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)
- Supercharger (AREA)
- Rolling Contact Bearings (AREA)
Abstract
610,010. Lubricating toothed gearing. POWER JETS (RESEARCH & DEVELOPMENT), Ltd., and POWELL, J. A. BENNETT-. June 8, 1944, No. 11030. [Class 80 (i)] [Also in Group XXVI] In a lubrication system for supplying lubricant to a plurality of localities disposed along the shafting of a gas turbine engine comprising internal substantially axial ducting through the shafting communicating towards one end with a delivery point for lubricant at atmospheric pressure, the bore of the ducting has change of radius with respect to the axis of rotation of the shafting so as to impel the lubricant through the shafting and the lubricant is led from the supply source to the delivery point over a path disposed externally of the shafting. The lubricant is injected from a fixed pipe 97, Fig. 2, into the bore of the shaft 63, an increase in the diameter of which at 8 causes the oil to be pressurized by centrifugal action and flow rearwardly. Passage 39 and chambers 41 and 42 pass oil from the bore to the clutch mechanism 43 and passages 44 pass oil to the bearing 46. The high - speed pinion 62 and driving serrations 64 are lubricated through passages 9 which are positioned rearwardly of another increase in the diameter of the bore. The lubricant then flows rearwardly through the tube 74, the inclined passages 80, Fig. 3, in the nut 76 to the splines 81 transmitting the power from the turbine to the compressor. From the splines, the lubricant flows to a chamber 23 and a well 26 supplying oil to the turbine bearing 25. The tube 74 is held in position by bushes 75 in the shaft 85 and by a spring-loaded flanged bush 37 in the shaft 10. The oil for the front bearing 50 is supplied from an independent source. A screw. thread may be formed on the wall of the bore adjacent to the point 8 to pick up and impel the oil rearwardly. In a modification, the tube 74 leads to a bore in the stub shaft 82 and radial holes pass the lubricant to the chamber 23.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1103044A GB610010A (en) | 1944-06-08 | 1944-06-08 | Improvements relating to lubrication systems of gas turbine engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1103044A GB610010A (en) | 1944-06-08 | 1944-06-08 | Improvements relating to lubrication systems of gas turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB610010A true GB610010A (en) | 1948-10-11 |
Family
ID=9978763
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1103044A Expired GB610010A (en) | 1944-06-08 | 1944-06-08 | Improvements relating to lubrication systems of gas turbine engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB610010A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2802547A (en) * | 1954-03-03 | 1957-08-13 | Studebaker Packard Corp | Shaft lubrication arrangement |
US2866522A (en) * | 1954-08-06 | 1958-12-30 | Rolls Royce | Lubricating arrangements for bearings of rotatable shafts |
US2874803A (en) * | 1955-07-26 | 1959-02-24 | United Aircraft Corp | Lubrication means |
-
1944
- 1944-06-08 GB GB1103044A patent/GB610010A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2802547A (en) * | 1954-03-03 | 1957-08-13 | Studebaker Packard Corp | Shaft lubrication arrangement |
US2866522A (en) * | 1954-08-06 | 1958-12-30 | Rolls Royce | Lubricating arrangements for bearings of rotatable shafts |
US2874803A (en) * | 1955-07-26 | 1959-02-24 | United Aircraft Corp | Lubrication means |
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