GB627386A - Cooling of lubricating oil of internal-combustion turbine engines - Google Patents
Cooling of lubricating oil of internal-combustion turbine enginesInfo
- Publication number
- GB627386A GB627386A GB2295547A GB2295547A GB627386A GB 627386 A GB627386 A GB 627386A GB 2295547 A GB2295547 A GB 2295547A GB 2295547 A GB2295547 A GB 2295547A GB 627386 A GB627386 A GB 627386A
- Authority
- GB
- United Kingdom
- Prior art keywords
- internal
- cooling
- combustion turbine
- lubricating oil
- turbine engines
- 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
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P11/00—Component parts, details, or accessories not provided for in, or of interest apart from, groups F01P1/00 - F01P9/00
- F01P11/08—Arrangements of lubricant coolers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Lubrication Of Internal Combustion Engines (AREA)
Abstract
627,386. Cooling lubricant. ARMSTRONG SIDDELEY MOTORS, Ltd., and LINDSEY, W. H. Aug. 19, 1947, No. 22955. [Class 12 (iii)] [Also in Group XXVI] In an internal-combustion turbine for aircraft, lubricant is cooled in a tank 11 through which liquid fuel is led in a tortuous path through a pipe 18 and thus heated. The lubricant is fed to the plant by a pump 12 and the liquid fuel is drawn from a tank 16 by a pump 17.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2295547A GB627386A (en) | 1947-08-19 | 1947-08-19 | Cooling of lubricating oil of internal-combustion turbine engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2295547A GB627386A (en) | 1947-08-19 | 1947-08-19 | Cooling of lubricating oil of internal-combustion turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB627386A true GB627386A (en) | 1949-08-08 |
Family
ID=10187772
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2295547A Expired GB627386A (en) | 1947-08-19 | 1947-08-19 | Cooling of lubricating oil of internal-combustion turbine engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB627386A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2675671A (en) * | 1954-04-20 | Malgieri | ||
US2731239A (en) * | 1951-06-15 | 1956-01-17 | Garrett Corp | Oil cooler cooled by air and fuel |
US2959915A (en) * | 1955-12-27 | 1960-11-15 | Texaco Inc | Fuel for and method of operating a jet engine |
US2974475A (en) * | 1955-04-06 | 1961-03-14 | Exxon Research Engineering Co | Method for operating a rocket motor or the like |
US3000180A (en) * | 1957-04-04 | 1961-09-19 | Napier & Son Ltd | Engines for high speed aircraft or missiles |
-
1947
- 1947-08-19 GB GB2295547A patent/GB627386A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2675671A (en) * | 1954-04-20 | Malgieri | ||
US2731239A (en) * | 1951-06-15 | 1956-01-17 | Garrett Corp | Oil cooler cooled by air and fuel |
US2974475A (en) * | 1955-04-06 | 1961-03-14 | Exxon Research Engineering Co | Method for operating a rocket motor or the like |
US2959915A (en) * | 1955-12-27 | 1960-11-15 | Texaco Inc | Fuel for and method of operating a jet engine |
US3000180A (en) * | 1957-04-04 | 1961-09-19 | Napier & Son Ltd | Engines for high speed aircraft or missiles |
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