GB525937A - Improvements relating to liquid-cooling apparatus for use in conjunction with an aircraft engine - Google Patents
Improvements relating to liquid-cooling apparatus for use in conjunction with an aircraft engineInfo
- Publication number
- GB525937A GB525937A GB703139A GB703139A GB525937A GB 525937 A GB525937 A GB 525937A GB 703139 A GB703139 A GB 703139A GB 703139 A GB703139 A GB 703139A GB 525937 A GB525937 A GB 525937A
- Authority
- GB
- United Kingdom
- Prior art keywords
- liquid
- cooling apparatus
- aircraft engine
- cowl
- conjunction
- 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
- F16N—LUBRICATING
- F16N39/00—Arrangements for conditioning of lubricants in the lubricating system
- F16N39/02—Arrangements for conditioning of lubricants in the lubricating system by cooling
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
- Lubrication Of Internal Combustion Engines (AREA)
Abstract
525,937. Oil coolers. BRISTOL AEROPLANE CO., Ltd., and COPLEY, J. W. March 3, 1939, No. 7031. [Class 4] [Also in Group XIII] Cooling apparatus for oil or other liquid used in an aircraft engine comprises a cooler 10, through which the liquid is circulated, an air intake 11 facing the direction of flight, and a cowl 21 around the cooler and intake forming an air passage discharging through an orifice 23 between the front of the cowl and the outturned lip 14 of the air intake. The cowl is supported independently of the cooler and intake.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB703139A GB525937A (en) | 1939-03-03 | 1939-03-03 | Improvements relating to liquid-cooling apparatus for use in conjunction with an aircraft engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB703139A GB525937A (en) | 1939-03-03 | 1939-03-03 | Improvements relating to liquid-cooling apparatus for use in conjunction with an aircraft engine |
Publications (1)
Publication Number | Publication Date |
---|---|
GB525937A true GB525937A (en) | 1940-09-06 |
Family
ID=9825311
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB703139A Expired GB525937A (en) | 1939-03-03 | 1939-03-03 | Improvements relating to liquid-cooling apparatus for use in conjunction with an aircraft engine |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB525937A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1062469B (en) * | 1957-01-25 | 1959-07-30 | Hans Molly Dipl Ing | Liftable angled reversible plow |
-
1939
- 1939-03-03 GB GB703139A patent/GB525937A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1062469B (en) * | 1957-01-25 | 1959-07-30 | Hans Molly Dipl Ing | Liftable angled reversible plow |
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