GB533767A - Improvements relating to oil coolers - Google Patents
Improvements relating to oil coolersInfo
- Publication number
- GB533767A GB533767A GB3075239A GB3075239A GB533767A GB 533767 A GB533767 A GB 533767A GB 3075239 A GB3075239 A GB 3075239A GB 3075239 A GB3075239 A GB 3075239A GB 533767 A GB533767 A GB 533767A
- Authority
- GB
- United Kingdom
- Prior art keywords
- oil
- over
- outlet
- coolers
- tubes
- 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)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
533,767. Oil coolers. SERCK RADIATORS, Ltd., and GARNER, E. Nov. 24, 1939, No. 30752. [Class 64 (iii)] In an oil cooler intended particularly for use on aircraft and of the kind in which the oil flows over tubes through which air or other coolant passes, the oil flows first over a central group of tubes b and then passes around partitions e and over side tube groups c. When the oil is cold, it passes under the control of a spring-pressed or thermostatically operated relief valve r in the outlet k directly from the central tube group to the outlet through an annular passage n. The oil may be directed in a longitudinal or transverse sinuous course over the side groups by baffles f, and it may flow through the side groups in series or in parallel. Pairs of coolers may be connected in series, and a further relief valve may be provided to connect the inlet of the first cooler and the outlet of the second.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3075239A GB533767A (en) | 1939-11-24 | 1939-11-24 | Improvements relating to oil coolers |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3075239A GB533767A (en) | 1939-11-24 | 1939-11-24 | Improvements relating to oil coolers |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB533767A true GB533767A (en) | 1941-02-19 |
Family
ID=10312579
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3075239A Expired GB533767A (en) | 1939-11-24 | 1939-11-24 | Improvements relating to oil coolers |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB533767A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2903244A (en) * | 1955-04-07 | 1959-09-08 | Rolls Royce | Oil coolers for engines |
| EP2218883A1 (en) * | 2009-02-13 | 2010-08-18 | Sullair Corporation | Two-stage heat exchanger with interstage bypass |
-
1939
- 1939-11-24 GB GB3075239A patent/GB533767A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2903244A (en) * | 1955-04-07 | 1959-09-08 | Rolls Royce | Oil coolers for engines |
| EP2218883A1 (en) * | 2009-02-13 | 2010-08-18 | Sullair Corporation | Two-stage heat exchanger with interstage bypass |
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