GB463303A - Oil coolers for aircraft - Google Patents
Oil coolers for aircraftInfo
- Publication number
- GB463303A GB463303A GB2612535A GB2612535A GB463303A GB 463303 A GB463303 A GB 463303A GB 2612535 A GB2612535 A GB 2612535A GB 2612535 A GB2612535 A GB 2612535A GB 463303 A GB463303 A GB 463303A
- Authority
- GB
- United Kingdom
- Prior art keywords
- radiator
- oil cooler
- engine
- air
- aircraft
- 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
463,303. Aircraft engine accessories. PARAVICINI, T. P. DE. Sept. 20, 1935, No. 26125. [Class 4] [Also in Group XIII] An oil cooler C, Fig. 1 is arranged in a tunnel A<2> in which the engine radiator A is located and in such a position that it is exposed to a stream of air which has been warmed by passage over the radiator, whereby overcooling of the oil is avoided. The oil cooler may be placed behind the radiator or between front and rear parts of a divided radiator. The air flow through the tunnel may be controlled by a hinged flap A<5> at the rear. In the case of an air-cooled engine with the cylinders in line the oil cooler may be located in the rear of the cylinder cowling, and in a radial-cylinder engine, Fig. 5, cowled in a ring H<2>, the oil cooler I occupies a position in the gap between the fuselage and the ring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2612535A GB463303A (en) | 1935-09-20 | 1935-09-20 | Oil coolers for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2612535A GB463303A (en) | 1935-09-20 | 1935-09-20 | Oil coolers for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB463303A true GB463303A (en) | 1937-03-22 |
Family
ID=10238772
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2612535A Expired GB463303A (en) | 1935-09-20 | 1935-09-20 | Oil coolers for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB463303A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2312738A (en) * | 1996-05-02 | 1997-11-05 | Rover Group | Heat exchanger assembly |
-
1935
- 1935-09-20 GB GB2612535A patent/GB463303A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2312738A (en) * | 1996-05-02 | 1997-11-05 | Rover Group | Heat exchanger assembly |
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