GB466286A - Improved means for controlling oil cooling on the internal combustion engines of aircraft, land and marine vehicles - Google Patents
Improved means for controlling oil cooling on the internal combustion engines of aircraft, land and marine vehiclesInfo
- Publication number
- GB466286A GB466286A GB3449235A GB3449235A GB466286A GB 466286 A GB466286 A GB 466286A GB 3449235 A GB3449235 A GB 3449235A GB 3449235 A GB3449235 A GB 3449235A GB 466286 A GB466286 A GB 466286A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cold air
- aircraft
- cooler
- piston
- land
- 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
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M5/00—Heating, cooling, or controlling temperature of lubricant; Lubrication means facilitating engine starting
- F01M5/002—Cooling
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Lubrication Of Internal Combustion Engines (AREA)
Abstract
466,286. Radiators for aircraft &c. FAIREY AVIATION CO., Ltd., HALL, G. W., and LOBELLE, M. J. O. Dec. 12, 1935, No. 34492. [Class 29] The flow of hot air or cold air or both to an oil cooler b is regulated in accordance with the oil pressure acting on a piston e against a spring g arranged in the oil inlet pipe a of the cooler, the piston being connected to louvres c, Fig. 1, shown as controlling the supply of hot air while leaving uncontrolled the cold air passages h. Where the cold air passages are controlled the louvres act in an opposite sense to those of the hot air passage, and may be actuated from the same or a separate piston. A plate o, Fig. 3, with two apertures s, t may have an arcuate or sliding motion over branch passages u, v, for hot and cold air leading to a single air passage to the cooler. According to the Provisional Specification a shutter plate with rectilinear or arcuate motion may have an aperture the effective area of which increases gradually to a maximum and then decreases more rapidly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3449235A GB466286A (en) | 1935-12-12 | 1935-12-12 | Improved means for controlling oil cooling on the internal combustion engines of aircraft, land and marine vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3449235A GB466286A (en) | 1935-12-12 | 1935-12-12 | Improved means for controlling oil cooling on the internal combustion engines of aircraft, land and marine vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB466286A true GB466286A (en) | 1937-05-26 |
Family
ID=10366315
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3449235A Expired GB466286A (en) | 1935-12-12 | 1935-12-12 | Improved means for controlling oil cooling on the internal combustion engines of aircraft, land and marine vehicles |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB466286A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2492675A (en) * | 1943-06-16 | 1949-12-27 | Missouri Automatic Contr Corp | Control for temperature changing mechanisms |
-
1935
- 1935-12-12 GB GB3449235A patent/GB466286A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2492675A (en) * | 1943-06-16 | 1949-12-27 | Missouri Automatic Contr Corp | Control for temperature changing mechanisms |
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