GB547406A - Improvements in or relating to internal combustion engine installations - Google Patents
Improvements in or relating to internal combustion engine installationsInfo
- Publication number
- GB547406A GB547406A GB70541A GB70541A GB547406A GB 547406 A GB547406 A GB 547406A GB 70541 A GB70541 A GB 70541A GB 70541 A GB70541 A GB 70541A GB 547406 A GB547406 A GB 547406A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- ducts
- cooling
- engine
- exhaust
- 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
- F01P1/00—Air cooling
- F01P1/02—Arrangements for cooling cylinders or cylinder heads, e.g. ducting cooling-air from its pressure source to cylinders or along cylinders
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
547,406. Cooling cylinders and exhaust. BRISTOL AEROPLANE CO., Ltd., FEDDEN, A. H. R., and THOMAS, F. M. Jan. 17, 1941, No. 705. [Class 7 (ii)] In an air-cooled engine installation, the cold air for cooling the engine, the air which has become heated in cooling the engine and the exhaust gases are so disposed in ducts 15, 25, 24, that the cold air and the exhaust gases are separated by the heated air. As shown, the installation comprises radial-cylinder engines 10 which are arranged coaxially face-to-face in a casing 17 in the fuselage of an aircraft and drive airscrews through laterally extending shafts 13. Air is admitted through the ducts 15 in the wings to a space 12 between the engines, and is deflected by tubular partitions 19 over the cylinder heads and barrels as described in Specification 547,404. The heated air then passes around exhaust rings 22 and the tailpipes 24 to outlets 28 at the rear of the wings. Oil coolers 26 may be arranged in ducts 27 branched. from the air ducts 15 and leading to the outlet duct 25. Specifications 546,630, [Group XXXIII], 547,403 and 547,405 also are referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB70541A GB547406A (en) | 1941-01-17 | 1941-01-17 | Improvements in or relating to internal combustion engine installations |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB70541A GB547406A (en) | 1941-01-17 | 1941-01-17 | Improvements in or relating to internal combustion engine installations |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB547406A true GB547406A (en) | 1942-08-26 |
Family
ID=9709101
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB70541A Expired GB547406A (en) | 1941-01-17 | 1941-01-17 | Improvements in or relating to internal combustion engine installations |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB547406A (en) |
-
1941
- 1941-01-17 GB GB70541A patent/GB547406A/en not_active Expired
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