GB410199A - Improvements in or relating to the cooling systems for internal combustion engines - Google Patents
Improvements in or relating to the cooling systems for internal combustion enginesInfo
- Publication number
- GB410199A GB410199A GB2593632A GB2593632A GB410199A GB 410199 A GB410199 A GB 410199A GB 2593632 A GB2593632 A GB 2593632A GB 2593632 A GB2593632 A GB 2593632A GB 410199 A GB410199 A GB 410199A
- Authority
- GB
- United Kingdom
- Prior art keywords
- radiator
- condenser
- steam
- cooling
- water
- 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
- F01P3/00—Liquid cooling
- F01P3/22—Liquid cooling characterised by evaporation and condensation of coolant in closed cycles; characterised by the coolant reaching higher temperatures than normal atmospheric boiling-point
- F01P3/2271—Closed cycles with separator and liquid return
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
410,199. Cooling cylinders. FAIREY AVIATION CO., Ltd., Cranford Lane, Hayes, Middlesex, and FORSYTH, A; G., Venlaw, Burdon Lane, Cheam, Surrey. Sept. 17, 1932, Nos. 25936/32 and 3122/33. [Class 7 (ii).] A cooling system for aircraft engines is provided with a water-cooling radiator 14 of such size as to effect adequate cooling under normal conditions and a steam-condenser 17 which becomes operative under abnormal conditions, the condenser being located behind the radiator or incorporated in the wing or fuselage structure in known manner so that only the water-cooling radiator offers head resistance. Liquid and steam from the engine jackets 10 pass by a pipe 11 to a steam separator 12 whence the liquid descends to the radiator and steam passes through a dome 15 to the condenser, which is preferably formed of two similar triangular parts 18, 19, Fig. 3. The water from the radiator is returned by a pump 24 to the jackets and the condensate is delivered by a pump 21 back to the separator. In a modification, Fig. 4, a centrifugal steam separator 26, as. described in Specification 315,007, [Class 23], is employed, and the condenser is constituted by headers 31 and conduits 32 in the wing surface. The condensate is fed into the radiator 27, and the radiator may be movable into and out of the air stream as described in Specification 252,082, [Class 29]. The quantity of the water circulating through the radiator may be regulated by a valved byepass pipe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2593632A GB410199A (en) | 1932-09-17 | 1932-09-17 | Improvements in or relating to the cooling systems for internal combustion engines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2593632A GB410199A (en) | 1932-09-17 | 1932-09-17 | Improvements in or relating to the cooling systems for internal combustion engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB410199A true GB410199A (en) | 1934-05-17 |
Family
ID=10235714
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2593632A Expired GB410199A (en) | 1932-09-17 | 1932-09-17 | Improvements in or relating to the cooling systems for internal combustion engines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB410199A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE743420C (en) * | 1939-04-05 | 1943-12-24 | Messerschmitt A G | Evaporative cooling system with a storage coolant container for aircraft engines |
| US2649082A (en) * | 1950-06-03 | 1953-08-18 | Engineering Controls Inc | Engine cooling system utilizing waste heat |
| CN101929372A (en) * | 2010-08-31 | 2010-12-29 | 哈尔滨工业大学 | Engine tail gas water collecting system |
-
1932
- 1932-09-17 GB GB2593632A patent/GB410199A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE743420C (en) * | 1939-04-05 | 1943-12-24 | Messerschmitt A G | Evaporative cooling system with a storage coolant container for aircraft engines |
| US2649082A (en) * | 1950-06-03 | 1953-08-18 | Engineering Controls Inc | Engine cooling system utilizing waste heat |
| CN101929372A (en) * | 2010-08-31 | 2010-12-29 | 哈尔滨工业大学 | Engine tail gas water collecting system |
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