GB473340A - Improvements in cooling means for internal combustion engines - Google Patents
Improvements in cooling means for internal combustion enginesInfo
- Publication number
- GB473340A GB473340A GB1037436A GB1037436A GB473340A GB 473340 A GB473340 A GB 473340A GB 1037436 A GB1037436 A GB 1037436A GB 1037436 A GB1037436 A GB 1037436A GB 473340 A GB473340 A GB 473340A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cooling
- engine
- wings
- nose
- discharged
- 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
- F01P7/00—Controlling of coolant flow
- F01P7/02—Controlling of coolant flow the coolant being cooling-air
- F01P7/023—Cowlings for airplane engines
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
473,340. Cooling cylinders. ELLOR, J. E., and PARAVICINI, T. P. DE. April 8, 1936, No. 10374. [Class 7 (ii)] [Also in Group XXXIII] In an aircraft in which the engine is mounted in front of, and in a cowling continuous with, the wings, the cooling air enters through slots C<1> in the wings and passes forwardly over the engine cooling surfaces to be discharged through an annular opening D, the size of which can be adjusted by sliding axially a nose D<1>, preferably mounted on a tubular member D<3> projecting into the airscrew spinner. The nose may be adjusted manually or by a thermal device. The air flow may be assisted by fans C<2> driven by the engine or by electric motors, and slats C<3> may aid the flow round the bends. The cross-sectional area of the ducts increases progressively ; exhaust is discharged by an annular ring E, air flow being thereby increased and drag on the aircraft reduced. The surfaces cooled may be finned cylinders or a liquid-cooling radiator.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1037436A GB473340A (en) | 1936-04-08 | 1936-04-08 | Improvements in cooling means for internal combustion engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1037436A GB473340A (en) | 1936-04-08 | 1936-04-08 | Improvements in cooling means for internal combustion engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB473340A true GB473340A (en) | 1937-10-08 |
Family
ID=9966664
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1037436A Expired GB473340A (en) | 1936-04-08 | 1936-04-08 | Improvements in cooling means for internal combustion engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB473340A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1000186B (en) * | 1954-04-21 | 1957-01-03 | Motoren Werke Mannheim Ag | Air-cooled internal combustion engine with cylinders arranged in a V shape |
US3951114A (en) * | 1974-03-22 | 1976-04-20 | Hans List | Cooling of internal combustion engines with sound-proof encasings |
-
1936
- 1936-04-08 GB GB1037436A patent/GB473340A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1000186B (en) * | 1954-04-21 | 1957-01-03 | Motoren Werke Mannheim Ag | Air-cooled internal combustion engine with cylinders arranged in a V shape |
US3951114A (en) * | 1974-03-22 | 1976-04-20 | Hans List | Cooling of internal combustion engines with sound-proof encasings |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US1779186A (en) | Aircraft power plant | |
GB473340A (en) | Improvements in cooling means for internal combustion engines | |
US2221905A (en) | Engine cowling and cooling | |
US2401584A (en) | Air flow inducing device | |
GB471371A (en) | Cooling of aircraft engines | |
GB447283A (en) | Improvements in cowling for liquid cooled internal combustion engines of aircraft | |
GB464348A (en) | Improvements in inter-coolers for superchargers of internal combustion engines | |
US2047948A (en) | Cowling for aircraft motors | |
GB493673A (en) | Improvements in and relating to radiators for the engines of aircraft or other vehicles | |
GB463303A (en) | Oil coolers for aircraft | |
US2172139A (en) | Engine cooling means | |
US1975776A (en) | Air cooled internal combustion engine | |
GB407216A (en) | Improvements in or relating to the air-cooling of internal combustion engines | |
GB472820A (en) | Improvements in the cooling of engines particularly for aircraft | |
GB504992A (en) | Oil cooler for aircraft engines | |
GB531299A (en) | De-icing apparatus for the airscrews of air-cooled aircraft engines | |
GB456819A (en) | Improvements in and relating to air cooled aero engines with a view to securing an improved cooling effect | |
GB489076A (en) | Improvements in or relating to the air-cooling of the cylinders of internal combustion engines on aircraft | |
GB284063A (en) | Improvements relating to the air-cooling of crankless internal combustion engines | |
GB463474A (en) | Cooling of aircraft engines | |
GB472555A (en) | Improvements in aircraft | |
GB446702A (en) | Improvements in or relating to aircraft having air-cooled internal-combustion engines | |
GB544598A (en) | Improvements relating to the cooling of aircraft engines | |
GB480345A (en) | Improvements in cowlings for aircraft engines | |
GB547406A (en) | Improvements in or relating to internal combustion engine installations |