GB474327A - Improvements in and relating to liquid cooling systems of internal combustion engines on aircraft - Google Patents
Improvements in and relating to liquid cooling systems of internal combustion engines on aircraftInfo
- Publication number
- GB474327A GB474327A GB35148/36A GB3514836A GB474327A GB 474327 A GB474327 A GB 474327A GB 35148/36 A GB35148/36 A GB 35148/36A GB 3514836 A GB3514836 A GB 3514836A GB 474327 A GB474327 A GB 474327A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- engine
- relating
- internal combustion
- combustion engines
- 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
- F01P11/02—Liquid-coolant filling, overflow, venting, or draining devices
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
474,327. Cooling cylinders. SAULNIER, R. Dec. 22, 1936, No. 35148. Convention date, Dec. 27, 1935. [Class 7 (ii)] [Also in Group XIII] A liquid-circulating system of an aircraft engine is kept full of liquid at all inclinations of the aircraft by the provision of a supply tank 10 at the rear in addition to the normal supply tank 9 at the front of .the engine, the tops of the tanks being connected together by a pipe 13. The tank 9 is connected to the system by two pipes 11, 14 and has a vent pipe 15 for the escape of steam, a spring-pressed release valve 17 being located behind the engine where it is free from the dynamic effect of evolutions of the aircraft. An inwardlyopening safety valve is provided in the filler cap 18.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR474327X | 1935-12-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB474327A true GB474327A (en) | 1937-10-29 |
Family
ID=8902853
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB35148/36A Expired GB474327A (en) | 1935-12-27 | 1936-12-22 | Improvements in and relating to liquid cooling systems of internal combustion engines on aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB474327A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE740661C (en) * | 1939-01-31 | 1943-10-26 | Aeroplanes Morane Saulnier | Liquid cooling device for internal combustion engines in vehicles |
DE3424470A1 (en) * | 1983-07-11 | 1985-01-24 | Nissan Motor Co., Ltd., Yokohama, Kanagawa | CYLINDER HEAD OF AN INTERNAL COMBUSTION ENGINE |
-
1936
- 1936-12-22 GB GB35148/36A patent/GB474327A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE740661C (en) * | 1939-01-31 | 1943-10-26 | Aeroplanes Morane Saulnier | Liquid cooling device for internal combustion engines in vehicles |
DE3424470A1 (en) * | 1983-07-11 | 1985-01-24 | Nissan Motor Co., Ltd., Yokohama, Kanagawa | CYLINDER HEAD OF AN INTERNAL COMBUSTION ENGINE |
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