GB627017A - Improvements in or relating to air-cooled internal-combustion engines - Google Patents
Improvements in or relating to air-cooled internal-combustion enginesInfo
- Publication number
- GB627017A GB627017A GB1106546A GB1106546A GB627017A GB 627017 A GB627017 A GB 627017A GB 1106546 A GB1106546 A GB 1106546A GB 1106546 A GB1106546 A GB 1106546A GB 627017 A GB627017 A GB 627017A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cylinder
- air
- fins
- baffles
- bolts
- 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
627,017. Cooling cylinders. BRISTOL AEROPLANE CO., Ltd., MANSELL, H. C., and GORRELL, H. N. April 10, 1946, No. 11065. [Class 7 (ii)] In a sleeve-valve engine cylinder cooling air is divided by baffles to flow in two paths as shown by arrows, one path being across the cylinder head and the other down the cylinder barrel. The air enters by a duct 19 and part is deflected by a cowl 21 and a trough 29 to flow past fins 28 on the junk head. The remainder flows round the annular space formed by cutting away the tops of longitudinal cylinder fins and bounded by a casing 20 formed in two parts connected by a band 36. The upper part is attached to the cylinder by bolts 53, and the two parts are drawn together by bolts 32 and wing nuts 35. Openings 47, 48 are arranged for the exhaust and inlet pipes, that for the exhaust pipe being large enough to allow cooling air to escape and thus cool the pipe. Baffles 49 prevent air from flowing through gaps left between groups of cylinder fins. Specifications 610,584 and 627,018 are referred to in the Provisional Specification.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1106546A GB627017A (en) | 1946-04-10 | 1946-04-10 | Improvements in or relating to air-cooled internal-combustion engines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1106546A GB627017A (en) | 1946-04-10 | 1946-04-10 | Improvements in or relating to air-cooled internal-combustion engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB627017A true GB627017A (en) | 1949-07-26 |
Family
ID=9979350
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1106546A Expired GB627017A (en) | 1946-04-10 | 1946-04-10 | Improvements in or relating to air-cooled internal-combustion engines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB627017A (en) |
-
1946
- 1946-04-10 GB GB1106546A patent/GB627017A/en not_active Expired
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