GB463474A - Cooling of aircraft engines - Google Patents
Cooling of aircraft enginesInfo
- Publication number
- GB463474A GB463474A GB2426135A GB2426135A GB463474A GB 463474 A GB463474 A GB 463474A GB 2426135 A GB2426135 A GB 2426135A GB 2426135 A GB2426135 A GB 2426135A GB 463474 A GB463474 A GB 463474A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- air
- cowling
- aircraft
- trailing edge
- 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)
- Braking Arrangements (AREA)
- General Details Of Gearings (AREA)
Abstract
463,474. Cooling cylinders. ARMSTRONG WHITWORTH AIRCRAFT, Ltd., Sm W. G., and LLOYD, J. Aug. 30, 1935, No. 24261. [Class 7 (ii)] [Also in Group XXXIII] In an aircraft having a cowled air-cooled engine, arranged behind the airscrew with its crankshaft longitudinally of the aircraft and a passage in the interior of a wing which merges into the cowling, the whole of the cooling air which has passed through the cowling is transmitted to an outlet adjacent the trailing edge of the wing. An engine 11 is mounted on a wing 12 and is surrounded by an annular cowling 13 which is faired into the wing and its rear end is connected to an outlet opening 14 provided in the trailing edge of the wing and controlled by a pivoted flap 15 which may constitute an air-brake. In a modification, the rear end of the cowling is directly connected to the leading edges of the wings, the air being discharged between the trailing edge of the wing and the ailerons 18. In a still further modification, a fifteen-cylinder engine of star form with the cylinders arranged in lines of three is housed in the wing 12, the air-inlet being through horizontal slots. Inter. nal baffles are provided.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2426135A GB463474A (en) | 1935-08-30 | 1935-08-30 | Cooling of aircraft engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2426135A GB463474A (en) | 1935-08-30 | 1935-08-30 | Cooling of aircraft engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB463474A true GB463474A (en) | 1937-03-30 |
Family
ID=10208943
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2426135A Expired GB463474A (en) | 1935-08-30 | 1935-08-30 | Cooling of aircraft engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB463474A (en) |
-
1935
- 1935-08-30 GB GB2426135A patent/GB463474A/en not_active Expired
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