GB447283A - Improvements in cowling for liquid cooled internal combustion engines of aircraft - Google Patents
Improvements in cowling for liquid cooled internal combustion engines of aircraftInfo
- Publication number
- GB447283A GB447283A GB3289834A GB3289834A GB447283A GB 447283 A GB447283 A GB 447283A GB 3289834 A GB3289834 A GB 3289834A GB 3289834 A GB3289834 A GB 3289834A GB 447283 A GB447283 A GB 447283A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cowling
- radiator
- exhaust
- air
- pipes
- 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)
- Exhaust Silencers (AREA)
Abstract
447,283. Propelling aircraft. ELLOR, J. E., Grandell, South Drive, Chain Lane, Mickleover, Derby. Nov. 15, 1934, No. 32898. [Class 4] [See also Group XXVII] The radiator b of a liquid-cooled aircraft engine is housed in a tunnel-like cowling b<1>, through which the slip stream flows by a contracted entrance and exit b<3>, b<6> and into which the exhaust is discharged by nozzles f; the exhaust system thus has less drag on the aircra,ft, and the air flow past the radiator is increased. The radiator is of horseshoe shape in cross-section, and inclined and Venturishaped slats b<4>, f<1> are provided to steady the air flow and to act as silencers and flame dampers. The exhaust may be led by D- sectioned pipes d<1> arranged within the contour of the cowling, but separated therefrom by a cooling-air space. Alternatively the pipes may be circular and located inside the cowling ; they are surrounded by jackets through which air is led by diverging intakes in the air stream and from which it is discharged behind the radiator. An oil cooler g is arranged in the cowling underneath the radiator. The two exhaust pipes of a V-engine extend down the two sides of the cowling and are united to the pipe having the nozzles f.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3289834A GB447283A (en) | 1934-11-15 | 1934-11-15 | Improvements in cowling for liquid cooled internal combustion engines of aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3289834A GB447283A (en) | 1934-11-15 | 1934-11-15 | Improvements in cowling for liquid cooled internal combustion engines of aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB447283A true GB447283A (en) | 1936-05-15 |
Family
ID=10345681
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3289834A Expired GB447283A (en) | 1934-11-15 | 1934-11-15 | Improvements in cowling for liquid cooled internal combustion engines of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB447283A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE767314C (en) * | 1940-11-16 | 1952-05-23 | Daimler Benz Ag | Airplane with exhaust gases blowing out over the wings |
US2623355A (en) * | 1946-04-30 | 1952-12-30 | Boulet Georges | Hot pressurized gas producing means |
DE961317C (en) * | 1951-07-04 | 1957-04-04 | Kloeckner Humboldt Deutz Ag | Conveyor device for gaseous media |
US12203392B2 (en) | 2023-03-06 | 2025-01-21 | Rtx Corporation | Heat exchanger(s) for recovering water and/or heat energy from turbine engine combustion products |
-
1934
- 1934-11-15 GB GB3289834A patent/GB447283A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE767314C (en) * | 1940-11-16 | 1952-05-23 | Daimler Benz Ag | Airplane with exhaust gases blowing out over the wings |
US2623355A (en) * | 1946-04-30 | 1952-12-30 | Boulet Georges | Hot pressurized gas producing means |
DE961317C (en) * | 1951-07-04 | 1957-04-04 | Kloeckner Humboldt Deutz Ag | Conveyor device for gaseous media |
US12203392B2 (en) | 2023-03-06 | 2025-01-21 | Rtx Corporation | Heat exchanger(s) for recovering water and/or heat energy from turbine engine combustion products |
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