GB530094A - Improvements in and relating to engine and radiator installations, particularly for aircraft - Google Patents
Improvements in and relating to engine and radiator installations, particularly for aircraftInfo
- Publication number
- GB530094A GB530094A GB17650/39A GB1765039A GB530094A GB 530094 A GB530094 A GB 530094A GB 17650/39 A GB17650/39 A GB 17650/39A GB 1765039 A GB1765039 A GB 1765039A GB 530094 A GB530094 A GB 530094A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- radiators
- radiator
- duct
- disposed
- 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
- 238000009434 installation Methods 0.000 title abstract 2
- 238000001816 cooling Methods 0.000 abstract 1
- JHIVVAPYMSGYDF-UHFFFAOYSA-N cyclohexanone Chemical compound O=C1CCCCC1 JHIVVAPYMSGYDF-UHFFFAOYSA-N 0.000 abstract 1
- 230000001105 regulatory effect Effects 0.000 abstract 1
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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
- B64D33/10—Radiator arrangement
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
530,094. Aircraft engines and radiators. BREVETS AERO-MECANIQUES SOC. ANON. June 16, 1939, No. 17650. Convention date, April 28. [Class 4] In an engine and radiator installation enclosed by a cowling, the radiator length lies in the direction (f the driving shaft and its lower and upper surfaces form the inlet and outlet for the cooling air, the air conduit progressively increasing towards the radiator. As shown, radiators b are disposed on both sides of an aeroengine 2 which is housed in a streamlined cowling 3. The radiators are disposed approximately parallel tc the crank-shaft of the engine, the cylinder of which are arranged in V-formation. The radiators are housed in divergentconvergent duct 4, 5 arranged as shown and either or both the inlet or outlet sections of the ducts may be provided with regulating means. A duct may be arranged above or below the engine and the exit from the duct may be disposed in a region of reduced pressure.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| BE530094X | 1939-04-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB530094A true GB530094A (en) | 1940-12-04 |
Family
ID=3871670
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB17650/39A Expired GB530094A (en) | 1939-04-28 | 1939-06-16 | Improvements in and relating to engine and radiator installations, particularly for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB530094A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2012065713A3 (en) * | 2010-11-16 | 2012-08-16 | Airbus Operations Gmbh | Aircraft outer skin heat exchanger, aircraft cooling system and method for operating an aircraft outer skin heat exchanger |
-
1939
- 1939-06-16 GB GB17650/39A patent/GB530094A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2012065713A3 (en) * | 2010-11-16 | 2012-08-16 | Airbus Operations Gmbh | Aircraft outer skin heat exchanger, aircraft cooling system and method for operating an aircraft outer skin heat exchanger |
| CN103282278A (en) * | 2010-11-16 | 2013-09-04 | 空中客车作业有限公司 | Aircraft outer skin heat exchanger, aircraft cooling system and method for operating an aircraft outer skin heat exchanger |
| CN103282278B (en) * | 2010-11-16 | 2016-11-16 | 空中客车作业有限公司 | Aircraft outer skin heat exchanger, aircraft cooling system and the method being used for operating aircraft outer skin heat exchanger |
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