GB570615A - Improvements in or relating to aircraft radiators - Google Patents
Improvements in or relating to aircraft radiatorsInfo
- Publication number
- GB570615A GB570615A GB1395640A GB1395640A GB570615A GB 570615 A GB570615 A GB 570615A GB 1395640 A GB1395640 A GB 1395640A GB 1395640 A GB1395640 A GB 1395640A GB 570615 A GB570615 A GB 570615A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ways
- water
- air
- radiator
- pitch
- 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
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
570,615. Plate heat-exchangers. DUNN, A. W. and IMPERIAL CHEMICAL INDUSTRIES, Ltd. Sept. 6, 1940, No. 13956. [Class 64 (iii)] In a radiator with corrugated sheets 5 forming air-ways between and at right angles to flat-sided water-ways 4, the width of the water-ways is 1/16 in. and their pitch in., and the pitch of the air-ways is 1/10 in. The depth of the radiator is 9 in. Corrugated plates 14 in the water-ways may be continuous instead of being formed in spaced sections, and each air-way may contain two currugated sheets, one on each side of a plane sheet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1395640A GB570615A (en) | 1940-09-06 | 1940-09-06 | Improvements in or relating to aircraft radiators |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1395640A GB570615A (en) | 1940-09-06 | 1940-09-06 | Improvements in or relating to aircraft radiators |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB570615A true GB570615A (en) | 1945-07-16 |
Family
ID=10032417
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1395640A Expired GB570615A (en) | 1940-09-06 | 1940-09-06 | Improvements in or relating to aircraft radiators |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB570615A (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 |
-
1940
- 1940-09-06 GB GB1395640A patent/GB570615A/en not_active Expired
Cited By (4)
| 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 |
| US10011362B2 (en) | 2010-11-16 | 2018-07-03 | Airbus Operations Gmbh | Aircraft outer skin heat exchanger, aircraft cooling system and method for operating an aircraft outer skin heat exchanger |
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