GB506146A - Improvements in radiators for aeroplanes and the like - Google Patents
Improvements in radiators for aeroplanes and the likeInfo
- Publication number
- GB506146A GB506146A GB31553/38A GB3155338A GB506146A GB 506146 A GB506146 A GB 506146A GB 31553/38 A GB31553/38 A GB 31553/38A GB 3155338 A GB3155338 A GB 3155338A GB 506146 A GB506146 A GB 506146A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aerofoil
- air
- radiators
- climbing
- aircraft
- 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
- 230000009194 climbing Effects 0.000 abstract 2
- 238000001816 cooling Methods 0.000 abstract 2
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangement 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)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
506,146. Radiators for aircraft engines. BELAIEFF, J. F., DELANEY, C. T., and GALLAY, Ltd. Nov. 1, 1938, No. 31553. [Class 64(iii)] [Also in Group XXXIII] A radiator for aircraft engines comprises cooling units d arranged in V-form within an aerofoil having air inlet and outlet openings b, c respectively. The inlet is so placed that the flow of air through the aerofoil is a maximum when the aircraft is climbing, The air issuing from the outlet may be used to assist propulsion, and a variable flap may be provided at the rear of the aerofoil to assist climbing. In a modification, the cooling units are of curved form. In another arrangement, units are disposed as shown in Fig. 2. Further, a single unit or limb of the V-form may be used.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB31553/38A GB506146A (en) | 1938-11-01 | 1938-11-01 | Improvements in radiators for aeroplanes and the like |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB31553/38A GB506146A (en) | 1938-11-01 | 1938-11-01 | Improvements in radiators for aeroplanes and the like |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB506146A true GB506146A (en) | 1939-05-23 |
Family
ID=10324836
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB31553/38A Expired GB506146A (en) | 1938-11-01 | 1938-11-01 | Improvements in radiators for aeroplanes and the like |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB506146A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2131941A (en) * | 1982-10-13 | 1984-06-27 | Honda Motor Co Ltd | Motorcycle radiator |
-
1938
- 1938-11-01 GB GB31553/38A patent/GB506146A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2131941A (en) * | 1982-10-13 | 1984-06-27 | Honda Motor Co Ltd | Motorcycle radiator |
| US4660624A (en) * | 1982-10-13 | 1987-04-28 | Honda Giken Kogyo Kabushiki Kaisha | Motorcycle radiator |
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