GB129128A - Improvements in Regulating the Cooling of Internal Combustion Engines on Aircraft, and particularly on Aeroplane Flying Machines. - Google Patents
Improvements in Regulating the Cooling of Internal Combustion Engines on Aircraft, and particularly on Aeroplane Flying Machines.Info
- Publication number
- GB129128A GB129128A GB11437/18A GB1143718A GB129128A GB 129128 A GB129128 A GB 129128A GB 11437/18 A GB11437/18 A GB 11437/18A GB 1143718 A GB1143718 A GB 1143718A GB 129128 A GB129128 A GB 129128A
- Authority
- GB
- United Kingdom
- Prior art keywords
- doors
- hinged
- aircraft
- regulating
- cooling
- 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
- 238000001816 cooling Methods 0.000 title abstract 2
- 230000001105 regulatory effect Effects 0.000 title abstract 2
- 238000002485 combustion reaction Methods 0.000 title 1
- 230000000694 effects Effects 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 POWERÂ PLANTSÂ 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)
- Combines (AREA)
Abstract
129,128. Blackburn Aeroplane & Motor Co., and Booth, H. July 12, 1918. Propelling.-Hinged doors are provided at the sides of the fuselage or other chamber containing the engine whereby the flow of air through the radiator or through the engine chamber, and the consequent cooling effect, may-be regulated. The doors are preferably of triangular shape to leave an unobstructed view to the pilot, and are hinged about the forward edge so as to close under air pressure. The doors may be formed with a tubular frame 6, 9, 10, hinged along the forward edge 6 in bearings 7, 8, the rear edge 9 being approximately vertical and the bottom edge 10 horizontal when the door is closed. The doors may be held in the closed position by rubber or other springs 13, 14, and may be opened by cords 15, 16 connected to a single cord 20, or by a system of levers, under the control of the pilot.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB11437/18A GB129128A (en) | 1918-07-12 | 1918-07-12 | Improvements in Regulating the Cooling of Internal Combustion Engines on Aircraft, and particularly on Aeroplane Flying Machines. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB11437/18A GB129128A (en) | 1918-07-12 | 1918-07-12 | Improvements in Regulating the Cooling of Internal Combustion Engines on Aircraft, and particularly on Aeroplane Flying Machines. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB129128A true GB129128A (en) | 1919-07-10 |
Family
ID=32345010
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB11437/18A Expired GB129128A (en) | 1918-07-12 | 1918-07-12 | Improvements in Regulating the Cooling of Internal Combustion Engines on Aircraft, and particularly on Aeroplane Flying Machines. |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB129128A (en) |
-
1918
- 1918-07-12 GB GB11437/18A patent/GB129128A/en not_active Expired
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