GB514209A - Improvements in or relating to cooling devices in aircraft - Google Patents
Improvements in or relating to cooling devices in aircraftInfo
- Publication number
- GB514209A GB514209A GB10287/38A GB1028738A GB514209A GB 514209 A GB514209 A GB 514209A GB 10287/38 A GB10287/38 A GB 10287/38A GB 1028738 A GB1028738 A GB 1028738A GB 514209 A GB514209 A GB 514209A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flap
- aircraft
- air
- cooling
- wing
- 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 3
- 230000007246 mechanism 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 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
514,209. Controlling aircraft. WESTLAND AIRCRAFT, Ltd., RICHARDS, S. T. A., and DIGBY, F. J. W. W. April 4, 1938, No. 10287: [Class 4] - An aircraft having engines cooled by air passing through the wings has a flap for controlling the flow of the cooling air' operatively connected to .a lift-increasing device such as a flap or slot so that the position of the cooling-air flap is determined by the .position of the lift-increasing device. In one form, Fig. 2, the cooling air for the radiator passes through a channel formed in the wing, the channel having-its lower surface formed by the flap a and its upper surface by the cooling-air flap c. The flap c is hinged to the wing at d and carries trackways so that as the flap a moves outwards the roller g causes the flap c to take up successively the positions shown. in dotted lines 33-37. The trackway carries a roller i which, when the flap a is closed, engages a bracket j, and thus relatively locks the flaps -in their closed positions. Other mechanisms shown for carrying ,the invention into effect include links and pivoted levers, toothed gearing, and flexible cables, and in some cases the flap is interconnected to a slot at the leading. edge of the wing. Controls such as are disclosed in Specification 375,115, [Group XXV], or 419,310 may be used. ,
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB10287/38A GB514209A (en) | 1938-04-04 | 1938-04-04 | Improvements in or relating to cooling devices in aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB10287/38A GB514209A (en) | 1938-04-04 | 1938-04-04 | Improvements in or relating to cooling devices in aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB514209A true GB514209A (en) | 1939-11-02 |
Family
ID=9965080
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB10287/38A Expired GB514209A (en) | 1938-04-04 | 1938-04-04 | Improvements in or relating to cooling devices in aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB514209A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114810416A (en) * | 2022-06-27 | 2022-07-29 | 中国航发四川燃气涡轮研究院 | Zigzag variable cycle engine adjustable front duct ejector structure |
-
1938
- 1938-04-04 GB GB10287/38A patent/GB514209A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114810416A (en) * | 2022-06-27 | 2022-07-29 | 中国航发四川燃气涡轮研究院 | Zigzag variable cycle engine adjustable front duct ejector structure |
| CN114810416B (en) * | 2022-06-27 | 2022-09-23 | 中国航发四川燃气涡轮研究院 | Zigzag variable cycle engine adjustable front duct ejector structure |
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