GB516616A - Improvements in or relating to aircraft wings - Google Patents
Improvements in or relating to aircraft wingsInfo
- Publication number
- GB516616A GB516616A GB12139/38A GB1213938A GB516616A GB 516616 A GB516616 A GB 516616A GB 12139/38 A GB12139/38 A GB 12139/38A GB 1213938 A GB1213938 A GB 1213938A GB 516616 A GB516616 A GB 516616A
- Authority
- GB
- United Kingdom
- Prior art keywords
- slat
- duct
- flap
- aircraft
- entrance
- 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 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—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)
- Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)
Abstract
516,616. Aircraft. WESTLAND AIRCRAFT, Ltd., WIDGERY, W. M., and PAINE, W. H. April 22, 1938, No. 12139 [Class 4] In an aircraft wing having a duct with a forward opening, for cooling air or other purposes, a slat is provided immediately above the entrance to the duct, the duct entrance being substantially unrestricted by ' the opening and closing of the slat. The slat may be formed partly from the upper lip of the duct. In the form shown in Fig. 4, the slat a is supported by two curved arms d carried on rollers e. The slat is pivotally mounted at h and an adjustable locking device is provided. In Fig. 1, the slat a is shown interconnected through the linkage k, m, n with a rearwardly displaceable flap p, for simultaneous operation. The slat a may also be operated in combination with other forms of flap or with wing-tip flaps. In one form a rearwardly moving flap actuates a hydraulic valve to cause first the opening and then the closing of the slat as the flap moves rearwardly. The slat may extend to each side of and be in part formed of the upper lip of a circular or oval duct entrance.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB12139/38A GB516616A (en) | 1938-04-22 | 1938-04-22 | Improvements in or relating to aircraft wings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB12139/38A GB516616A (en) | 1938-04-22 | 1938-04-22 | Improvements in or relating to aircraft wings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB516616A true GB516616A (en) | 1940-01-08 |
Family
ID=9999050
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB12139/38A Expired GB516616A (en) | 1938-04-22 | 1938-04-22 | Improvements in or relating to aircraft wings |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB516616A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE10335482A1 (en) * | 2003-08-02 | 2005-05-12 | Airbus Gmbh | Raptor air intake of an aircraft |
-
1938
- 1938-04-22 GB GB12139/38A patent/GB516616A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE10335482A1 (en) * | 2003-08-02 | 2005-05-12 | Airbus Gmbh | Raptor air intake of an aircraft |
| DE10335482B4 (en) * | 2003-08-02 | 2008-04-03 | Airbus Deutschland Gmbh | Raptor air intake of an aircraft |
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