GB504360A - Improvements in aeroplanes - Google Patents
Improvements in aeroplanesInfo
- Publication number
- GB504360A GB504360A GB28651/37A GB2865137A GB504360A GB 504360 A GB504360 A GB 504360A GB 28651/37 A GB28651/37 A GB 28651/37A GB 2865137 A GB2865137 A GB 2865137A GB 504360 A GB504360 A GB 504360A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- air
- over
- duct
- housing
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Ventilation (AREA)
Abstract
504,360. Aircraft wings. SPEARPOINT, H. G., and STANWAY, H. Oct. 21, 1937, No. 28651. [Class 4] Air is collected by one or more intakes disposed in the slipstream of the airscrew or airscrews of an aircraft, the intakes being divided into concentric orifices each of which communicates with one or more sections of a continuous slot extending along the entire length of the wings close to their leading edges. A streamlined housing b is provided with visor shutters b<3> adapted to control the flow of air thereinto. Communicating with the housing are three ducts which extend along the leading edge and terminate at the housing end in concentric openings. The ducts are of differing lengths and taper toward the wing tip. The uppermost duct b<2> communicates with a longitudinal slot a over the root portion of the wing, the duct b<1> over the middle portion of the wing and the lowermost duct over the tip portion. The shape of the nosing defining the slot is stated to be such that the air issuing therefrom increases the lift of the wing. Heated air maybe supplied by air entering a cowl c<1> surrounding an exhaust collector ring c<2>.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB28651/37A GB504360A (en) | 1937-10-21 | 1937-10-21 | Improvements in aeroplanes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB28651/37A GB504360A (en) | 1937-10-21 | 1937-10-21 | Improvements in aeroplanes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB504360A true GB504360A (en) | 1939-04-21 |
Family
ID=10278964
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB28651/37A Expired GB504360A (en) | 1937-10-21 | 1937-10-21 | Improvements in aeroplanes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB504360A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2674420A (en) * | 1949-05-06 | 1954-04-06 | Lockheed Aircraft Corp | Antenna installation |
| US5114100A (en) * | 1989-12-29 | 1992-05-19 | The Boeing Company | Anti-icing system for aircraft |
-
1937
- 1937-10-21 GB GB28651/37A patent/GB504360A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2674420A (en) * | 1949-05-06 | 1954-04-06 | Lockheed Aircraft Corp | Antenna installation |
| US5114100A (en) * | 1989-12-29 | 1992-05-19 | The Boeing Company | Anti-icing system for aircraft |
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