GB510192A - Improvements in or relating to aircraft - Google Patents
Improvements in or relating to aircraftInfo
- Publication number
- GB510192A GB510192A GB420838A GB420838A GB510192A GB 510192 A GB510192 A GB 510192A GB 420838 A GB420838 A GB 420838A GB 420838 A GB420838 A GB 420838A GB 510192 A GB510192 A GB 510192A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- rotors
- retraction
- rotor
- extended
- 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
- B64C23/08—Influencing air flow over aircraft surfaces, not otherwise provided for using Magnus effect
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Gear Transmission (AREA)
Abstract
510,192. Aircraft with additional supporting surfaces. FAIREY AVIATION CO., Ltd., and LOBELLE, M..J. 0. Feb. 10, 1938, No. 4208. [Class 4] In an aircraft provided with rotors which may be mechanically driven or autorotative and which may be extended into the aircraft slip-stream or retracted to lie alongside the fuselage of the aircraft, the rotors are arranged to lie, when extended, immediately in the rear of the trailing edges of the wings of the aircraft. As shown, operation of a jack 21 through links 19 effects extension and retraction of frustoconical rotors 11 mounted on shafts 14. The rotors 11 may be driven, by an electric motor 22, in one or opposite directions according to the position of a member 39 of a dog clutch. The drive is transmitted through either bevel gears 24, 25, 28, 29 and spur gears 33, 34 or spur gears 33, 34. The gear 34 is mounted on a shaft carrying the rotor. A pin 26 forms the hinge about which the rotor is moved for extension or retraction.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB420838A GB510192A (en) | 1938-02-10 | 1938-02-10 | Improvements in or relating to aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB420838A GB510192A (en) | 1938-02-10 | 1938-02-10 | Improvements in or relating to aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB510192A true GB510192A (en) | 1939-07-28 |
Family
ID=9772762
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB420838A Expired GB510192A (en) | 1938-02-10 | 1938-02-10 | Improvements in or relating to aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB510192A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2266498A (en) * | 1992-04-30 | 1993-11-03 | Graeme Keith Walden | Magnus effect lifter unit. |
-
1938
- 1938-02-10 GB GB420838A patent/GB510192A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2266498A (en) * | 1992-04-30 | 1993-11-03 | Graeme Keith Walden | Magnus effect lifter unit. |
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