GB418121A - Improvements in or relating to aircraft - Google Patents
Improvements in or relating to aircraftInfo
- Publication number
- GB418121A GB418121A GB15676/34A GB1567634A GB418121A GB 418121 A GB418121 A GB 418121A GB 15676/34 A GB15676/34 A GB 15676/34A GB 1567634 A GB1567634 A GB 1567634A GB 418121 A GB418121 A GB 418121A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- wing
- fixed wing
- relating
- rotatable
- 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)
- Automatic Cycles, And Cycles In General (AREA)
Abstract
418,121. Aircraft with rotary wing systems. DORNIER, C., Friedrichshafen, Lake Constance, Germany. Nov. 30, 1933, No. 15676/34. Convention date, Feb. 16, 1933. Divided out of 416,820. Drawings to Specification. [Class 4.] An aircraft has a stationary or fixed wing and at least two sets of rotatable wings adapted to be retracted into the fixed wing so that a wing of each rotatable set protrudes at each free end of the fixed wing for the purpose of producing additional lift during flight.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE418121X | 1933-02-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB418121A true GB418121A (en) | 1934-10-18 |
Family
ID=6448805
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15676/34A Expired GB418121A (en) | 1933-02-16 | 1933-11-30 | Improvements in or relating to aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB418121A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3207457A (en) * | 1962-11-06 | 1965-09-21 | Adrijan V Kisovec | Convertiplane |
-
1933
- 1933-11-30 GB GB15676/34A patent/GB418121A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3207457A (en) * | 1962-11-06 | 1965-09-21 | Adrijan V Kisovec | Convertiplane |
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