GB416820A - Improvements in or relating to aircraft - Google Patents
Improvements in or relating to aircraftInfo
- Publication number
- GB416820A GB416820A GB33638/33A GB3363833A GB416820A GB 416820 A GB416820 A GB 416820A GB 33638/33 A GB33638/33 A GB 33638/33A GB 3363833 A GB3363833 A GB 3363833A GB 416820 A GB416820 A GB 416820A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wings
- shaft
- aircraft
- retracted
- superposed
- 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
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/02—Gyroplanes
- B64C27/021—Rotor or rotor head construction
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/30—Inverted burners, e.g. for illumination
Abstract
416,820. Aircraft with rotary wing systems. DORNIER, C., Friedrichshafen, Lake Constance, Germany. Nov. 30, 1933, No. 33638. Convention date, Feb. 16. [Class 4.] An aircraft comprises stationary wings 5 and an arrangement of rotatable wings which are adapted to be displaced so as to occupy a position parallel or approximately parallel to their supporting shaft, or to be displaced so as to occupy a superposed position, and to be withdrawn or retracted wholly or partly into the aircraft fuselage. In one form, the rotatable wings 7 articulated on a hub 9 may be folded through struts 10 by movement of a sleeve 11 lockable on the shaft 8 and the whole may then be retracted by hinging the shaft 8 about a pivot 12. A support 13 for the retracted wings is provided. In a modification, bracings 21, Fig. 3, are removed and the wings 18, 19 are rocked around the shaft 20 to assume a superposed position over the wing 17. The wings when superposed may be locked in a fore and aft direction.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE416820X | 1909-06-23 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB416820A true GB416820A (en) | 1934-09-21 |
Family
ID=6448621
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB33638/33A Expired GB416820A (en) | 1933-02-16 | 1933-11-30 | Improvements in or relating to aircraft |
Country Status (2)
| Country | Link |
|---|---|
| FR (1) | FR416820A (en) |
| GB (1) | GB416820A (en) |
-
1910
- 1910-06-06 FR FR416820D patent/FR416820A/en not_active Expired
-
1933
- 1933-11-30 GB GB33638/33A patent/GB416820A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR416820A (en) | 1910-10-29 |
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