GB182464A - Improvements in aircraft - Google Patents
Improvements in aircraftInfo
- Publication number
- GB182464A GB182464A GB17644/22A GB1764422A GB182464A GB 182464 A GB182464 A GB 182464A GB 17644/22 A GB17644/22 A GB 17644/22A GB 1764422 A GB1764422 A GB 1764422A GB 182464 A GB182464 A GB 182464A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ribs
- wings
- cords
- portions
- steering
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
- B64C3/50—Varying camber by leading or trailing edge flaps
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
Abstract
182,464. Dewoitine, E. June 27, 1921, [Convention date]. Void [Published under Sect. 91 of the Act]. Planes, construction of; steering and balancing.-Aircraft wings have indeformable front portions a, rigidly secured to the fuselage, and rear portions formed of upper and lower flexible members b<1>, b<2> connected to ribs c which are hinged to the portions a at c', so that the camber of the wings increases as the incidence is increased. There may be flexible trailing edges g deformable by the wind. For steering purposes, the wings on opposite sides of the machine may be separately operated. Springs d may connect the members b<1> to the ribs c. The ribs c may be moved by cams e on shafts f, or, as shown in Fig. 4, they may be actuated by hollow rods i screw-coupled to the front portions a by nuts having drums j around which cords q are wound. The cords q are passed around pulleys i<1> on a shaft m, which can be turned by a wheel o through worm-gear m, for extending or retracting the rods i.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| BE182464X | 1921-06-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB182464A true GB182464A (en) | 1923-09-26 |
Family
ID=3864342
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB17644/22A Expired GB182464A (en) | 1921-06-27 | 1922-06-27 | Improvements in aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB182464A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1998021091A1 (en) * | 1996-11-14 | 1998-05-22 | Philippe Arribi | Flow form |
| CN113562159A (en) * | 2021-08-10 | 2021-10-29 | 大连理工大学 | Wing rib structure of intelligent bionic deformable wing |
-
1922
- 1922-06-27 GB GB17644/22A patent/GB182464A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1998021091A1 (en) * | 1996-11-14 | 1998-05-22 | Philippe Arribi | Flow form |
| CN113562159A (en) * | 2021-08-10 | 2021-10-29 | 大连理工大学 | Wing rib structure of intelligent bionic deformable wing |
| CN113562159B (en) * | 2021-08-10 | 2023-07-14 | 大连理工大学 | Wing rib structure of intelligent bionic deformable wing |
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