GB442667A - Ornithopter - Google Patents
OrnithopterInfo
- Publication number
- GB442667A GB442667A GB15806/34A GB1580634A GB442667A GB 442667 A GB442667 A GB 442667A GB 15806/34 A GB15806/34 A GB 15806/34A GB 1580634 A GB1580634 A GB 1580634A GB 442667 A GB442667 A GB 442667A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- winglets
- spar
- springs
- wings
- 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
- 230000004075 alteration Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C33/00—Ornithopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/40—Ornithopters
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
442,667. Ornithopter. HAENLE, K., 99, Finkenkrugerweg, Staaken, Berlin. May 28, 1934, No. 15806. [Class 4] The wings of an ornithopter comprise several stiff and indeformable winglets rotatable over the wing span by means of bearings disposed between the leading edge of the winglets and the centre of pressure, springs being disposed between the winglets and the spar in such manner that alteration of the angle of incidence between the winglets and the spar alters the tension of the springs. As shown in Fig. 6, the machine comprises a fixed wing W and flapping wings F<1>, F<2>, adapted to oscillate about axes A, Fig. 2. Wings F<1>, F<2> comprise spars H and rigid wing- lets f connected thereto by bearings and by springs K, Fig. 3. Means are provided for altering the tension of the springs K in each wing either in the same sense to provide elevator control or in opposite senses to give lateral control. These means comprise a screw spindle X, Fig. 9, carried by the fore- and-aft bearing of each flapping wing and having a recess at its inner end engaged by pins affixed to a lever P secured to the spar. Rotation of screw X thus causes rotation of the spar about its longitudinal axis.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB15806/34A GB442667A (en) | 1934-05-28 | 1934-05-28 | Ornithopter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB15806/34A GB442667A (en) | 1934-05-28 | 1934-05-28 | Ornithopter |
Publications (1)
Publication Number | Publication Date |
---|---|
GB442667A true GB442667A (en) | 1936-01-29 |
Family
ID=10065806
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15806/34A Expired GB442667A (en) | 1934-05-28 | 1934-05-28 | Ornithopter |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB442667A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1958681A1 (en) * | 2007-02-13 | 2008-08-20 | Proxflyer As | System for controlling flight direction |
CN109353498A (en) * | 2018-12-04 | 2019-02-19 | 南京航空航天大学 | The wing of flapping wing aircraft |
-
1934
- 1934-05-28 GB GB15806/34A patent/GB442667A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1958681A1 (en) * | 2007-02-13 | 2008-08-20 | Proxflyer As | System for controlling flight direction |
CN101293568B (en) * | 2007-02-13 | 2011-06-08 | 普罗克斯飞行有限公司 | System for controlling flight direction |
US8336809B2 (en) | 2007-02-13 | 2012-12-25 | Proxflyer As | System for controlling flight direction |
CN109353498A (en) * | 2018-12-04 | 2019-02-19 | 南京航空航天大学 | The wing of flapping wing aircraft |
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