GB338348A - Monoplanes - Google Patents
MonoplanesInfo
- Publication number
- GB338348A GB338348A GB33765/29A GB3376529A GB338348A GB 338348 A GB338348 A GB 338348A GB 33765/29 A GB33765/29 A GB 33765/29A GB 3376529 A GB3376529 A GB 3376529A GB 338348 A GB338348 A GB 338348A
- Authority
- GB
- United Kingdom
- Prior art keywords
- struts
- braced
- strut
- span
- semi
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
338,348. Armstrong Whitworth Aircraft, Ltd., Sir W. G., and Lloyd, J. Nov. 6. 1929. Planes, construction of, and connecting to machine; land wheels; propelling.-A monoplane is braced by depending V-sbaped struts 4 attached to each wing at approximately 30 per cent of the semi-span from the body 2, the strut being cross-braced to the top and bottom of the body by wires 5, 6 also arranged in vees; lift wires 7 extend from the bottom of each strut to a point about 60 per cent of the semi-span from the body, and the bottom ends of the struts are connected by a tension member 8. The struts 4 may support or locate part of a landing gear comprising wheels 13, carried by a centrally jointed axle 14 and enshrouded by fairings 12 carried by the lower ends of the struts. The axes of the propellers are arranged in the wings, as shown, so that the bracing is largely unaffected by the slipstream therefrom.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB33765/29A GB338348A (en) | 1929-11-06 | 1929-11-06 | Monoplanes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB33765/29A GB338348A (en) | 1929-11-06 | 1929-11-06 | Monoplanes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB338348A true GB338348A (en) | 1930-11-20 |
Family
ID=10357148
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB33765/29A Expired GB338348A (en) | 1929-11-06 | 1929-11-06 | Monoplanes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB338348A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113148149A (en) * | 2020-12-21 | 2021-07-23 | 中国航天空气动力技术研究院 | Solar unmanned aerial vehicle with pull wire |
-
1929
- 1929-11-06 GB GB33765/29A patent/GB338348A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113148149A (en) * | 2020-12-21 | 2021-07-23 | 中国航天空气动力技术研究院 | Solar unmanned aerial vehicle with pull wire |
| CN113148149B (en) * | 2020-12-21 | 2023-08-04 | 中国航天空气动力技术研究院 | Solar unmanned aerial vehicle with stay wire |
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