GB206514A - - Google Patents
Info
- Publication number
- GB206514A GB206514A GB27768/23A GB2776823A GB206514A GB 206514 A GB206514 A GB 206514A GB 27768/23 A GB27768/23 A GB 27768/23A GB 2776823 A GB2776823 A GB 2776823A GB 206514 A GB206514 A GB 206514A
- Authority
- GB
- United Kingdom
- Prior art keywords
- riveted
- plates
- spars
- braces
- brackets
- 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)
- Joining Of Building Structures In Genera (AREA)
Abstract
206,514. Rohrbach, A. Nov. 3, 1922, [Convention date]. Planes, construction of; framework.-A metal wing for an aeroplane is built up by attaching front and rear shaping portions 3, 4, Fig. 1, to a central box girder 2 comprising front and rear spars 7, 8, connected at intervals by stiffening bulkheads, braces, or frames, and provided with reinforced top and bottom skin plates 5, 6. The spars 7, 8 may be plates formed with apertures 13, Fig. 6, to reduce their weight or may be constituted by flanged channel members 15, Fig. 8, connected by inclined channeled braces 16. Figs. 4 and 6 show stiffening frames each comprising two vertical bars 14 riveted through brackets 19 to the spars 7, 8, upper and lower cross bars 17, 18 riveted through brackets 11 to the plates 5, 6, and cross-braces 9 riveted to the bars 14, 17, 18. The spars 7, 8 are riveted to the plates 5, 6 through brackets 12. Reinforcing channel members 10 are riveted to the inner faces of the plates 5, 6. Specifications 138,687, 152,308, and 186,039 are referred to.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE206514T | 1922-11-03 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB206514A true GB206514A (en) | 1925-01-22 |
Family
ID=31893094
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB27768/23A Expired GB206514A (en) | 1922-11-03 | 1923-11-05 |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB206514A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111605716A (en) * | 2019-02-22 | 2020-09-01 | 空中客车运营简化股份公司 | Main structure of aircraft hanging rack and aircraft |
-
1923
- 1923-11-05 GB GB27768/23A patent/GB206514A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111605716A (en) * | 2019-02-22 | 2020-09-01 | 空中客车运营简化股份公司 | Main structure of aircraft hanging rack and aircraft |
| CN111605716B (en) * | 2019-02-22 | 2024-02-20 | 空中客车运营简化股份公司 | Main structure of aircraft hanging frame and aircraft |
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