GB138401A - Improvements in the manufacture of aeroplane wings - Google Patents
Improvements in the manufacture of aeroplane wingsInfo
- Publication number
- GB138401A GB138401A GB882/19A GB88219A GB138401A GB 138401 A GB138401 A GB 138401A GB 882/19 A GB882/19 A GB 882/19A GB 88219 A GB88219 A GB 88219A GB 138401 A GB138401 A GB 138401A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ribs
- spars
- strips
- spar
- tenon
- 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
138,401. Tarrant, W. G. Jan. 13. 1919. No Patent granted (Sealing fee not paid). Planes, construction of; framework.-In a wing structure for aeroplanes, the front and rear spars 1 are connected to the ribs 3 by pairs of wooden strips 8, 10 attached to the webs 4 of the ribs in front of and behind each spar, a tenon 9, which passes through the spar, being secured between each pair of strips 8, 10. At the leading edge of the wing, the upper and lower portions of the rib are connected by a member 111, and a pair of strips 12. with a tenon 13 between them, are secured to the webs 4. The spars 1 are composed of longitudinal members 5 grooved to receive the beaded ends 6 of crossbraces 7. The upper and lower portions of the ribs are connected by cross-braces 14, and the ribs arc connected by stringers parallel to the spars.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB882/19A GB138401A (en) | 1919-01-13 | 1919-01-13 | Improvements in the manufacture of aeroplane wings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB882/19A GB138401A (en) | 1919-01-13 | 1919-01-13 | Improvements in the manufacture of aeroplane wings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB138401A true GB138401A (en) | 1920-02-12 |
Family
ID=9712124
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB882/19A Expired GB138401A (en) | 1919-01-13 | 1919-01-13 | Improvements in the manufacture of aeroplane wings |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB138401A (en) |
-
1919
- 1919-01-13 GB GB882/19A patent/GB138401A/en not_active Expired
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