GB410405A - Improvements in and connected with aeroplane wings and/or tail sections - Google Patents
Improvements in and connected with aeroplane wings and/or tail sectionsInfo
- Publication number
- GB410405A GB410405A GB29090/33A GB2909033A GB410405A GB 410405 A GB410405 A GB 410405A GB 29090/33 A GB29090/33 A GB 29090/33A GB 2909033 A GB2909033 A GB 2909033A GB 410405 A GB410405 A GB 410405A
- Authority
- GB
- United Kingdom
- Prior art keywords
- secured
- members
- spars
- struts
- aircraft
- 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)
- Tents Or Canopies (AREA)
Abstract
410,405. Aircraft planes. MARTIN, J., Martin's Aircraft Works, Higher Denham, Buckinghamshire. Oct. 20, 1933, No. 29090. [Class 4.] An aircraft wing, tail plane or control plane is constructed with two spars connected together by stiff X-shaped bracing extending the full depth of the spar and rigidly secured together at their intersections. The upper and lower edges of the bracing may be curved to the contour of the plane or separate profiling members may be secured thereto. A metal wing structure is shown having two spars composed of tubular booms 3 secured to webs 1, the two spars being interconnected by channel section bracing members 11 with abutting members 12, 13. These members, together with struts 20 when used, are secured to flattened portions 6 on the spars by plates 7 and to the webs 1 by L-brackets 16. The members 11, 12, 13 are secured together at their intersection by L-brackets 14 and at their upper and lower edges by plates 15. In a biplane structure, any interplane struts have flared ends secured to the.struts 20. A wooden framework is described comprising flat boards secured at their junctions by angular blocks.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB29090/33A GB410405A (en) | 1933-10-20 | 1933-10-20 | Improvements in and connected with aeroplane wings and/or tail sections |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB29090/33A GB410405A (en) | 1933-10-20 | 1933-10-20 | Improvements in and connected with aeroplane wings and/or tail sections |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB410405A true GB410405A (en) | 1934-05-17 |
Family
ID=10285984
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB29090/33A Expired GB410405A (en) | 1933-10-20 | 1933-10-20 | Improvements in and connected with aeroplane wings and/or tail sections |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB410405A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2563422A (en) * | 2017-06-15 | 2018-12-19 | Airbus Operations Ltd | A spar arrangement in a wing tip device |
-
1933
- 1933-10-20 GB GB29090/33A patent/GB410405A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2563422A (en) * | 2017-06-15 | 2018-12-19 | Airbus Operations Ltd | A spar arrangement in a wing tip device |
| US11643183B2 (en) | 2017-06-15 | 2023-05-09 | Airbus Operations Limited | Spar arrangement in a wing tip device |
| US11958597B2 (en) | 2017-06-15 | 2024-04-16 | Airbus Operations Limited | Spar arrangement in a wing tip device |
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