GB352287A - Improvements in aircraft wings and the like - Google Patents
Improvements in aircraft wings and the likeInfo
- Publication number
- GB352287A GB352287A GB23488/30A GB2348830A GB352287A GB 352287 A GB352287 A GB 352287A GB 23488/30 A GB23488/30 A GB 23488/30A GB 2348830 A GB2348830 A GB 2348830A GB 352287 A GB352287 A GB 352287A
- Authority
- GB
- United Kingdom
- Prior art keywords
- spar
- members
- point
- hill
- rear spar
- 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)
- Braking Arrangements (AREA)
Abstract
352,287. Aircraft wings. BOULTON & PAUL, Ltd., Riverside Works, and NORTH, J. D., Hill House, Eaton Hill, both in Norwich. Aug. 6, 1930, No. 23488. [Class 4.] To prevent relative vertical movements of the two spars of a wing beyond the outermost bracing strut, the top and bottom portions of the relatively deep front spar immediately outside the strut are connected by convergent members E<1>, E<2> to a point on the rear spar near its outer end. The resulting torque of the front spar is resisted by a strong rib or by a second pair of convergent members J<1>, J<2> connected to a point on the rear spar directly behind the connection to the front spar. The members E<1>, E<2>, J<1>, J<2> may converge to single points as shown or they may be spaced apart where they meet the rear spar.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB23488/30A GB352287A (en) | 1930-08-06 | 1930-08-06 | Improvements in aircraft wings and the like |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB23488/30A GB352287A (en) | 1930-08-06 | 1930-08-06 | Improvements in aircraft wings and the like |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB352287A true GB352287A (en) | 1931-07-09 |
Family
ID=10196413
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB23488/30A Expired GB352287A (en) | 1930-08-06 | 1930-08-06 | Improvements in aircraft wings and the like |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB352287A (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 |
-
1930
- 1930-08-06 GB GB23488/30A patent/GB352287A/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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