GB574413A - Improvements relating to aircraft wings - Google Patents
Improvements relating to aircraft wingsInfo
- Publication number
- GB574413A GB574413A GB11265/39A GB1126539A GB574413A GB 574413 A GB574413 A GB 574413A GB 11265/39 A GB11265/39 A GB 11265/39A GB 1126539 A GB1126539 A GB 1126539A GB 574413 A GB574413 A GB 574413A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ring
- wing
- space
- spars
- secured
- 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)
- Wind Motors (AREA)
Abstract
574,413. Aircraft wings. BOULTON PAUL AIRCRAFT, Ltd., and NORTH, J. D. April 13, 1939, No. 11265. [Class 4] An aircraft wing has a central part provided with a stress-resisting frame of ring form in plan, the circular space within which is entirely free from bracing so as to accommodate a rotatable gun turret or afford space for cargo, fuel tanks, equipment or passengers. The frame comprises a ring 16 of box section to whichare secured main spars 10, 12 and a subsidiary spar 14. The ribs and spars may extend through the annular space or it may be free of bracing. The central space 18 is, in either case, kept free and may be covered by a member conforming to the contour of the wing or by a domed cupola extending to the outer edge of the ring. Modifications are described in which a single wide spar in each wing is secured to the central ring, or two spars in each wing may be secured to the ring approximately tangentially. The ring may be of I-section instead of box section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB11265/39A GB574413A (en) | 1939-04-13 | 1939-04-13 | Improvements relating to aircraft wings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB11265/39A GB574413A (en) | 1939-04-13 | 1939-04-13 | Improvements relating to aircraft wings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB574413A true GB574413A (en) | 1946-01-04 |
Family
ID=9983027
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB11265/39A Expired GB574413A (en) | 1939-04-13 | 1939-04-13 | Improvements relating to aircraft wings |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB574413A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2656136A (en) * | 1951-01-03 | 1953-10-20 | James V Martin | Flying ship |
-
1939
- 1939-04-13 GB GB11265/39A patent/GB574413A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2656136A (en) * | 1951-01-03 | 1953-10-20 | James V Martin | Flying ship |
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