GB484305A - Improvements in or relating to aircraft wing construction - Google Patents
Improvements in or relating to aircraft wing constructionInfo
- Publication number
- GB484305A GB484305A GB29909/36A GB2990936A GB484305A GB 484305 A GB484305 A GB 484305A GB 29909/36 A GB29909/36 A GB 29909/36A GB 2990936 A GB2990936 A GB 2990936A GB 484305 A GB484305 A GB 484305A
- Authority
- GB
- United Kingdom
- Prior art keywords
- webs
- aircraft
- wing
- flanges
- members
- 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
Abstract
484,305. Aircraft - wing structure. DEEKAY AIRCRAFT CORPORATION, Ltd., and STILL, S. C. HART-. Nov. 3, 1936, No. 29909. [Class 4] A stressed skin aircraft wing comprises two or more spanwise cells formed by vertical members of multi-ply wood and top and bottom chordwise members of the same material, the vertical members being reinforced by beams secured thereto at or adjacent the top and bottom surfaces thereof. A main wing portion, Fig. 1, to which leading and trailing parts may be hinged comprises multi-ply webs 2 having wood flanges 4 and vertical stiffeners 9, Fig. 2, united by plywood covering 3 which may be re-inforced by fore and aft stringers 10 located by notches cut in the marginal surfaces of the webs and flanges. Bulkheads 17 may be provided. The webs 2 may taper and approach one another toward the wing tip.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB29909/36A GB484305A (en) | 1936-11-03 | 1936-11-03 | Improvements in or relating to aircraft wing construction |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB29909/36A GB484305A (en) | 1936-11-03 | 1936-11-03 | Improvements in or relating to aircraft wing construction |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB484305A true GB484305A (en) | 1938-05-03 |
Family
ID=10299173
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB29909/36A Expired GB484305A (en) | 1936-11-03 | 1936-11-03 | Improvements in or relating to aircraft wing construction |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB484305A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2482798A (en) * | 1946-02-27 | 1949-09-27 | Jr George B Rheinfrank | Aircraft wing and method of manufacture |
| US2563218A (en) * | 1948-04-09 | 1951-08-07 | United Aircraft Corp | Laminated airfoil section and method of making same |
| CN104340356A (en) * | 2013-08-09 | 2015-02-11 | 波音公司 | Aircraft side of body joint |
| CN107745798A (en) * | 2017-10-23 | 2018-03-02 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | A kind of aircraft clip center span is to beam and wing root area attachment structure |
-
1936
- 1936-11-03 GB GB29909/36A patent/GB484305A/en not_active Expired
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2482798A (en) * | 1946-02-27 | 1949-09-27 | Jr George B Rheinfrank | Aircraft wing and method of manufacture |
| US2563218A (en) * | 1948-04-09 | 1951-08-07 | United Aircraft Corp | Laminated airfoil section and method of making same |
| CN104340356A (en) * | 2013-08-09 | 2015-02-11 | 波音公司 | Aircraft side of body joint |
| CN104340356B (en) * | 2013-08-09 | 2018-06-05 | 波音公司 | Aircraft body joint side |
| US10479475B2 (en) | 2013-08-09 | 2019-11-19 | The Boeing Company | Composite stringer beam joint structure of an aircraft |
| US10717511B2 (en) | 2013-08-09 | 2020-07-21 | The Boeing Company | Aircraft side of body joint |
| CN107745798A (en) * | 2017-10-23 | 2018-03-02 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | A kind of aircraft clip center span is to beam and wing root area attachment structure |
| CN107745798B (en) * | 2017-10-23 | 2023-08-25 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Connection structure for central spanwise beam and wing root zone of aircraft shear port |
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