GB500076A - Aerofoil structure - Google Patents
Aerofoil structureInfo
- Publication number
- GB500076A GB500076A GB1030/38A GB103038A GB500076A GB 500076 A GB500076 A GB 500076A GB 1030/38 A GB1030/38 A GB 1030/38A GB 103038 A GB103038 A GB 103038A GB 500076 A GB500076 A GB 500076A
- Authority
- GB
- United Kingdom
- Prior art keywords
- segments
- wing
- members
- secured
- longitudinally
- 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
500,076. Aircraft structures. BARKLEY, A. ST. C. Jan. 12, 1938, No. 1030. [Claes 4] In an aircraft wing structure in which longitudinally-fluted sheet-metal segments are secured together to form a series of closed polygonal or circular passages extending along the wing, longitudinally-extending reinforcing- members are secured to the upper and lower stressed skins of the wing and to the segments. In one form, the segments are flanged at 7 and riveted to the skin 4. A member 9 may be inserted. In further modifications, the segments may be secured to the skin by members 10, Fig. 3, of greater thickness than the segments. The thickness of the members 10 is reduced towards the wing tips. British Specification 482,166 and U.S.A. Specification 2,071,317 are referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1030/38A GB500076A (en) | 1938-01-12 | 1938-01-12 | Aerofoil structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1030/38A GB500076A (en) | 1938-01-12 | 1938-01-12 | Aerofoil structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB500076A true GB500076A (en) | 1939-02-02 |
Family
ID=9714916
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1030/38A Expired GB500076A (en) | 1938-01-12 | 1938-01-12 | Aerofoil structure |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB500076A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2203530A (en) * | 1987-03-31 | 1988-10-19 | Actionair Equip | Shut-off damper |
| US8087614B2 (en) | 2006-06-15 | 2012-01-03 | Airbus Operations Limited | Stringer for an aircraft wing and a method of forming thereof |
-
1938
- 1938-01-12 GB GB1030/38A patent/GB500076A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2203530A (en) * | 1987-03-31 | 1988-10-19 | Actionair Equip | Shut-off damper |
| GB2203530B (en) * | 1987-03-31 | 1991-05-01 | Actionair Equip | Shut-off damper |
| US8087614B2 (en) | 2006-06-15 | 2012-01-03 | Airbus Operations Limited | Stringer for an aircraft wing and a method of forming thereof |
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