GB356129A - Mode of construction of wings for flying apparatus - Google Patents
Mode of construction of wings for flying apparatusInfo
- Publication number
- GB356129A GB356129A GB6540/30A GB654030A GB356129A GB 356129 A GB356129 A GB 356129A GB 6540/30 A GB6540/30 A GB 6540/30A GB 654030 A GB654030 A GB 654030A GB 356129 A GB356129 A GB 356129A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- spars
- wing
- angles
- 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)
- Joining Of Building Structures In Genera (AREA)
Abstract
356,129. Aircraft wings. SOC. ANON. DES ATELIERS & CHANTIERS DE LA LOIRE, 4, Rue de Teheran, Paris. Feb. 27, 1930, No. 6540. Convention date, March 1, 1929. Void [Published under Sect. 91 of the Acts]. [Class 4.] Aircraft wings have the drag-bracing between the spars composed of compression members b arranged as in a Warren girder. The compression members may extend the full depth of the wing and be shaped to its profile so as to support the covering material through the intermediary of stringers c, let into notches in the members b, thus dispensing with ribs. The members b make angles of 60‹ with the spars so that identical flanged gusset plates e, Fig. 5, may be used in all the angles for securing the members b to the spar flanges and to one another. At the angles between the members b, gusset plates may be used at intervals along the full depth of the wing. The members b may be reinforced by L-members bl. A wing having detachable leading and trailing edges is described, attachment lugs being formed on the members b where they meet the spars. Where an intermediate spar is used, the front and rear spars are similarly braced to the intermediate spar.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR356129X | 1929-03-01 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB356129A true GB356129A (en) | 1931-08-31 |
Family
ID=8893448
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB6540/30A Expired GB356129A (en) | 1929-03-01 | 1930-02-27 | Mode of construction of wings for flying apparatus |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB356129A (en) |
-
1930
- 1930-02-27 GB GB6540/30A patent/GB356129A/en not_active Expired
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