GB315793A - Improvements in single spar aircraft wings and damping surfaces - Google Patents
Improvements in single spar aircraft wings and damping surfacesInfo
- Publication number
- GB315793A GB315793A GB21905/29A GB2190529A GB315793A GB 315793 A GB315793 A GB 315793A GB 21905/29 A GB21905/29 A GB 21905/29A GB 2190529 A GB2190529 A GB 2190529A GB 315793 A GB315793 A GB 315793A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sections
- spar
- wing
- stiffening
- plates
- 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
- B64C3/18—Spars; Ribs; Stringers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
Abstract
315,793. Messerschmitt, W. July 18, 1928, [Convention date]. Planes and the like, construction of.-A single spar aircraft wing or damping surface is constructed with the stiffening ribs divided into several sections R' - - R<4>, these sections being combined with the adjoining plates a-b, a-c, b-d, c-e of the outer skin B extending along the whole or a, large portion of the span and with continuous stiffening sections P secured to the plates, to form partial aggregates which may be trough-shaped or flat according to the shape of the part of the wing which they form, and are singly connected to the spar H to form a final continuous structure in which all the parts, including the skin B, contribute to the strength of the wing. The rib sections are T-section and are attached to spar H and to a light division G by angle sections n; one or more diagonals D may be included. Rivets or screws may be used in assembling and additional stiffening may be provided at the connections.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE315793X | 1928-07-18 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB315793A true GB315793A (en) | 1930-08-21 |
Family
ID=6150295
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB21905/29A Expired GB315793A (en) | 1928-07-18 | 1929-07-16 | Improvements in single spar aircraft wings and damping surfaces |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB315793A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2433999A (en) * | 1944-06-10 | 1948-01-06 | Vidal Corp | Wing and stabilizer structure for gliders |
| US2451458A (en) * | 1943-06-28 | 1948-10-12 | Budd Co | Aircraft airfoil construction |
| US2451454A (en) * | 1943-06-28 | 1948-10-12 | Budd Co | Method of fabricating airfoils |
-
1929
- 1929-07-16 GB GB21905/29A patent/GB315793A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2451458A (en) * | 1943-06-28 | 1948-10-12 | Budd Co | Aircraft airfoil construction |
| US2451454A (en) * | 1943-06-28 | 1948-10-12 | Budd Co | Method of fabricating airfoils |
| US2433999A (en) * | 1944-06-10 | 1948-01-06 | Vidal Corp | Wing and stabilizer structure for gliders |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB315793A (en) | Improvements in single spar aircraft wings and damping surfaces | |
| GB524721A (en) | Improvements in and relating to "stressed skin" fuselages or nacelles for aircraft | |
| GB303360A (en) | Improvements in metal aircraft wings | |
| GB520249A (en) | Improvements in stressed-skin structures of fuselages, wings and other hollow bodies of aircraft | |
| ES178645A1 (en) | IMPROVEMENTS IN AIRCRAFT CONSTRUCTION | |
| GB482166A (en) | Aeroplane wing structure | |
| US1939506A (en) | Aircraft construction | |
| GB329615A (en) | Improvements in aeroplane fuselage construction | |
| US1766376A (en) | Method for attaching on fuselages wings having single spars | |
| GB458286A (en) | Improvements in or relating to aircraft wings | |
| GB364534A (en) | Improvements in aircraft | |
| GB392447A (en) | Single spar aircraft wing with auxiliary spars | |
| GB339132A (en) | Improvements in or relating to airplane construction | |
| GB204304A (en) | Improvements in or relating to stays for aeroplanes, hydroplanes, and the like | |
| GB329612A (en) | Improvements in aeroplane fuselage construction | |
| GB288683A (en) | Improvements in the aerofoils of monoplanes | |
| GB229389A (en) | Improvements in metal construction for aeronautical machines | |
| GB315792A (en) | Improvements in single spar aircraft wings and damping surfaces | |
| GB458789A (en) | Improvements in or connected with the construction of aircraft wings | |
| GB382176A (en) | Improvements in or relating to wing structure for flying machines | |
| GB259995A (en) | Improvements in and relating to aircraft wings | |
| GB341853A (en) | Improvements in the construction of aeroplane wings | |
| GB190254A (en) | Improvements in the construction of metal aeroplane wings | |
| GB305675A (en) | Improvements in and relating to supporting wings or planes for aircraft | |
| GB289640A (en) | Improvements relating to aircraft wing rib construction |