GB206998A - Improvements in the construction of wings and like members of aeroplane flying machines - Google Patents
Improvements in the construction of wings and like members of aeroplane flying machinesInfo
- Publication number
- GB206998A GB206998A GB28196/22A GB2819622A GB206998A GB 206998 A GB206998 A GB 206998A GB 28196/22 A GB28196/22 A GB 28196/22A GB 2819622 A GB2819622 A GB 2819622A GB 206998 A GB206998 A GB 206998A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sections
- members
- flight
- wing
- transverse
- 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
- 238000010276 construction Methods 0.000 title abstract 2
- 239000002184 metal Substances 0.000 abstract 3
- 238000007747 plating Methods 0.000 abstract 2
- 238000005728 strengthening Methods 0.000 abstract 1
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)
- Connection Of Plates (AREA)
Abstract
206,998. Short, H. O. Oct. 17, 1922. Planes and the like, construction of.-A metal wing is built up of tubular sections the divisions between which extend parallel to the direction of flight, the edges of adjacent sections being overlapped and riveted together. Stiffening members extending in or transverse to the direction of flight, or in both directions, may be fixed to the internal surfaces of the wing sections. Figs. 2 and 3 show respectively crosssections of a wing section 4 taken in the direction of flight and transverse to the direction of flight. The sections are built up of overlapping sheet metal plates 6 of suitable shape, continuous stiffening members 8 of right angle section being positioned externally at the junctions of the wing sections. Strengthening members 7 of channel section are also fixed at intervals to the internal surfaces of the sections and extend transverse to the direction of flight between the members 8, the ends of the flanges of these members 7 being bent downwards so that the edge of the plating 6 of the next wing section 5 and a flange of the angle strip 8 can be inserted between the plating 6 and the bent-down flanges of the members 8, and the whole riveted together. Plates 10 may also be riveted at the nose and trailing edge. The Provisional Specification states that the sections may be fitted with internal structures, which permit them to be threaded on to spars, or if all internal supports are dispensed with the metal covering may be corrugated.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB28196/22A GB206998A (en) | 1922-10-17 | 1922-10-17 | Improvements in the construction of wings and like members of aeroplane flying machines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB28196/22A GB206998A (en) | 1922-10-17 | 1922-10-17 | Improvements in the construction of wings and like members of aeroplane flying machines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB206998A true GB206998A (en) | 1923-11-22 |
Family
ID=10271807
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB28196/22A Expired GB206998A (en) | 1922-10-17 | 1922-10-17 | Improvements in the construction of wings and like members of aeroplane flying machines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB206998A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7677496B2 (en) | 2006-11-03 | 2010-03-16 | Airbus Operations Limited | Stringer for an aircraft wing and a method of reinforcing thereof |
-
1922
- 1922-10-17 GB GB28196/22A patent/GB206998A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7677496B2 (en) | 2006-11-03 | 2010-03-16 | Airbus Operations Limited | Stringer for an aircraft wing and a method of reinforcing thereof |
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