GB333833A - Improvements in and relating to the construction of wings, tail units, and the like for flying machines - Google Patents
Improvements in and relating to the construction of wings, tail units, and the like for flying machinesInfo
- Publication number
- GB333833A GB333833A GB35217/29A GB3521729A GB333833A GB 333833 A GB333833 A GB 333833A GB 35217/29 A GB35217/29 A GB 35217/29A GB 3521729 A GB3521729 A GB 3521729A GB 333833 A GB333833 A GB 333833A
- Authority
- GB
- United Kingdom
- Prior art keywords
- booms
- corrugated sheet
- construction
- wings
- relating
- 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)
- Tents Or Canopies (AREA)
Abstract
333,833. Junkers, H. Dec. 10, 1928, [Convention date]. Planes, construction of. - Aircraft supporting surfaces of the type consisting of an internal framework enclosed by a sheathing of corrugated metal so arranged that the corrugation run in a fore and aft direction in the line of flight, are modified in that non-corrugated sheet covering is used for the major portion of the upper part of the surface and for portions, such as the wing tip, of the lower part as are not highly stressed. Those portions of the upper surface which require reinforcement such as the leading edge and walkways have corrugated sheet-metal covering. Fig. 1 illustrates a cross-section of a wing having an internal structure composed of booms 1, diagonal struts 2 and profile ribs 3; the upper surface is covered by plain sheets 5 secured to the booms 1 and to the ribs 3 whilst the lower surface is constituted by a corrugated sheet 4 secured directly to the lower booms 1 and forming a crosstie between them.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE333833X | 1928-12-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB333833A true GB333833A (en) | 1930-08-21 |
Family
ID=6212452
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB35217/29A Expired GB333833A (en) | 1928-12-10 | 1929-11-18 | Improvements in and relating to the construction of wings, tail units, and the like for flying machines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB333833A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8602356B2 (en) | 2005-08-17 | 2013-12-10 | Airbus Operations Gmbh | Framework wing box for a wing |
-
1929
- 1929-11-18 GB GB35217/29A patent/GB333833A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8602356B2 (en) | 2005-08-17 | 2013-12-10 | Airbus Operations Gmbh | Framework wing box for a wing |
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