GB462390A - Improved construction of wings, aerofoils and the like for aeronautical machines - Google Patents
Improved construction of wings, aerofoils and the like for aeronautical machinesInfo
- Publication number
- GB462390A GB462390A GB24138/35A GB2413835A GB462390A GB 462390 A GB462390 A GB 462390A GB 24138/35 A GB24138/35 A GB 24138/35A GB 2413835 A GB2413835 A GB 2413835A GB 462390 A GB462390 A GB 462390A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ribs
- flats
- booms
- straps
- secured
- 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)
- Body Structure For Vehicles (AREA)
Abstract
462,390. Aircraft structures. MAYROW, J. J. Aug. 29, 1935, No. 24138. [Class 4] Aircraft structures and in particular thick wing structures comprise ribs 2 of zigzag formation, Fig. 2, assembled in such manner as to form upper and lower reticulated frames which are spaced apart by posts 4 and are directly secured to the outer covering or skin 1 of the wing or other structure. Longitudinal booms 3 are also secured to the outer covering and to the ribs at the points of inter-attachment thereof, Fig. 6. Ribs 2 are of channel section shaped at the bends to form flats 2a and to form recesses to allow passage of the booms 3. Adjacent ribs are attached to each other and to the booms at each junction by straps 5, Fig. 5, bent to the shape of the rib angle at 5a, and to that of the underside of the boom at 5b. Parts 5a of opposed straps are introduced between flats 2a of the ribs, the strap extending under the rib channel and then upwardly to connect with the boom, Fig. 6. Tubular posts 4 are secured to flats 5c, Fig. 5, of straps 5 by flanges 6, Fig. 2 ; the joints may be stiffened by additional gussets such as 7.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB24138/35A GB462390A (en) | 1935-08-29 | 1935-08-29 | Improved construction of wings, aerofoils and the like for aeronautical machines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB24138/35A GB462390A (en) | 1935-08-29 | 1935-08-29 | Improved construction of wings, aerofoils and the like for aeronautical machines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB462390A true GB462390A (en) | 1937-03-01 |
Family
ID=10206983
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24138/35A Expired GB462390A (en) | 1935-08-29 | 1935-08-29 | Improved construction of wings, aerofoils and the like for aeronautical machines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB462390A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2007020069A1 (en) * | 2005-08-17 | 2007-02-22 | Airbus Deutschland Gmbh | Support structure for a wing |
-
1935
- 1935-08-29 GB GB24138/35A patent/GB462390A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2007020069A1 (en) * | 2005-08-17 | 2007-02-22 | Airbus Deutschland Gmbh | Support structure for a wing |
US8205834B2 (en) | 2005-08-17 | 2012-06-26 | Airbus Deutschland Gmbh | Support structure for a wing |
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