GB367049A - Aircraft wings - Google Patents
Aircraft wingsInfo
- Publication number
- GB367049A GB367049A GB34933/30A GB3493330A GB367049A GB 367049 A GB367049 A GB 367049A GB 34933/30 A GB34933/30 A GB 34933/30A GB 3493330 A GB3493330 A GB 3493330A GB 367049 A GB367049 A GB 367049A
- Authority
- GB
- United Kingdom
- Prior art keywords
- spars
- secured
- wing
- aircraft
- bracing
- 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)
- Curing Cements, Concrete, And Artificial Stone (AREA)
- Manufacture Of Wood Veneers (AREA)
- Tires In General (AREA)
Abstract
367,049. Aircraft wings. ARMSTRONG WHITWORTH AIRCRAFT, Ltd., SIR W. G. and LLOYD, J., Whitley, near Coventry. Nov. 20,1930, No. 34933. [Class 4.] Each rib of an aircraft wing comprising upper and lower flanges connected by inclined bracing is connected to each spar at one place only. A metal wing is shown in which shaped channel members 26, 27 of the ribs are connected together by shear bracing 28, 29 certain of the members 28 being connected to gusset plates 33 secured to the centres of vertical struts 16 of the spars which have no other connections to the ribs. The metal covering of the wing is connected to the spars through wooden blocks 35, Fig. 5, secured to the flanges of the spars by wood screws passed through hollow rivets 37. Alternatively the blocks 35 may be secured to the spars by long hollow rivets 38, Fig. 6, which alternate with short rivets 37, strips of plywood 39 being inserted under the rivet heads. The spar is constructed as described in Specification 367,048, or it may have shear bracing comprising a lattice work of channel members crossing one another back to back.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34933/30A GB367049A (en) | 1930-11-20 | 1930-11-20 | Aircraft wings |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34933/30A GB367049A (en) | 1930-11-20 | 1930-11-20 | Aircraft wings |
Publications (1)
Publication Number | Publication Date |
---|---|
GB367049A true GB367049A (en) | 1932-02-18 |
Family
ID=10371722
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB34933/30A Expired GB367049A (en) | 1930-11-20 | 1930-11-20 | Aircraft wings |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB367049A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5706764A (en) * | 1996-10-15 | 1998-01-13 | Irbinskas; Heather | Animal training assist apparatus |
US20120273617A1 (en) * | 2009-12-02 | 2012-11-01 | Bladena Aps | Reinforced airfoil shaped body |
-
1930
- 1930-11-20 GB GB34933/30A patent/GB367049A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5706764A (en) * | 1996-10-15 | 1998-01-13 | Irbinskas; Heather | Animal training assist apparatus |
US20120273617A1 (en) * | 2009-12-02 | 2012-11-01 | Bladena Aps | Reinforced airfoil shaped body |
US9416768B2 (en) * | 2009-12-02 | 2016-08-16 | Bladena Aps | Reinforced airfoil shaped body |
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