GB429311A - Improvements in or relating to wing structures for aircraft - Google Patents
Improvements in or relating to wing structures for aircraftInfo
- Publication number
- GB429311A GB429311A GB10018/34A GB1001834A GB429311A GB 429311 A GB429311 A GB 429311A GB 10018/34 A GB10018/34 A GB 10018/34A GB 1001834 A GB1001834 A GB 1001834A GB 429311 A GB429311 A GB 429311A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- spar
- aircraft
- class
- spars
- 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)
- Tires In General (AREA)
Abstract
429,311. Aircraft wing structures. DUNCANSON, F., Seaplane Base, Brough, near Hull. April 3, 1934, No. 10018. [Class 4] Planes, construction of; framework.-The spar or spars of an aircraft wing are arranged to have their weakest section located substantially midway between the wing root and the inner end of the aileron in order that failure of the spar or spars under excessive compression load may result merely in buckling of the wing at this point instead of at the wing root. Fig. 1 shows a wing spar 11 of the type described in Specification 326,870*, [Class 4], which is weakened at A by locally reducing the amount of corrugated material 15, Fig. 3, applied to the upper surface of the spar.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB10018/34A GB429311A (en) | 1934-04-03 | 1934-04-03 | Improvements in or relating to wing structures for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB10018/34A GB429311A (en) | 1934-04-03 | 1934-04-03 | Improvements in or relating to wing structures for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB429311A true GB429311A (en) | 1935-05-28 |
Family
ID=9959912
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB10018/34A Expired GB429311A (en) | 1934-04-03 | 1934-04-03 | Improvements in or relating to wing structures for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB429311A (en) |
-
1934
- 1934-04-03 GB GB10018/34A patent/GB429311A/en not_active Expired
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