GB127711A - Improvements in or relating to Aeroplane-wings having Metal Frames. - Google Patents
Improvements in or relating to Aeroplane-wings having Metal Frames.Info
- Publication number
- GB127711A GB127711A GB9034/18A GB903418A GB127711A GB 127711 A GB127711 A GB 127711A GB 9034/18 A GB9034/18 A GB 9034/18A GB 903418 A GB903418 A GB 903418A GB 127711 A GB127711 A GB 127711A
- Authority
- GB
- United Kingdom
- Prior art keywords
- elements
- spar
- rib
- sections
- plates
- 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)
- Connection Of Plates (AREA)
Abstract
127,711. Mooney, D. J., Brown, E. E., and Wescombe, A. C. May 31. 1918. Planes, construction of; framework.-An assembling. templet for connecting the elements of a metal aeroplane wing spar together and to the rib-sections comprises upper and lower plates C<1>, C<2> connected together by a web C<3>, which constitutes a spacing-piece between the elements A', A<2> of the spar and may be perforated at C<5> to receive these elements. Flanges C<6> at the sides of these perforations provide a riveting connexion. Tongues C<7> - - C" formed on the the plates C<1>, C<2> serve further to position the spar elements. The templet may extend at each side of the spar so as to afford means for connecting the rib-sections D<1>, D<2>; snap-fastenings C<13>, D3 serve to position the rib-sections. Additional connexions between the ribs and spars may be provided by angle-irons F. The spar shown comprises two elements A<1>, A<2> each formed of upper and lower channels A<3>, A<4> connected by corrugated webs A<5>. The elements A', A<2> may be further connected by plates E', E<2>.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB9034/18A GB127711A (en) | 1918-05-31 | 1918-05-31 | Improvements in or relating to Aeroplane-wings having Metal Frames. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB9034/18A GB127711A (en) | 1918-05-31 | 1918-05-31 | Improvements in or relating to Aeroplane-wings having Metal Frames. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB127711A true GB127711A (en) | 1919-06-02 |
Family
ID=32670779
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB9034/18A Expired GB127711A (en) | 1918-05-31 | 1918-05-31 | Improvements in or relating to Aeroplane-wings having Metal Frames. |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB127711A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2013173429A (en) * | 2012-02-24 | 2013-09-05 | Airbus Operations Ltd | Rib-spar joint of aircraft |
-
1918
- 1918-05-31 GB GB9034/18A patent/GB127711A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2013173429A (en) * | 2012-02-24 | 2013-09-05 | Airbus Operations Ltd | Rib-spar joint of aircraft |
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