GB129023A - Improvements in the Construction of Metal Frames for Aircraft. - Google Patents
Improvements in the Construction of Metal Frames for Aircraft.Info
- Publication number
- GB129023A GB129023A GB13856/17A GB1385617A GB129023A GB 129023 A GB129023 A GB 129023A GB 13856/17 A GB13856/17 A GB 13856/17A GB 1385617 A GB1385617 A GB 1385617A GB 129023 A GB129023 A GB 129023A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plates
- spars
- shows
- cross
- construction
- 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)
- Rod-Shaped Construction Members (AREA)
Abstract
129,023. Brown, E. E., and Mooney, D. J. Sept. 26, 1917. Framework; planes, construction of. -The spars of aircraft wings and fuselages are constructed of top and bottom metal plates a, Figs. 1 and 2, connected together at each side by rectangular plates b flanged along each edge, transverse plates d being secured between the ends of adjacent plates b and extended on one or more sides to form wing ribs or cross-frames of fuselages, or for the attachment of ribs, fairing edges, &c. The plates b, d are formed with apertures and embossed. In the .form shown in Fig. 5, the top and bottom plates a are made continuous with a side portion f, which replaces one row of plates b. Fig. 10, shows a section of a rib formed from a plate d, the upper and lower flanges i being strengthened by diagonal strips k. Fig. 13 shows a rib composed of upper and lower channels n connected by a web formed by diagonal wiring or channel strip o, which is nipped between the flanges of the channels at the parts p and secured to the plates d of the spars. Fig. 14 shows a cross-section of a fuselage composed of spars r and transverse members s formed as a continuation of, or connected to, the cross-plates d of the spars.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB13856/17A GB129023A (en) | 1917-09-26 | 1917-09-26 | Improvements in the Construction of Metal Frames for Aircraft. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB13856/17A GB129023A (en) | 1917-09-26 | 1917-09-26 | Improvements in the Construction of Metal Frames for Aircraft. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB129023A true GB129023A (en) | 1919-07-10 |
Family
ID=32346174
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB13856/17A Expired GB129023A (en) | 1917-09-26 | 1917-09-26 | Improvements in the Construction of Metal Frames for Aircraft. |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB129023A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115447763A (en) * | 2022-10-12 | 2022-12-09 | 中国航空工业集团公司西安飞机设计研究所 | Main fairing structure of airplane |
-
1917
- 1917-09-26 GB GB13856/17A patent/GB129023A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115447763A (en) * | 2022-10-12 | 2022-12-09 | 中国航空工业集团公司西安飞机设计研究所 | Main fairing structure of airplane |
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