GB117926A - Improvements in or relating to Aircraft and other Light-weight Apparatus. - Google Patents
Improvements in or relating to Aircraft and other Light-weight Apparatus.Info
- Publication number
- GB117926A GB117926A GB1073617A GB1073617A GB117926A GB 117926 A GB117926 A GB 117926A GB 1073617 A GB1073617 A GB 1073617A GB 1073617 A GB1073617 A GB 1073617A GB 117926 A GB117926 A GB 117926A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- tubes
- tube
- aircraft
- shows
- 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
- B64C3/18—Spars; Ribs; Stringers
- B64C3/185—Spars
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Rod-Shaped Construction Members (AREA)
Abstract
117,926. Crowe, S. July 26, 1917. Framework; planes, construction of.-Spars, girders, struts, &c. for aircraft and other light structures are composed of outer longitudinal members connected together and to one or more intermediate tubular members or cores by series of transverse members. Fig. 1 shows upper and lower channels a connected to a tube b bv transverse members c comprising tubes with splayed ends. The tubes c are passed through holes in the tube b and secured thereto; or the tube b may pass through the tubes c. Fig. 3 shows another form having two tubes b<1>, b<2> connected by short lengths of rectangular tubing g to the members a, which are composed of angle-members with their flanges f placed together. In another form, the transverse members comprise flanged plates set obliquely. Fig. 6 shows a method of jointing together a spar and web by means of plates j. The outer members a may be constituted by a tubular structure surrounding the core b, and the tubes b may be ribbed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1073617A GB117926A (en) | 1917-07-26 | 1917-07-26 | Improvements in or relating to Aircraft and other Light-weight Apparatus. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1073617A GB117926A (en) | 1917-07-26 | 1917-07-26 | Improvements in or relating to Aircraft and other Light-weight Apparatus. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB117926A true GB117926A (en) | 1918-07-26 |
Family
ID=32671495
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1073617A Expired GB117926A (en) | 1917-07-26 | 1917-07-26 | Improvements in or relating to Aircraft and other Light-weight Apparatus. |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB117926A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8186622B2 (en) | 2006-03-27 | 2012-05-29 | Airbus Operations Limited | Aircraft component |
-
1917
- 1917-07-26 GB GB1073617A patent/GB117926A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8186622B2 (en) | 2006-03-27 | 2012-05-29 | Airbus Operations Limited | Aircraft component |
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