GB126710A - Improvements in or relating to Aircraft. - Google Patents
Improvements in or relating to Aircraft.Info
- Publication number
- GB126710A GB126710A GB2569/17A GB256917A GB126710A GB 126710 A GB126710 A GB 126710A GB 2569/17 A GB2569/17 A GB 2569/17A GB 256917 A GB256917 A GB 256917A GB 126710 A GB126710 A GB 126710A
- Authority
- GB
- United Kingdom
- Prior art keywords
- boarding
- grooved
- longerons
- hoops
- receive
- 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
- 238000005192 partition Methods 0.000 abstract 1
- 239000011122 softwood Substances 0.000 abstract 1
- 239000002023 wood Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/064—Stringers; Longerons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0063—Fuselage structures substantially made from particular materials from wood
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Rod-Shaped Construction Members (AREA)
Abstract
126,710. Vickers, Ltd., and Burgoine, S. F. Feb. 21, 1917. Framework; cars. - Aeroplane fuselages and nacelles and airship cars are constructed wholly of wood and comprise longerons grooved to receive boarding which is cut at intervals into holes strengthened at their edges by hoops. Figs. 1 and 2 show an elevation and plan of a fuselage having four longerons A of soft wood grooved to receive three-ply boarding B, E having openings C, F fitted with hoops D, G of ash grooved to fit over the boarding. Strengthening-struts H, J, each in two parts laid on opposite sides of the boarding, are connected to the longerons A, and the inner parts are grooved to receive transverse partitions which also have openings strengthened by hoops. The boarding is cut in small sections joined as shown at N along their smallest dimensions.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2569/17A GB126710A (en) | 1917-02-21 | 1917-02-21 | Improvements in or relating to Aircraft. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2569/17A GB126710A (en) | 1917-02-21 | 1917-02-21 | Improvements in or relating to Aircraft. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB126710A true GB126710A (en) | 1919-05-22 |
Family
ID=32341043
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2569/17A Expired GB126710A (en) | 1917-02-21 | 1917-02-21 | Improvements in or relating to Aircraft. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB126710A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2469421A (en) * | 1944-04-15 | 1949-05-10 | Richard L Tuve | Heat-action explosive pyrotechnic marker |
-
1917
- 1917-02-21 GB GB2569/17A patent/GB126710A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2469421A (en) * | 1944-04-15 | 1949-05-10 | Richard L Tuve | Heat-action explosive pyrotechnic marker |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB531357A (en) | Improvements in or relating to aircraft fusilages | |
GB126710A (en) | Improvements in or relating to Aircraft. | |
GB524721A (en) | Improvements in and relating to "stressed skin" fuselages or nacelles for aircraft | |
GB130623A (en) | Improvements in or connected with Aeroplane Fuselages. | |
GB759529A (en) | Improvements in and relating to fuselages and nacelles for aircraft and the like | |
GB327805A (en) | Improvements relating to aeroplanes | |
GB191324872A (en) | Improvements in or relating to the Body or Fuselage of Aeroplanes. | |
US1939506A (en) | Aircraft construction | |
GB127029A (en) | Improvements in the Construction of the Fuselages or Framing of Aircraft. | |
GB128651A (en) | Improvements in Connection with the Fuselages of Aeronautical Machines. | |
GB123564A (en) | Improvements in or relating to the Propulsion and Control of Aeroplanes. | |
GB135836A (en) | Improvements in or relating to Fuselages of Aeroplanes. | |
GB315793A (en) | Improvements in single spar aircraft wings and damping surfaces | |
GB722857A (en) | Improvements relating to the construction of hollow bodies of streamline form | |
GB128993A (en) | Improvements in the Manufacture of the Fuselage, Wings, Struts and the like of Aircraft. | |
GB120452A (en) | Improvements in and relating to Airplane Constructions. | |
GB316247A (en) | Improvements in airplanes | |
GB130818A (en) | Improved Method of Construction of all Classes of Wood Spars used in the Construction of Aircraft. | |
GB532145A (en) | Improvements in or relating to the construction of hollow wooden structures, particularly parts of aircraft | |
GB258841A (en) | Improvements in or relating to girders, particularly those used as aircraft wings | |
GB126514A (en) | Improvements in Bodies or Fuselages for Aeroplanes and other Aircraft. | |
GB128329A (en) | An Improved Construction of Laminated Spar for Aircraft. | |
GB136426A (en) | Improvements in the Construction of Fuselages, Hulls and the like for Aircraft. | |
GB123604A (en) | Improvements in or relating to the Heels of Airships or the like. | |
GB508348A (en) | Improvements in or relating to aircraft hollow structural members |