GB264546A - Flying machines and process of making same - Google Patents
Flying machines and process of making sameInfo
- Publication number
- GB264546A GB264546A GB1898325A GB1898325A GB264546A GB 264546 A GB264546 A GB 264546A GB 1898325 A GB1898325 A GB 1898325A GB 1898325 A GB1898325 A GB 1898325A GB 264546 A GB264546 A GB 264546A
- Authority
- GB
- United Kingdom
- Prior art keywords
- framework
- members
- longerons
- wings
- class
- 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
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Road Paving Structures (AREA)
Abstract
264,546. Strauss, J. B. July 25, 1925. Fuselages; planes and the like; construction of. -The surface-covering for the bodies and wings of aircraft is composed of a metallic mesh the interstices of which are filled with a concrete composition, such as a mixture of cement and porous stone-like material, or mineralized sawdust, applied in a plastic state. Fig. 1 shows an aeroplane the fuselage of which is constructed of a skeleton framework comprising aluminium longerons 2 and bracing members 1, covered with a metal mesh 3 which is secured to the framework members and treated in the above manner. The wings also may be composed of a framework, comprising longerons, ribs, and bounding members, which is covered by upper and lower mesh surfaces connected at the edges, and then treated with the plastic composition. Reference has been directed by the Comptroller to Specifications 12514/10; 2341/14, [Class 108 (i), Road vehicles, Body details &c. of], 125,655, and 142,082; 147,613 and 202,129, [both in Class 108 (i), Road vehicles, Body details &c. of].
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1898325A GB264546A (en) | 1925-07-25 | 1925-07-25 | Flying machines and process of making same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1898325A GB264546A (en) | 1925-07-25 | 1925-07-25 | Flying machines and process of making same |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB264546A true GB264546A (en) | 1927-01-25 |
Family
ID=10121766
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1898325A Expired GB264546A (en) | 1925-07-25 | 1925-07-25 | Flying machines and process of making same |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB264546A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2455838A (en) * | 1944-06-19 | 1948-12-07 | Vickers Armstrongs Ltd | Air frame structure |
| FR2653090A1 (en) * | 1989-10-17 | 1991-04-19 | Mitsubishi Heavy Ind Ltd | Interior doubling plate for a fuselage wall |
-
1925
- 1925-07-25 GB GB1898325A patent/GB264546A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2455838A (en) * | 1944-06-19 | 1948-12-07 | Vickers Armstrongs Ltd | Air frame structure |
| FR2653090A1 (en) * | 1989-10-17 | 1991-04-19 | Mitsubishi Heavy Ind Ltd | Interior doubling plate for a fuselage wall |
| US5165627A (en) * | 1989-10-17 | 1992-11-24 | Mitsubishi Jukogyo Kabushiki Kaisha | Fuselage wall inner lining plate |
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