GB130425A - Improvements relating to Aircraft Framework. - Google Patents
Improvements relating to Aircraft Framework.Info
- Publication number
- GB130425A GB130425A GB312618A GB312618A GB130425A GB 130425 A GB130425 A GB 130425A GB 312618 A GB312618 A GB 312618A GB 312618 A GB312618 A GB 312618A GB 130425 A GB130425 A GB 130425A
- Authority
- GB
- United Kingdom
- Prior art keywords
- frames
- framework
- framing
- corners
- boom
- 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
- B64C35/00—Flying-boats; Seaplanes
Abstract
130,425. Flower, S. A., Hale, K. O., and Butt, E. E. W. Feb. 21, 1918. Frames and framing; floats for aerial machines. -The framework of a flying-boat consists of a central longitudinal compression boom A and polygonal transverse frames B connected to the boom by radial spokes D. The corners of the frames B are connected by longitudinal and crossed diagonal tension wires I<1>, I<2> and J<1>, J<2>. The external sheeting or plating C may be of wood or fabric, but it is preferably of metal supported between the frames B by wood fillets F pressed on the inner side by metallic tape. Skates L are supported by several of the frames B. Specification 125,398, [Class 4, Aeronautics], is referred to According to the Provisional Specification, the framing of aeroplane fuselages, flying boats, and gondolas of airships may consist of longitudinal compression members a, the corners of the framework, compression beirg induced by a central longitudinal tension member or, in the case of an airship gondola, by suspending the structure by means of bell-crank levers located at the bow and stern.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB312618A GB130425A (en) | 1918-02-21 | 1918-02-21 | Improvements relating to Aircraft Framework. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB312618A GB130425A (en) | 1918-02-21 | 1918-02-21 | Improvements relating to Aircraft Framework. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB130425A true GB130425A (en) | 1919-08-07 |
Family
ID=32341267
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB312618A Expired GB130425A (en) | 1918-02-21 | 1918-02-21 | Improvements relating to Aircraft Framework. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB130425A (en) |
-
1918
- 1918-02-21 GB GB312618A patent/GB130425A/en not_active Expired
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