GB191017185A - Improvements in Aeroplanes. - Google Patents
Improvements in Aeroplanes.Info
- Publication number
- GB191017185A GB191017185A GB191017185DA GB191017185A GB 191017185 A GB191017185 A GB 191017185A GB 191017185D A GB191017185D A GB 191017185DA GB 191017185 A GB191017185 A GB 191017185A
- Authority
- GB
- United Kingdom
- Prior art keywords
- booms
- pair
- struts
- pairs
- members
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Jib Cranes (AREA)
- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
Abstract
17,185. Dunne, J. W. July 19. Planes, arrangem e n t and construction o f ; framework. - To avoid collapse of an aeroplane when a boom or strut is broken by a bullet or otherwise, each boom and strut is duplicated, one member being set immediately behind the other, and the shapes and cross-sectional areas of the members are so arranged that, while the effective strength of the structure is maintained, the total weight is not materially increased. Fig. 4 shows the application to a biplane. The framework for each supporting-plane is formed with two pairs of transverse booms b, one pair, Fig. 6, near the forward edge, and the other pair, Fig. 7, slightly in advance of the trailing edge. The booms of the upper and lower planes are connected by vertical struts d, of which the members of each pair are provided at intervals with distances-pieces 3, Fig. 3. The cross-sectional shapes of the booms and struts are substantially such as would be obtained by the longitudinal severance of the usual solid members followed by a slight thickening of the parts in a fore and aft direction. The booms b may be strengthened by forming them with a curved forward edge as shown at 1, Fig. 4. The pairs of struts d may be enclosed in canvas or the like g, Fig. 3, so as to give a stream-line form to the section. In the application to a monoplane, the booms are stayed to corresponding vertical masts arranged in pairs along the inner edge of each wing.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB191017185T | 1910-07-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB191017185A true GB191017185A (en) | 1911-07-19 |
Family
ID=32638416
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB191017185D Expired GB191017185A (en) | 1910-07-19 | 1910-07-19 | Improvements in Aeroplanes. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB191017185A (en) |
-
1910
- 1910-07-19 GB GB191017185D patent/GB191017185A/en not_active Expired
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