GB300267A - Improvements in supporting structures for aeroplanes - Google Patents
Improvements in supporting structures for aeroplanesInfo
- Publication number
- GB300267A GB300267A GB30716/28A GB3071628A GB300267A GB 300267 A GB300267 A GB 300267A GB 30716/28 A GB30716/28 A GB 30716/28A GB 3071628 A GB3071628 A GB 3071628A GB 300267 A GB300267 A GB 300267A
- Authority
- GB
- United Kingdom
- Prior art keywords
- struts
- springs
- arrangement
- planes
- lower beam
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Dampers (AREA)
Abstract
300,267. Soc. Anon. des Ateliers d'Aviation L. Breguet. Nov. 10, 1927, [Convention date]. Planes, arrangement of; propelling; balancing; shock-absorbers, application of; land wheels; floats, arrangement of.-Large aeroplanes have a central structure 1 rigidly connected to a lower beam which may form part of the frame of the fuselage 4, and wings 7 are pivoted to or rigidly secured to the ends of the structure 1 and are stayed by struts 9, 13<a> and 11 to the ends of the lower beam. The struts 13<a> which may be pivoted or fixed to the lower beam may be faired to form small planes. Engines 14 may be carried at the ends of the structure 1 and floats or wheels at the ends of the struts 13a. Springs and dampers may be inserted in the struts 9 to allow the planes to give under stress. A modification is described in which springs are inserted in inclined struts connecting the wings, midway of their length to the beam at the lower edge of the fuselage. Fig. 6 shows an arrangement of struts and springs when a landing wheel is mounted at the point 10.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR300267X | 1927-11-10 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB300267A true GB300267A (en) | 1929-11-28 |
Family
ID=8888445
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB30716/28A Expired GB300267A (en) | 1927-11-10 | 1928-10-23 | Improvements in supporting structures for aeroplanes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB300267A (en) |
-
1928
- 1928-10-23 GB GB30716/28A patent/GB300267A/en not_active Expired
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