GB329657A - Improvements in or relating to aircraft structures - Google Patents
Improvements in or relating to aircraft structuresInfo
- Publication number
- GB329657A GB329657A GB5811/29A GB581129A GB329657A GB 329657 A GB329657 A GB 329657A GB 5811/29 A GB5811/29 A GB 5811/29A GB 581129 A GB581129 A GB 581129A GB 329657 A GB329657 A GB 329657A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- members
- internal
- strut
- external
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Jib Cranes (AREA)
Abstract
329,657. Bristol Aeroplane Co., Ltd.. and Pollard, F. J. Feb. 21, 1929. Planes, construction of; planes connecting together and to machine.-A strut or tie for supporting an aircraft wing structure from without comprises an external part and a plurality of internal parts all engaging the external part (for example at a common point) within the structure, the free ends of the internal parts being connected to the interior of the structure at distributed points. In the example shown a, wing structure is built up of seven spars 10 each comprising an upper and lower boom spaced round the periphery of the wing. To each upper boom a member 11 is secured and these have their lower ends brought together in two groups as shown and connected to external strut members 12 and 13 which are anchored to the fuselage at 14, or, in the case of a biplane structure, to similar internal bracing members within the lower wing: the lower plane may, in turn, be similarly supported. Alternatively in a very light structure all the internal members may be grouped together and a single external strut used. Each of the internal members 11 may be secured to the wing structure at more, than one point. Specification 309,110 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5811/29A GB329657A (en) | 1929-02-21 | 1929-02-21 | Improvements in or relating to aircraft structures |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5811/29A GB329657A (en) | 1929-02-21 | 1929-02-21 | Improvements in or relating to aircraft structures |
Publications (1)
Publication Number | Publication Date |
---|---|
GB329657A true GB329657A (en) | 1930-05-21 |
Family
ID=9803041
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5811/29A Expired GB329657A (en) | 1929-02-21 | 1929-02-21 | Improvements in or relating to aircraft structures |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB329657A (en) |
-
1929
- 1929-02-21 GB GB5811/29A patent/GB329657A/en not_active Expired
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB329657A (en) | Improvements in or relating to aircraft structures | |
GB520249A (en) | Improvements in stressed-skin structures of fuselages, wings and other hollow bodies of aircraft | |
US1813814A (en) | Aircraft structure | |
US1551983A (en) | Hydroaeroplane | |
ES178645A1 (en) | IMPROVEMENTS IN AIRCRAFT CONSTRUCTION | |
GB338348A (en) | Monoplanes | |
GB329963A (en) | Improvements in and relating to fronts for furnaces | |
US1457222A (en) | Aeroplane | |
GB844519A (en) | Improvements in or relating to aircraft | |
GB300393A (en) | An improved method of bracing a framed structure such as a cantilever beam against torsional deflection | |
US1728806A (en) | Aeronautical apparatus | |
US1900631A (en) | Air brake for airplanes | |
GB329612A (en) | Improvements in aeroplane fuselage construction | |
US2308935A (en) | Aircraft wing | |
GB364534A (en) | Improvements in aircraft | |
GB305675A (en) | Improvements in and relating to supporting wings or planes for aircraft | |
GB418066A (en) | Improvements in or connected with biplane wing structures for aircraft | |
GB717194A (en) | Improvements relating to kites | |
GB339486A (en) | Improvements in the structure of monoplanes with thick wings | |
GB530561A (en) | Aeroplane landing gear | |
GB321364A (en) | Improvements in and relating to aeroplanes | |
GB742771A (en) | A maintenance platform for aircraft | |
GB575392A (en) | Improvements in airframe structures | |
GB338690A (en) | Improvements in aircraft | |
GB512407A (en) | Improvements in and relating to devices for erecting bodies such as parts of aircraft |