GB515562A - Improvements in or relating to the structure of aircraft - Google Patents
Improvements in or relating to the structure of aircraftInfo
- Publication number
- GB515562A GB515562A GB19560/38A GB1956038A GB515562A GB 515562 A GB515562 A GB 515562A GB 19560/38 A GB19560/38 A GB 19560/38A GB 1956038 A GB1956038 A GB 1956038A GB 515562 A GB515562 A GB 515562A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- fuselage
- twin
- wing
- securing means
- 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)
- Tires In General (AREA)
Abstract
515,562. Aeroplanes. FAIREY AVIATION CO., Ltd., and LOBELLE, M. J. O. July 1, 1938, No. 19560. [Class 4] In an aircraft having detachable wings and in ' which a wing may be secured directly to the fuselage by standard securing means, the aircraft is convertible into a twin fuselage aircraft by the provision of an auxiliary fuselage and centre sections for the main and tail planes adapted to be secured between and directly to the fuselage by standard securing means. Fig. 7, shows respectively a component consisting of a wing section 14 and nacelle 15. Further components include a wing section 16, and a tail plane centre section 17. A twin-fuselage aircraft, Fig. 1, comprising components 16 and 17, may be converted to a four-engined craft by the addition of the components shown in Fig. 7, tail planes being added.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB19560/38A GB515562A (en) | 1938-07-01 | 1938-07-01 | Improvements in or relating to the structure of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB19560/38A GB515562A (en) | 1938-07-01 | 1938-07-01 | Improvements in or relating to the structure of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB515562A true GB515562A (en) | 1939-12-07 |
Family
ID=10131406
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB19560/38A Expired GB515562A (en) | 1938-07-01 | 1938-07-01 | Improvements in or relating to the structure of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB515562A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2496087A (en) * | 1944-09-23 | 1950-01-31 | Fleming Jacob Waggoner Partee | Aerial train |
| DE1068119B (en) * | 1959-10-29 | |||
| WO1986003172A1 (en) * | 1984-11-23 | 1986-06-05 | Fox Brothers Limited Partnership | Graduated aircraft design and construction method |
| WO1987003265A1 (en) * | 1985-11-22 | 1987-06-04 | Fox Brothers Limited Partnership | Graduated aircraft design and construction method |
| GB2328918A (en) * | 1997-09-04 | 1999-03-10 | British Aerospace | Selecting modules to produce aircraft variants |
| GB2403462A (en) * | 2003-06-24 | 2005-01-05 | John Edward Randell | A fixed-wing twin-body aircraft and a land vehicle |
| CN111017185A (en) * | 2019-12-19 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | Laminar flow technology verification machine |
-
1938
- 1938-07-01 GB GB19560/38A patent/GB515562A/en not_active Expired
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1068119B (en) * | 1959-10-29 | |||
| US2496087A (en) * | 1944-09-23 | 1950-01-31 | Fleming Jacob Waggoner Partee | Aerial train |
| WO1986003172A1 (en) * | 1984-11-23 | 1986-06-05 | Fox Brothers Limited Partnership | Graduated aircraft design and construction method |
| WO1987003265A1 (en) * | 1985-11-22 | 1987-06-04 | Fox Brothers Limited Partnership | Graduated aircraft design and construction method |
| GB2328918A (en) * | 1997-09-04 | 1999-03-10 | British Aerospace | Selecting modules to produce aircraft variants |
| US6065720A (en) * | 1997-09-04 | 2000-05-23 | British Aerospace Public Limited Company | Manufacture of aircraft |
| GB2403462A (en) * | 2003-06-24 | 2005-01-05 | John Edward Randell | A fixed-wing twin-body aircraft and a land vehicle |
| GB2403462B (en) * | 2003-06-24 | 2007-07-04 | John Edward Randell | A land vehicle |
| CN111017185A (en) * | 2019-12-19 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | Laminar flow technology verification machine |
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