GB565889A - Improved means for transporting fuselages of aeroplanes - Google Patents
Improved means for transporting fuselages of aeroplanesInfo
- Publication number
- GB565889A GB565889A GB6436/43A GB643643A GB565889A GB 565889 A GB565889 A GB 565889A GB 6436/43 A GB6436/43 A GB 6436/43A GB 643643 A GB643643 A GB 643643A GB 565889 A GB565889 A GB 565889A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuselage
- fuselages
- transporting
- aeroplanes
- allen
- 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
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/50—Handling or transporting aircraft components
Landscapes
- Engineering & Computer Science (AREA)
- Transportation (AREA)
- Manufacturing & Machinery (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
Abstract
565,889. Transporting aeroplane fuselages. ALLEN, P. J., and ALLEN & CO. (ENGINEERS), Ltd., A. H. April 21, 1943, No. 6436. [Class 108 (i)] Aeroplane fuselages are transported by the use of a wheeled structure adapted to be fitted transversely over the top of the fuselage and around its sides, detachable fastening means being provided whereby the fuselage can be suspended from and supported by the wheeled structure while lifted off the ground ; the points of suspension are near the nose of the fuselage, the rear end of which is connected to the rear of a towing vehicle to form a trailertractor combination. Fig. 1 shows an archformed wheel structure 1 comprising two frame members 3 which support the fuselage by fastening means 17 ; as shown in Fig. 2, towing means 13 are provided for transport of the unloaded structure.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB6436/43A GB565889A (en) | 1943-04-21 | 1943-04-21 | Improved means for transporting fuselages of aeroplanes |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB6436/43A GB565889A (en) | 1943-04-21 | 1943-04-21 | Improved means for transporting fuselages of aeroplanes |
Publications (1)
Publication Number | Publication Date |
---|---|
GB565889A true GB565889A (en) | 1944-12-04 |
Family
ID=9814437
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB6436/43A Expired GB565889A (en) | 1943-04-21 | 1943-04-21 | Improved means for transporting fuselages of aeroplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB565889A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2006137994A1 (en) * | 2005-06-16 | 2006-12-28 | The Boeing Company | Rotating internal support apparatus and method for large hollow structures |
WO2008088653A1 (en) * | 2007-01-12 | 2008-07-24 | The Boeing Company | Methods and systems for lifting a vehicle |
-
1943
- 1943-04-21 GB GB6436/43A patent/GB565889A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2006137994A1 (en) * | 2005-06-16 | 2006-12-28 | The Boeing Company | Rotating internal support apparatus and method for large hollow structures |
JP2008543657A (en) * | 2005-06-16 | 2008-12-04 | ザ・ボーイング・カンパニー | Rotating internal support device and method for large hollow structures |
WO2008088653A1 (en) * | 2007-01-12 | 2008-07-24 | The Boeing Company | Methods and systems for lifting a vehicle |
GB2459221A (en) * | 2007-01-12 | 2009-10-21 | Boeing Co | Methods and systems for lifting a vehicle |
GB2459221B (en) * | 2007-01-12 | 2011-06-22 | Boeing Co | Methods and systems for lifting a vehicle |
US8066252B2 (en) | 2007-01-12 | 2011-11-29 | The Boeing Company | Methods and systems for lifting a vehicle |
US8360388B1 (en) | 2007-01-12 | 2013-01-29 | The Boeing Company | Methods and systems for lifting a vehicle |
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