GB511762A - Improvements in and relating to the construction or erection of large bodies, such as aircraft parts - Google Patents
Improvements in and relating to the construction or erection of large bodies, such as aircraft partsInfo
- Publication number
- GB511762A GB511762A GB8806/39A GB880639A GB511762A GB 511762 A GB511762 A GB 511762A GB 8806/39 A GB8806/39 A GB 8806/39A GB 880639 A GB880639 A GB 880639A GB 511762 A GB511762 A GB 511762A
- Authority
- GB
- United Kingdom
- Prior art keywords
- parts
- large bodies
- erection
- relating
- construction
- 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
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
Abstract
511,762. Tram-carriages for workshops. JUNKERS FLUGZEUG - UND - MOTORENWERKE AKT.-GES. March 20, 1939, No. 8806. Convention date, April 9, 1938. Drawings to Specification. [Class 103 (iv)] [Also in Group XXXIII] A method of constructing or erecting comparatively large bodies, e.g., aircraft fuselages and wings, includes subdividing the body into several component parts each constructed in a separate transportable erecting-device the parts subsequently being moved together so that the body can be completed. The parts may be moved by a crane or may be adapted to run on rails. In the latter case the devices are provided with adjustable feet to facilitate assembly of the body.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE511762X | 1938-04-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB511762A true GB511762A (en) | 1939-08-23 |
Family
ID=6547899
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8806/39A Expired GB511762A (en) | 1938-04-09 | 1939-03-20 | Improvements in and relating to the construction or erection of large bodies, such as aircraft parts |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB511762A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101829900A (en) * | 2010-03-30 | 2010-09-15 | 浙江大学 | Layout method of grand cross butting locator of aircraft wing body |
CN103171772A (en) * | 2013-03-11 | 2013-06-26 | 浙江大学 | System and layout method for airframe three-section involution and intersection hole machining |
-
1939
- 1939-03-20 GB GB8806/39A patent/GB511762A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101829900A (en) * | 2010-03-30 | 2010-09-15 | 浙江大学 | Layout method of grand cross butting locator of aircraft wing body |
CN101829900B (en) * | 2010-03-30 | 2012-11-28 | 浙江大学 | Layout method of grand cross butting locator of aircraft wing body |
CN103171772A (en) * | 2013-03-11 | 2013-06-26 | 浙江大学 | System and layout method for airframe three-section involution and intersection hole machining |
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