GB249463A - Improvements in and relating to scaffold frames for use in aircraft construction - Google Patents
Improvements in and relating to scaffold frames for use in aircraft constructionInfo
- Publication number
- GB249463A GB249463A GB18812/25A GB1881225A GB249463A GB 249463 A GB249463 A GB 249463A GB 18812/25 A GB18812/25 A GB 18812/25A GB 1881225 A GB1881225 A GB 1881225A GB 249463 A GB249463 A GB 249463A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wings
- aircraft
- fuselage
- templates
- template
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Jib Cranes (AREA)
Abstract
249,463. Junkers, H. March 17, 1925, [Convention date]. Addition to 238,208. Benches, work. - For enabling the scaffold or construction frames described in the parent Specification to be readily transported on an aeroplane to the place where a damaged machine may be situated, the frames are formed with air-cutting or streamline surfaces so that they can be fitted to an aircraft without undue interference with its flying capacity. Fig. 3 shows a wing-template 3 supported on jacks while a damaged aircraft is being repaired, the edges of the template being streamlined to enable it to be carried in a horizontal position beneath the wings of a transporting aircraft. Alternatively, streamlined templates may be secured to the sides of the fuselage and to the upper surface of the wings. Fig 9 shows wing templates 16 and a body template 17 temporarily inserted in the wings and fuselage of a transporting aeroplane, the connections between the parts of the wings and fuselage being lengthened for this purpose. Sighting devices are provided on the templates to facilitate adjustment on the damaged machine.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE249463X | 1925-03-17 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB249463A true GB249463A (en) | 1926-07-15 |
Family
ID=5935757
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB18812/25A Expired GB249463A (en) | 1925-03-17 | 1925-07-23 | Improvements in and relating to scaffold frames for use in aircraft construction |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB249463A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4161299A (en) * | 1978-04-20 | 1979-07-17 | Smisson Leonard F | Aircraft performance data qualifier |
| WO2010104972A3 (en) * | 2009-03-13 | 2011-03-03 | The Boeing Company | Automated wing painting system |
| US8455054B2 (en) | 2009-03-13 | 2013-06-04 | The Boeing Company | Automated wing painting system |
| CN105151318A (en) * | 2015-09-28 | 2015-12-16 | 山东太古飞机工程有限公司 | Auxiliary bracket for airplane wing installation |
-
1925
- 1925-07-23 GB GB18812/25A patent/GB249463A/en not_active Expired
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4161299A (en) * | 1978-04-20 | 1979-07-17 | Smisson Leonard F | Aircraft performance data qualifier |
| WO2010104972A3 (en) * | 2009-03-13 | 2011-03-03 | The Boeing Company | Automated wing painting system |
| US8088450B2 (en) | 2009-03-13 | 2012-01-03 | The Boeing Company | Automated wing painting system |
| US8455054B2 (en) | 2009-03-13 | 2013-06-04 | The Boeing Company | Automated wing painting system |
| CN105151318A (en) * | 2015-09-28 | 2015-12-16 | 山东太古飞机工程有限公司 | Auxiliary bracket for airplane wing installation |
| CN105151318B (en) * | 2015-09-28 | 2017-03-29 | 山东太古飞机工程有限公司 | Aircraft wing installs auxiliary bracket |
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