GB522337A - A device for the construction of aeroplanes, and composed of exchangeable individual members - Google Patents
A device for the construction of aeroplanes, and composed of exchangeable individual membersInfo
- Publication number
- GB522337A GB522337A GB599/39A GB59939A GB522337A GB 522337 A GB522337 A GB 522337A GB 599/39 A GB599/39 A GB 599/39A GB 59939 A GB59939 A GB 59939A GB 522337 A GB522337 A GB 522337A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- fitting
- connecting members
- semi
- fitting surfaces
- 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)
- Mutual Connection Of Rods And Tubes (AREA)
Abstract
522,337. Assembling aircraft structures. HENSCHEL FLUGZEUG-WERKE AKT.- GES. Jan. 7, 1939, No. 599. Convention date, Feb. 4, 1938. [Class 4] A scaffolding for use more particularly in aeroplane construction, e.g. for supporting the pattern members which reproduce the shape of the part to be constructed comprises tubes, 5, 6, 9 and connecting members 1, 3, 10 having semi-cylindrical recesses adjacent which are fitting surfaces to which can be connected either clips 4 to form cylindrical apertures to grip a tube or the fitting surfaces of other connecting members, also the connecting members may be connected to one another by other fitting surfaces. The members 3 are base members on which the scaffolding is erected and are provided with adjustable supporting surfaces 12 and rollers 13. The connecting members 1 have, on four outer surfaces semi-cylindrical recesses which on opposite surfaces are parallel and on adjacent surfaces at right angles. Two members are adapted to be bolted together the flat fitting surfaces beside the recesses fitting together. The connecting members 10 have on the opposite faces semi-cylindrical recesses at right angles to one another. A further member, Fig. 7 and 8, allows oblique positioning of the fitting surfaces to be connected and comprises a recess 2 on one side and arc-shaped slots 8 for the connecting bolts to allow angular relative positioning of the parts. A further member comprises an angle member for connecting pipes with intersecting axes.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE522337X | 1938-02-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB522337A true GB522337A (en) | 1940-06-14 |
Family
ID=6551640
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB599/39A Expired GB522337A (en) | 1938-02-04 | 1939-01-07 | A device for the construction of aeroplanes, and composed of exchangeable individual members |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB522337A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6671941B2 (en) | 1999-11-17 | 2004-01-06 | Bae Systems Plc | Method of manufacturing an aircraft assembly tool |
-
1939
- 1939-01-07 GB GB599/39A patent/GB522337A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6671941B2 (en) | 1999-11-17 | 2004-01-06 | Bae Systems Plc | Method of manufacturing an aircraft assembly tool |
EP1600379A3 (en) * | 1999-11-17 | 2005-12-14 | BAE SYSTEMS plc | Aircraft assembly rig |
US7047614B2 (en) | 1999-11-17 | 2006-05-23 | Bae Systems Plc | Aircraft assembly process |
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