GB313163A - - Google Patents

Info

Publication number
GB313163A
GB313163A GB16180/29A GB1618029A GB313163A GB 313163 A GB313163 A GB 313163A GB 16180/29 A GB16180/29 A GB 16180/29A GB 1618029 A GB1618029 A GB 1618029A GB 313163 A GB313163 A GB 313163A
Authority
GB
United Kingdom
Prior art keywords
members
templet
templets
frames
spars
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
Application number
GB16180/29A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of GB313163A publication Critical patent/GB313163A/en
Expired legal-status Critical Current

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

313,163. Junkers, K. June 8, 1028, [Convention date]. Repairing and assembling. - A jig for use in the assembly of multi-spar aeroplane wings or similar structures consists of frames 3 which are arranged to clamp on to channel rails 2 and can be set mutually parallel or in any desired coplanar position by transverse members 6, and of separate templet frames of the type shown in Fig. 3. The spars or longitudinal members 9 of the structure to be assembled are secured by clamps 8 to the frames 3 and their ends are located by clamping-devices on the templets. The templets are provided with bearing members 19 in which are formed sockets for ball ends 12 of the spars 9 which are secured by divided retaining-plates 20; these hearing members may be adjustably mounted on the templets. An adjusting rod 14 is slidably mounted in a bore formed in each bearing member at right-angles to the plane of the templet. One end of the rod is brought into contact with the ball end 12 and the other projects clear of the templet to form a sighting-mark for comparison with similar adjusting rods provided at the other adjusting points of the templet. In Fig. 2 is shown a sighting- tube 15 pivotally mounted on one of the templet members ; when adjustment of the members 9 is correct the ends of the rods 14 all lie in the plane swept by the pivoted tube 15.
GB16180/29A 1928-06-08 1929-05-25 Expired GB313163A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE313163T 1928-06-08

Publications (1)

Publication Number Publication Date
GB313163A true GB313163A (en) 1929-12-12

Family

ID=31894650

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16180/29A Expired GB313163A (en) 1928-06-08 1929-05-25

Country Status (1)

Country Link
GB (1) GB313163A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001036270A1 (en) * 1999-11-17 2001-05-25 Bae Systems Plc Aircraft assembly tool and method of manufacturing the same
CN102632469A (en) * 2012-05-08 2012-08-15 成都敏捷制造工程有限公司 Flexible jig capable of reusing components and convenient in disassembly and assembly
WO2015038041A1 (en) * 2013-09-11 2015-03-19 Saab Ab A fixture device for manufacture of aeronautical structures and a method for applying the device

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001036270A1 (en) * 1999-11-17 2001-05-25 Bae Systems Plc Aircraft assembly tool and method of manufacturing the same
US6671941B2 (en) 1999-11-17 2004-01-06 Bae Systems Plc Method of manufacturing an aircraft assembly tool
US7047614B2 (en) 1999-11-17 2006-05-23 Bae Systems Plc Aircraft assembly process
CN102632469A (en) * 2012-05-08 2012-08-15 成都敏捷制造工程有限公司 Flexible jig capable of reusing components and convenient in disassembly and assembly
WO2015038041A1 (en) * 2013-09-11 2015-03-19 Saab Ab A fixture device for manufacture of aeronautical structures and a method for applying the device
US10596683B2 (en) 2013-09-11 2020-03-24 Saab Ab Fixture device for manufacture of aeronautical structures and a method for applying the device

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