GB238213A - An improved method of and means for constructing elongated hollow bodies such as thebodies of aircraft - Google Patents

An improved method of and means for constructing elongated hollow bodies such as thebodies of aircraft

Info

Publication number
GB238213A
GB238213A GB18810/25A GB1881025A GB238213A GB 238213 A GB238213 A GB 238213A GB 18810/25 A GB18810/25 A GB 18810/25A GB 1881025 A GB1881025 A GB 1881025A GB 238213 A GB238213 A GB 238213A
Authority
GB
United Kingdom
Prior art keywords
girder
hollow bodies
aircraft
thebodies
improved method
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
GB18810/25A
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 GB238213A publication Critical patent/GB238213A/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)
  • Excavating Of Shafts Or Tunnels (AREA)

Abstract

238,213. Junkers, H. Aug. 8, 1924, [Convention date]. Benches, work.-For constructing hollow bodies such as the rear ends of aircraft fuselages, a rectangular girder 1 is pivotally mounted at its ends in trestles 3 and has adjustable members 4 for supporting the transverse frame members 6 of the body in their correct positions, the completed body being ultimately withdrawn from the girder without dismantling the latter. The girder may be rotated to give access to all parts as the longitudinals 7 and corrugated covering 10 are secured in position or it may be locked against rotation by a pin 9. The front part of the fuselage is constructed in an external cradle 11, Fig. 3, having push bolts 12 for holding the transverse frames 13 and longitudinals 14 in position, the covering being applied after removal from the cradle. The two parts of the fuselage are subsequently connected together.
GB18810/25A 1924-08-08 1925-07-23 An improved method of and means for constructing elongated hollow bodies such as thebodies of aircraft Expired GB238213A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE238213X 1924-08-08

Publications (1)

Publication Number Publication Date
GB238213A true GB238213A (en) 1926-10-07

Family

ID=5903478

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18810/25A Expired GB238213A (en) 1924-08-08 1925-07-23 An improved method of and means for constructing elongated hollow bodies such as thebodies of aircraft

Country Status (1)

Country Link
GB (1) GB238213A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2251270A1 (en) * 2002-11-21 2006-04-16 Manuel Torres Martinez Assembly system for fuselage of aircraft has pairs of semi-structures arranged such that second semi-structure of each pair of semi-structures is placed over first semi-structure that has been inverted

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2251270A1 (en) * 2002-11-21 2006-04-16 Manuel Torres Martinez Assembly system for fuselage of aircraft has pairs of semi-structures arranged such that second semi-structure of each pair of semi-structures is placed over first semi-structure that has been inverted

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