(19)
(11)EP 2 530 021 A3

(12)EUROPEAN PATENT APPLICATION

(88)Date of publication A3:
17.12.2014 Bulletin 2014/51

(43)Date of publication A2:
05.12.2012 Bulletin 2012/49

(21)Application number: 12170183.3

(22)Date of filing:  31.05.2012
(51)International Patent Classification (IPC): 
B64F 5/00(2006.01)
(84)Designated Contracting States:
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
Designated Extension States:
BA ME

(30)Priority: 31.05.2011 DE 102011076841
31.05.2011 US 201161491346 P

(71)Applicant: Airbus Operations GmbH
21129 Hamburg (DE)

(72)Inventors:
  • Roschat, Bernd
    21129 Hamburg (DE)
  • Halfmann, Niklas
    21073 Hamburg (DE)
  • Krause, Dieter
    21073 Hamburg (DE)

(74)Representative: Marschall, Stefan 
Elbpatent Marschall und Partner Bavariaring 26
80336 München
80336 München (DE)

  


(54)Assembling jig for at least one section of an aircraft fuselage


(57) Disclosed is a jig (1) for the modelling of at least one section of an aircraft fuselage (2), with a framework structure (4) and with a multiplicity of adapters (48) for the connection of stiffening elements (30) to the framework structure (4), which can be moved relative to the framework structure (4), and/or with a multiplicity of adapters (68) for the modelling of profiles of stiffening elements (30), which can be moved relative to the framework structure (4).







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