Patent ID: 9038686
Filing Date: 2015-05-26
Classification: B29C,B29D,B64C,Y02T

Abstract:
1. A positioning system configured to operate with sectors of a device ( 2 ) for producing an airplane fuselage in which a lamination mandrel ( 4 ) is defined by an external surface ( 5 ) which defines a rotation solid with respect to a symmetry axis ( 7 ); said lamination mandrel ( 4 ) is adapted to receive and support a band of impregnated synthetic material which is deposited and wound on the external surface ( 5 ) forming a plurality of overlapping layers which are subjected to a high temperature polymerisation process under vacuum for forming a structural section of the airplane; the lamination mandrel ( each guide ( characterised by comprising a positioning device (P) arranged between a portion of each mobile part ( the position of said central body (