Metal working – Method of mechanical manufacture – Structural member making
Reexamination Certificate
2011-06-28
2011-06-28
Hong, John C (Department: 3726)
Metal working
Method of mechanical manufacture
Structural member making
C029S281100
Reexamination Certificate
active
07966729
ABSTRACT:
The invention relates to a method for the economic production of entire fuselage cells of airplanes and to a site for carrying out the method. Differing from the conventional sectional assembly according to the invention separate shells (shell components) are attached to a substantially completed cockpit section and/or rear section. At this the half shell construction and the four shell construction as well as a combination hereof can be applied. Alternatively, the cockpit section and the rear section as well as the central wing box section can be aligned and positioned to each other in a site forming gaps in longitudinal direction. Subsequently, the shell components as well as the floor framework sections are adjusted circularly revolving between the sections and are ideally simultaneously connected to these by means of at least four cross-seams and a plurality of longitudinal seams.
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International Search Report with Written Opinion from PCT/EP2008/057850 dated Jan. 29, 2009.
Frauen Holger
Gnauck Tomas
Klemkow Eike
Airbus Operations GmbH
Hong John C
Jenkins Wilson Taylor & Hunt, P.A.
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