Method for producing part of an aircraft fuselage and tool for implementing said method
An aircraft fuselage, a part of the technology, applied in a part of the aircraft fuselage field, can solve problems such as uncontrollable internal stress
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[0055] Figure 2A , 2B and Figure 3-5 A panel of a portion of the aircraft fuselage, referenced 30, is shown.
[0056] In the description, once assembled, the panels 30 extend over half the section of the fuselage and are semi-cylindrical with a radius of curvature in a transverse plane. Of course, the present invention is not limited to this form. Thus, the shape of the panel 30 may not be a developable surface, having a double radius of curvature.
[0057] Panel 30 includes an inner surface 30I and an outer surface 30E, and is reinforced by stringers 32 connected to inner surface 30I. The panel 30 is defined by an upper edge 30H, a lower edge 30B and side edges 31, 31'. By way of example, each side edge is arranged in a transverse plane. The upper edge 30H corresponds to a part of the upper bus bar of the fuselage. The lower edge 30B corresponds to a part of the lower bus bar of the fuselage.
[0058] According to one embodiment, the panels 30 and the stringers 32 a...
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