| 摘要 |
The invention relates to a fuselage (10) comprising a fuselage section (11) with an inner surface (12) having a non-circular contour and a spherical pressure bulkhead (13) with an outer edge (16). The outer edge (16) of the spherical pressure bulkhead (13) is attached to the inner surface (12) of the fuselage section (11) and extends along a line, which is non-circular. The line (17) is a three-dimensional curve extending parallel to the inner surface (12) of the fuselage section (11). The invention further relates to an aircraft (40) and to a method for manufacturing a fuselage (10). |
