| 摘要 |
The subject of the invention is an aircraft fuselage frame element (101, 102, 103) characterized in that it comprises a portion of cross member (1a, 101a, 102a) and a section of frame (1b, 101b, 102b) brought together into a single part; an assembly of aircraft fuselage frame and cross members that comprises a frame element of the invention, for which the frame element (1) connects an upper frame (5), a floor cross member (3) and a lower frame (4), and comprises a segment (1c) that replaces a floor strut; an assembly of aircraft fuselage and cross members for which the portion of cross member of the frame element (101, 102) forms a cargo cross member of the aircraft or forms a cross member for mounting the luggage bins.
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