| 摘要 |
The invention relates to a wing-fuselage structural component (B) for the connection of two airfoils (F1, F2) and a fuselage section (3) of an air aircraft, having: a first wing shell part (11) for the first wing (F1) and a second wing shell part (12) for the second wing, each of which is produced in one part and formed from a shell part (11 a, 12a) on the wing side and a shell part (11 b, 12b) on the fuselage side, wherein each shell part (11 b, 12b) on the fuselage side has connecting parts (31, 32, 33; 41, 42) and recesses (34, 35; 43, 44, 45) in each case between the connecting parts, wherein the connecting parts and the recesses of the shell part (11 b, 12b) on the fuselage side for the first wing (F1) and of the shell part (11 b, 12b) on the fuselage side for the second wing (F2) interlock in the assembled state and wherein at least two connecting parts (31, 32, 33; 41, 42), on their shell part (11a, 12a) on the wing side, have an elongation part (31 a, 32a, 33a; 41a, 42a), a partially cylindrical fuselage shell part (30), the supporting edges (51, 52) of which have recesses (51 a, 51 b), with which the elongation paths of the wing shell parts (12) interlock. |
