| 摘要 |
PROBLEM TO BE SOLVED: To facilitate installation of a cargo liner and various systems.SOLUTION: A fuselage portion 200 of a vehicle (e.g., an aircraft) is disclosed. The fuselage portion comprises: a frame 202; a floor beam 204 attached to the frame and including ends; a structural stanchion 206 including a first end 206A and a second end 206B; a first structural coupling 207A joining the first end of the structural stanchion and the floor beam; a second structural coupling 207B joining the second end of the structural stanchion and the frame; a non-structural stanchion 208 including a third end 208A and a fourth end 208B; a first non-structural coupling 209A joining the third end of the non-structural stanchion and the floor beam; and a second non-structural coupling 209B joining the fourth end of the non-structural stanchion and the frame.SELECTED DRAWING: Figure 1 |
