| 摘要 |
A fuselage portion 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 comprising ends; a structural stanchion (206) comprising a first end and a second end; 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) comprising a third end and a fourth end; 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. |
