For maximum cargo capacity, a space-efficient compact spare is carried under the rear cargo floor.
为了获得最大的货运能力,节约空间的紧凑型备胎已在后货舱地板进行。
Using this design approach, a typical civil aircraft fuselage structural design with the shape parameters of the cabin floor struts, cargo floor and foam components has been studied as design case.
采用该设计方法,以典型民机机身下部结构设计问题为算例,对客舱地板支撑结构,货舱地板和泡沫构件形状参数进行优化。
On the cabin floor, there are cargo tiedown points.
在机舱地板上安装有货物固定点。
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