CPC B64D 11/0023 (2013.01) [F16B 12/32 (2013.01)] | 12 Claims |
1. An aircraft cabin partition system, comprising:
at least a first partition including a partition cut-out and a first flange, the first flange including a first flange cut-out;
a first coupling assembly, the first coupling assembly configured to be inserted within the first flange cut-out, the first coupling assembly configured to be inserted within an opening of a seat rail within a floor of an aircraft cabin, the first coupling assembly configured to couple the at least the first partition to the seat rail when engaged;
at least a second partition including a second flange, the second flange including a second flange cut-out;
a second coupling assembly, the second coupling assembly configured to be inserted within the partition cut-out, the second coupling assembly configured to be inserted within the second flange cut-out, the second coupling assembly configured to couple the at least the second partition to the at least the first partition when engaged; and
a cargo box with a plurality of sides defined by the at least the first partition, the at least the second partition, and a fuselage wall.
|