FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to fasteners of airliner cabin internal equipment, and to airliner equipped with structure of said fasteners. Proposed structure 9 comprises airframe elements 5 spaced apart by first interval in lengthwise direction of fuselage, system support 1 running under cabin floor 12 along first interval between airframe two elements 5. Besides, said structure includes suspension device 2 arranged in plane formed by airframe elements 5. Note here that suspension device 2 is attached so that its free end runs along passenger cabin. System support 1 is attached to free end of suspension device 2. Note here that system support 1 has multiple fastening elements equally space apart by second interval to secure internal equipment components 9.
EFFECT: flexible system of equipment fastening.
11 cl, 6 dwg
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Authors
Dates
2011-11-10—Published
2006-11-16—Filed