FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly structures for mounting components of aircraft passenger cabin internal equipment. Built-up structure for mounting components of equipment inside aircraft fuselage comprises means arranged on fuselage, suspension elements rigidly connected with said fasteners, and passing in longitudinal direction of fuselage system support coupled with suspension. Suspension elements include first suspension element and second element of suspension. Each of first suspension elements is rigidly connected with system support, and each of second suspension elements forms with system support sliding joint so that system support can slide relative to said second suspension elements along longitudinal axis of aircraft fuselage.
EFFECT: achieving considerable reduction of loads transmitted from system supports to frames in longitudinal direction, compensation of errors during manufacture, assembly, etc, and compensation of deformations of fuselage.
16 cl, 13 dwg
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