FIELD: transport.
SUBSTANCE: invention relates to aircraft cladding. Cladding for aircraft fuselage bay contains multiple mutually adjacent cladding panels. Between fuselage bay and cladding, interspace is provided. Cladding panel has such connection (going through interspace) with fuselage bay that in case of sudden pressure drop between fuselage bay internal space and interspace gap opening is provided to balance pressure.
EFFECT: lower weight of aircraft bay cladding.
11 cl, 7 dwg
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