FIELD: aviation.
SUBSTANCE: invention relates to aircraft fuel tanks. Housing of fuel carrying fuel tank consists of three main parts: front part, medium tight, consisting of housing front (10) and body rear (11), rear part, which is aggregate compartment (12). To provide centring of aircraft during fuel production, tank is divided into four fuel compartments by means of frame with sealed partitions. Tank housing has outer and inner shells with possibility of being located in annular space between these fuel shells, installation of pipe of pneumatic hydraulic systems and tunnel pipes for routing bundles of electric radio equipment with provision of tightness. Inner shell of tank housing is arranged with the possibility to place start-booster stage of aircraft with possibility of separation and ejection.
EFFECT: invention reduces labour intensity and increases manufacturability of manufacturing and assembly of carrying fuel tank and aircraft in general.
5 cl, 9 dwg
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