FIELD: aircraft fuel systems.
SUBSTANCE: invention relates to aircraft fuel systems. The fuel intake device from the aircraft tank is a thin-walled shell (2) placed in the fuel tank (1) with a permeable side surface. The side surface is made of a capillary volume-porous material molded in the form of corrugations. The lower part (3) of the device is connected to the fuel intake pipeline (4). The upper part (5) is movable and sealed. A float (6) is attached to the upper part (5) of the device.
EFFECT: increased reliability of aircraft fuel system operation with a sharp increase in fuel consumption.
1 cl, 1 dwg
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|
RU2666004C1 |
