FIELD: aviation.
SUBSTANCE: invention relates to the fuel tank of the aircraft's main wing (AC). The fuel tank contains the structural unit that is using plastic reinforced with carbon fiber. Plastic includes a reinforcing material which comprises carbon fibers and a matrix that contains plastic. The structural unit is formed by laminating a conductive sheet between prepregs of plastic reinforced with carbon fiber. Moreover, carbon fiber included in reinforcing material is exposed in internal circuit in which fuel is stored on the cut surface at the end of structural unit formed by cutting off the structural unit.
EFFECT: reduction of labour intensity of production, weight reduction of aircraft structure, increase of conductivity.
6 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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| AIRBORNE VEHICLE WING AND AIRBORNE VEHICLE'S FLIGHT METHOD | 2017 |
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