FIELD: transport.
SUBSTANCE: invention relates to window for transport facility, particularly, for aircraft. The window consists of transparent composite material. Composite material contains fibers and matrix material so that window is capable to withstand structural loads existing in window area (carrying window). Fibers and matrix material are transparent and have the same refraction coefficient. The window is integrated into fuselage skin made of composite material as primary material. The window is made of several layers of laminate, and laminate layers of the window are overlapped by laminate layers of fuselage.
EFFECT: achievement of damage tolerance and ability to withstand all structural loads in the area of window, mass lowering.
16 cl, 5 dwg
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