The aramid honeycomb sandwich panel is composed of a panel, an aramid honeycomb core and an adhesive. The panel provides the axial bending and in-plane shear stiffness required by the component, mainly glass fiber, carbon fiber, aluminum and other materials. The aramid honeycomb core carries the load and transverse shear of the component from one panel to the other. Aramid honeycomb sandwich structure is an advanced structure which can be applied in the field of aerospace. It is widely used in modern aircraft, especially in large composite aircraft, the main application parts include aircraft flaps, ailerons, vertical tail leading edge, rudder, canard, fuselage, blades, radome, radome, panel, cabin door, floor and other components, and the large rigid, secondary force components of the aircraft. As the preferred composite material of aircraft parts, aramid honeycomb sandwich structure can reduce the structural weight of aircraft, realize the wave transmission, noise reduction and thermal insulation performance of functional components.
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