Graphene composite material helicopter rotor anti-icing and deicing device and manufacturing method

Abstract

The invention discloses a graphene composite material helicopter rotor anti-icing and deicing device and a manufacturing method; the graphene composite material helicopter rotor anti-icing and deicingdevice comprises a skin, an insulation heat transfer layer, a heating layer and an insulation heat insulation layer, and the skin, the insulation heat transfer layer, the heating layer and the insulation heat insulation layer are sequentially arranged from outside to inside along the chordwise direction; the skin, the insulation heat transfer layer, the heating layer and the insulation heat insulation layer are attached to form an outer edge body, the outer edge body is integrally heated and cured into a rotor front edge shape, and the outer edge body is installed on the rotor base body. Theheating layer comprises a plurality of bent linear heating components, and the bent linear heating components can cover the front edge of the heating rotor. By adopting the heating components and theheat transfer and insulation parts which are specially arranged, the heating efficiency of the rotor is improved, and the deicing efficiency of the rotor is favorably improved.

Description

technical field [0001] The invention relates to the field of rotor deicing, in particular to a rotor base anti-icing device and a manufacturing method using graphene-doped composite materials. Background technique [0002] Icing has always been a major threat to helicopter flight safety. When the helicopter encounters severe flight conditions such as low temperature, rain and snow, if the liquid water content in the air is high, key components such as the rotor base are at risk of freezing. Ice accumulation on the rotor will change the aerodynamic shape of the rotor, resulting in reduced flight performance, reduced lift, increased drag, and increased fuel consumption. At the same time, it will destroy the balance of the rotor and cause vibration, which is very dangerous for helicopters. Specifically, the lift coefficient of the airfoil decreases and the drag coefficient increases after icing. Ice accumulation destroys the aerodynamic shape of the rotor surface, which in tu...

AI Technical Summary

Problems solved by technology

[0005] Aiming at the shortcomings of the existing rotor bases that are easy to freeze and difficult to de-ice, the present invention aims to propose a rotor base anti-icing device using graphene-doped composite materials, using specially arranged heating components and heat transfer, heat insulation Components, realize the improvement of the heating efficiency of the rotor, which is beneficial to improve the deicing efficiency of the rotor

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