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HYPERSONIC AIRCRAFT WING IN AERODYNAMIC HEATING CONDITIONS

机译:气动加热条件下的超音速飞机机翼

摘要

FIELD: transport.SUBSTANCE: invention relates to aircraft and aerospace engineering, particularly, to hypersonic craft thermal protection. Hypersonic craft wing comprises heat emission layer 2 arranged at its surface connected via onboard electric power using circuit 7 with electrically conducting element 3. Electrically conducting element 3 is thermally connected via insulating layer 4 with channels 6 communicated with onboard thermal control system cooling line. Aforesaid heat emission layer 2 is arranged at wing outer surface nearby leading edge. Electric conductor 3 is arranged at insulating layer 6 nearby wing trailing edge.EFFECT: reduced temperature of heating, higher reliability and lower drag.2 cl, 1 dwg
机译:技术领域本发明涉及飞机和航空航天工程,尤其涉及高超音速飞行器的热防护。高超音速飞行器机翼包括放热层2,该放热层2的表面通过使用电路7的车载电力与导电元件3连接。导电元件3经由绝缘层4与通道6进行热连接,该通道6与车载热控制系统冷却管线相通。上述散热层2配置在前缘附近的机翼外表面。电导体3布置在机翼后缘附近的绝缘层6上。效果:降低加热温度,更高的可靠性和更低的阻力2 cl,1 dwg

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