The invention relates to a supercooled large water drop icing detector capable of automatically adapting to a sideslip angle of an airplane and the airplane. The supercooled large water drop icing detector capable of automatically adapting to the sideslip angle of the aircraft comprises a probe, a weather vane structure, a transition structure, a supporting structure, a bearing and a rotating shaft, wherein a first icing sensor and a second icing sensor are arranged on the probe and are used for detecting icing conditions and distinguishing overcooled large water drop icing conditions, the weather vane structure is connected between the probe and the transition structure and is used for automatically adjusting the probe to be in the airflow direction under the action of wind power, and the transition structure is connected between the weather vane structure and the rotating shaft and is used for automatically adjusting the probe to be in the airflow direction under the action of wind power. The weather vane structure is installed on the aircraft skin and used for generating an eccentric effect so that stress of the weather vane structure can drive the rotating shaft to rotate, the supporting structure is installed on the aircraft skin and used for supporting the supercooled large water drop icing detector, and the bearing sleeve is arranged on the outer side of the rotating shaft and used for supporting and lubricating rotation of the rotating shaft.

    本发明涉及自动适应飞机侧滑角的过冷大水滴结冰探测器及飞机。该自动适应飞机侧滑角的过冷大水滴结冰探测器包括探头、风标结构、过渡结构、支撑结构、轴承和转动轴;其中,探头上布置有第一结冰传感器和第二结冰传感器,用于探测结冰条件并区分过冷大水滴结冰条件,风标结构连接在探头和过渡结构之间,用于受风力作用将探头自动调整成顺气流方向,过渡结构连接在风标结构和转动轴之间,用于产生偏心作用,以使风标结构的受力能够带动转动轴旋转,支撑结构安装至飞机蒙皮,用于支撑过冷大水滴结冰探测器,轴承套设于转动轴外侧,用于支持和润滑转动轴转动。


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    Title :

    Supercooled large water drop icing detector capable of automatically adapting to sideslip angle of airplane and airplane


    Additional title:

    自动适应飞机侧滑角的过冷大水滴结冰探测器及飞机


    Contributors:
    SHA ZHAOJUN (author) / CHEN HU (author) / CHEN NUO (author) / SHEN HAO (author) / LI ZHIMAO (author)

    Publication date :

    2024-11-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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