The invention provides an aircraft and an icing probe, an icing detector and an icing alarm method thereof, and the icing probe comprises a main body which is in a bullet shape and comprises a head part and a tail part; the two side wings are respectively arranged on two sides of the main body and are connected with the tail part; the first sensor is arranged on one side, deviating from the tail, of the head of the main body; the second sensor is arranged on the side, facing the head, of the side wing; the icing detector comprises a shell, the icing probe and an angle adjusting mechanism, the angle adjusting mechanism comprises an attack angle adjusting mechanism and a sideslip angle adjusting mechanism, the attack angle adjusting mechanism drives the icing probe to rotate in a first plane, and the sideslip angle adjusting mechanism drives the icing probe to rotate in a second plane; the aircraft comprises the icing detector. The icing alarm method adopts the icing detector. According to the aircraft and the icing probe, the icing detector and the icing alarm method thereof, the recognition and monitoring capability of large supercooled water drops can be improved.
本发明提供了一种飞行器及其结冰探头、结冰探测器和结冰告警方法,所述结冰探头包括:主体,呈弹头形状,所述主体包括头部和尾部;两个侧翼,分别设于主体上的两侧,且均与尾部连接;第一传感器,设于主体的头部上背离尾部的一侧;第二传感器,设于侧翼上朝向头部的一侧;所述结冰探测器包括壳体、上述的结冰探头以及角度调节机构,角度调节机构包括攻角调节机构和侧滑角调节机构,攻角调节机构驱动结冰探头在第一平面内转动,侧滑角调节机构驱动结冰探头在第二平面内转动;所述飞行器包括上述的结冰探测器;所述结冰告警方法采用上述的结冰探测器。本发明提供的飞行器及其结冰探头、结冰探测器和结冰告警方法能够提高对于过冷大水滴的识别监测能力。
Aircraft and icing probe, icing detector and icing alarm method thereof
飞行器及其结冰探头、结冰探测器和结冰告警方法
2023-08-08
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Icing detector probe and icing detector with the same
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|Europäisches Patentamt | 2021
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