The invention discloses an aircraft icing early warning method and system, electronic equipment and a storage medium. The method comprises the following steps: acquiring current flight parameters of an aircraft; acquiring the total temperature of the surface of the aircraft body corresponding to the current flight parameter from a mapping relation between a pre-stored flight parameter and the total temperature; responding to the situation that the total surface temperature of the aircraft body is smaller than or equal to the critical total temperature, and carrying out aircraft icing early warning. The possibility of false alarm of the icing detector can be reduced, and the starting frequency of the anti-icing system is reduced. And additional sensors are not required to be mounted or the airplane is not required to be designed again, so that early warning of icing on the surface of the airplane is simply and efficiently completed.
本发明公开了一种飞机结冰预警方法、系统、电子设备以及存储介质,方法包括:获取飞机的当前飞行参数;从预先存储的飞行参数与总温之间的映射关系中,获取与所述当前飞行参数对应的机体表面总温;响应于所述机体表面总温小于等于临界总温,进行飞机结冰预警。本发明能够降低结冰探测器误报的可能性,降低防冰系统的开启频次。也不需要安装额外的传感器或者重新对飞机进行设计,简单高效地完成对飞机表面结冰的预警。
Aircraft icing early warning method and system, electronic equipment and storage medium
一种飞机结冰预警方法、系统、电子设备以及存储介质
2024-03-05
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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