Aircraft, avionics systems, and methods for predicting a wake turbulence generated by an advancing aircraft are provided. In one example, an aircraft includes a fuselage having a cockpit area and an avionics system interfacing with the cockpit area. The avionics system is configured to receive a plurality of data signals. The data signals include ADS-B IN data signals from an advancing aircraft. The avionics system is operative to predict a wake turbulence generated by the advancing aircraft in response to at least one of the data signals, thereby defining a predicted wake turbulence.
提供了用于预测由行进飞机产生的尾迹湍流的飞机、航空电子系统以及方法。在一个示例中,一种飞机包括具有驾驶舱区域的机身和与该驾驶舱区域相接的航空电子系统。该航空电子系统被配置为接收多个数据信号。该数据信号包括来自行进飞机的ADS‑B IN数据信号。该航空电子系统可操作以响应于数据信号中的至少一个来预测由该行进飞机产生的尾迹湍流,从而限定预测的尾迹湍流。
PREDICTING WAKE TURBULENCE OF ADVANCING AIRCRAFT
预测行进飞机的尾迹湍流
2020-11-13
Patent
Elektronische Ressource
Chinesisch