The invention relates to the field of avionics systems, and discloses an avionics system of an electric aircraft, which comprises an indication recording unit, a communication unit, a navigation unit and an electric propulsion acquisition unit, and the communication unit, the navigation unit and the electric propulsion acquisition unit are electrically connected with the indication recording unit. The indication recording unit is used for displaying, recording and processing flight parameters, and the communication unit is used for communicating with other aircrafts and a ground station. The navigation unit is used for collecting attitude parameters of the airplane and external atmospheric environment parameters and automatically receiving and responding to inquiry signals of the ground station. The electric propulsion acquisition unit is used for acquiring parameters of a propulsion motor, a motor controller and a battery pack. According to the avionics system of the electric aircraft, parameters of the propulsion motor, the motor controller and the battery pack in the electric propulsion system can be collected through the electric propulsion collection unit, the collected information is integrated into the indication recording unit to be displayed, a pilot can conveniently monitor the state of the electric propulsion system, and the avionics system is suitable for the electric aircraft.
本发明涉及航电系统领域,公开了一种电动飞机的航电系统,包括指示记录单元、通信单元、导航单元和电推进采集单元,通信单元、导航单元和电推进采集单元均与指示记录单元电性连接。指示记录单元用于飞行参数的显示、记录和处理,通信单元用于与其他飞机和地面站通讯。导航单元用于采集飞机的姿态参数和外部大气环境参数,自动接收并应答地面站的询问信号。电推进采集单元用于采集推进电机、电机控制器和电池组的参数。该电动飞机的航电系统,可以通过电推进采集单元采集电推进系统中的推进电机、电机控制器和电池组的参数,并将采集到的信息整合至指示记录单元中显示,便于飞行员对电推进系统的状态进行监视,适用于电动飞机。
Avionics system of electric aircraft
一种电动飞机的航电系统
2025-01-14
Patent
Electronic Resource
Chinese
Aircraft Avionics (Digital Avionics Study)
NTIS | 1973
|Emerald Group Publishing | 1970