本发明公开了一种航空器的输能系统,涉及航空技术领域,用于实现对航空器的输能。本发明的主要技术方案为:所述系统包括:机载系统和地面能量系统;所述机载系统包括:机载接触式导电机构、机载电能单元;所述地面能量系统包括:地面接触式导电机构、地面能量单元;所述机载电能单元,用于在航空器处于滑行阶段或停止阶段,连接所述机载接触式导电机构和所述地面接触式导电机构;所述机载接触式导电机构和所述地面接触式导电机构为滑动接触;所述机载接触式导电机构,用于通过所述地面接触式导电机构获取所述地面能量单元中的电能,并将获取的电能传输至所述机载电能单元。
The invention discloses an energy transmission system of an aircraft, relates to the technical field of aviation, and is used for realizing energy transmission of the aircraft. According to the main technical scheme, the system comprises an airborne system and a ground energy system; the airborne system comprises an airborne contact type conductive mechanism and an airborne electric energy unit; the ground energy system comprises a ground contact type conductive mechanism and a ground energy unit; the airborne electric energy unit is used for connecting the airborne contact type conductive mechanism and the ground contact type conductive mechanism when the aircraft is in a taxiing stage or a stopping stage; the airborne contact type conductive mechanism and the ground contact type conductive mechanism are in sliding contact; and the airborne contact type conductive mechanism is used for acquiring the electric energy in the ground energy unit through the ground contact type conductive mechanism and transmitting the acquired electric energy to the airborne electric energy unit.
航空器的输能系统
2024-06-04
Patent
Electronic Resource
Chinese
IPC: | B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen |