The invention discloses a power supply system, the power supply system comprises a power supply, a piezoelectric patch and a control module, the power supply is used for supplying power to the operation of an aircraft, the piezoelectric patch swings in the flight process of the aircraft to generate electric energy, and the control module is used for controlling the electric energy generated by the piezoelectric patch to supply power to the operation of the aircraft. The invention also discloses a power management and control method, an aircraft and a computer readable storage medium. The invention aims to improve the cruising ability of the aircraft and avoid the problem of out-of-control flight of the aircraft caused by power failure.
本发明公开了一种电源系统,该电源系统包括电源、压电片以及控制模块,电源用于飞行器的运行供电,所述压电片在所述飞行器飞行过程中摆动产生电能,所述控制模块用于控制所述压电片产生的电能为飞行器的运行供电。本发明还公开了一种电源管控方法、飞行器以及计算机可读存储介质。本发明旨在提高飞行器的续航能力,避免飞行器由于断电造成的飞行失控问题。
Aircraft, power supply system thereof, power supply management and control method and readable storage medium
飞行器及其电源系统、电源管控方法、可读存储介质
2022-03-01
Patent
Electronic Resource
Chinese
IPC: | H02N Elektrische Maschinen, soweit nicht anderweitig vorgesehen , ELECTRIC MACHINES NOT OTHERWISE PROVIDED FOR / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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