The invention provides an unmanned helicopter electrical system design method in which a power manager, a standby storage battery, a generator, a rectification module, an external power supply, a night navigation lamp, a health management system, a load, a data link communication system, a flight control system, a rudder control system and an accelerator steering engine are arranged. The unmannedhelicopter electrical system design method is a universal unmanned helicopter electrical system design method, electrical system design can be carried out according to the overall requirements, the system should work reliably in any flight state, and the average fault interval time should meet the overall requirements of an airplane.
本发明提供一种无人直升机电气系统设计方法,包括电气系统设计方法,所述电气系统设计方法包括电源管理器、备用蓄电池、发电机及整流模块、外部电源、夜航灯、健康管理系统、载荷、数据链通信系统、飞行控制系统、舵控系统和油门舵机,该无人直升机电气系统设计方法为通用型无人直升机电气系统设计方法,可以根据总体需求,进行电气系统设计,在任何飞行状态下系统均应可靠工作,平均故障间隔时间应满足飞机总体要求。
Unmanned helicopter electrical system design method
一种无人直升机电气系统设计方法
2021-03-12
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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