A hybrid aerial hydraulic drone (10) is provided comprising a fuselage (12) having a plurality of hydraulic thrusters (14) supported on an outer surface of the fuselage (12) and configured to propel the fuselage (12) in a marine environment. The drone (10) further comprises a plurality of rotor arms (18) arranged on the fuselage (12), each rotor arm (18) comprising a rotor system (22) configured to propel the fuselage (12) in an aerial environment. Each rotor arm (18) is deployably arranged between a deployed position, in which the rotor system (22) extends from the fuselage (12) for air crossing, and a folded position, in which the arm (18) is hydrodynamically folded behind the fuselage (12) for ocean crossing. The fuselage (12) further comprises a controller (26), an energy source (28), a main ballast tank (30) and a pump (32) with a breather duct (34) for operating the drone (10).
提供了一种混合式空中水力无人机(10),包括具有多个液压推进器(14)的机身(12),液压推进器支撑在机身(12)的外表面上,并被配置为在海洋环境中推进机身(12)。无人机(10)还包括布置在机身(12)上的多个旋翼臂(18),每个旋翼臂(18)包括被配置为在空中环境中推进所述机身(12)的旋翼系统(22)。每个旋翼臂(18)可展开地配置在展开位置和折叠位置之间,在展开位置中,旋翼系统(22)从机身(12)延伸以进行空中穿越,在折叠位置中,臂(18)在流体动力学上折叠在机身(12)后面以进行海洋穿越。机身(12)还包括控制器(26)、能量源(28)、主压载舱(30)和用于操作无人机(10)的具有通气管(34)的泵(32)。
Hybrid aerial hydraulic unmanned aerial vehicle
混合式空中水力无人机
22.04.2025
Patent
Elektronische Ressource
Chinesisch