The invention provides a novel amphibious aircraft and a control method, and belongs to the field of aircrafts. The aircraft comprises an H-shaped rack, and a fuselage, a flight control module, a water surface navigation control module, a buoy module, a load module and a control module which are carried on the H-shaped rack; the flight control module can generate lift force and pull force; the water surface navigation control module can generate thrust in the navigation direction; the buoy module comprises two flat streamline buoys which are symmetrically arranged; the load module is used for carrying different devices; the control module is arranged in the fuselage and used for controlling action execution of the flight control module and the water surface navigation control module and execution control of flight tasks. According to the amphibious aircraft, the defects that most amphibious aircrafts are high in dependence on take-off and landing sites, poor in loading capacity and single in executable task at present are overcome; and meanwhile, the defects of low efficiency and high energy consumption of an amphibious aircraft which generates water surface navigation or underwater sneaking power through rotor wings are overcome.
本发明提供一种新型水陆两栖飞行器及控制方法,属于飞行器领域;飞行器包括H型机架及搭载于其上的机身、飞行控制模块、水面航行控制模块、浮筒模块、载荷模块及控制模块;所述飞行控制模块能够产生升力和拉力;所述水面航行控制模块能够产生航行方向的推力;所述浮筒模块包括对称设置的两个扁平流线型浮筒;所述载荷模块用于搭载不同的设备;所述控制模块置于机身内,用于控制飞行控制模块、水面航行控制模块的动作执行,及飞行任务的执行控制。本发明解决了目前大部分水陆两栖飞行器对起降场地的依赖性强、载荷能力差、可执行任务单一的缺点;同时解决了通过旋翼产生水面航行或者水下潜行动力的两栖飞行器效率低、能量消耗大的缺点。
Novel amphibious aircraft and control method
一种新型水陆两栖飞行器及控制方法
2024-03-19
Patent
Electronic Resource
Chinese