According to the manned aircraft with the tilting duct, a duct motor is connected with a fuselage large arm through a fuselage small arm, a bearing large arm is arranged below the fuselage large arm, an oil-electricity converter, an emergency power battery and liquid fuel are installed in the bearing large arm, and a large two-shaft balance motor connected with a personnel riding system is installed at the lower end of the bearing large arm; a mounting fixing base used for transferring is installed below a seat where a person sits, an emergency auxiliary ejection device is installed in the seat, an emergency parachute pack is installed in a backrest of the seat, and a fire extinguisher is placed on the rear side of a protective handrail, so that the life safety of the person under the emergency condition is guaranteed. By adopting an oil-electricity converter mode, the riding feeling of personnel can be taken into consideration while the endurance time is ensured, sufficient power redundancy can ensure that the aircraft can land in a stable flight attitude when an accident occurs, and by adopting a pan-tilt-type aircraft body, the personnel can ride stably when the aircraft shakes, so that the safety of the aircraft is ensured. Meanwhile, the machine body structure adopts a foldable design, so that the storage characteristic is improved.
一种倾转涵道的载人飞行器,其中,涵道电机通过机身小臂与机身大臂连接,承重大臂设置在机身大臂下方,并在承重大臂内装有油电转换器、应急动力电池与液体燃料,承重大臂下端安装有与人员乘坐系统连接的大型两轴平衡电机,人员乘坐的座椅下方安装有用于转运的挂载固定座,并在座椅内部安装有应急辅助弹射装置、座椅靠背内安装有应急伞包、防护扶手后侧置放有灭火器,以保证应急情况下人员的生命安全;通过采取油电转化器方式,在保证续航时间的同时还能兼顾人员的乘坐感受,足够的动力冗余能够保证发生意外时飞行器能够稳定飞行姿态进行降落,采用云台式机身,保证在飞行器发生晃动时人员乘坐平稳,同时机体结构采用可折叠设计,提高收纳特性。
Manned aircraft with tilting duct
一种倾转涵道的载人飞行器
2022-07-05
Patent
Elektronische Ressource
Chinesisch
Tilting coaxial double-propeller multi-power duct manned aircraft
Europäisches Patentamt | 2021
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