-
公开(公告)号：US20170297733A1
公开(公告)日：2017-10-19
申请号：US15278309
申请日：2016-09-28
发明人： Guocheng ZHAO , Wei LUO , Pengcheng QI
CPC分类号： B64D33/02 , B64C27/82 , B64C39/024 , B64C2201/024 , B64C2201/044 , B64C2201/141 , B64C2201/146 , B64D27/08 , B64D33/06 , B64D33/08 , B64D2033/0246 , B64D2033/028
摘要： The present invention discloses an unmanned helicopter, and belongs to the technical field of unmanned aerial vehicles. The unmanned helicopter includes an air inlet system, an exhaust system, a cooling system and a dynamic balance system. The air inlet system is fixed on a second side; the exhaust system is fixed on a third side; and the cooling system is fixed on a first side, and the dynamic balance system is fixed on a tail. The airflow at the outside of the unmanned helicopter flows into the air inlet system smoothly, quickly and efficiently under the action of its own flow velocity relative to the unmanned helicopter, therefore the technical problem in the prior art that the air entering the fuselage with a unit volume is burnt insufficiently, which generates adverse effects on the normal flight of the unmanned helicopter, is solved.
-
公开(公告)号：US20180030887A1
公开(公告)日：2018-02-01
申请号：US15661600
申请日：2017-07-27
发明人： Guocheng ZHAO , Wei LUO , Pengcheng QI
IPC分类号： F02B61/04 , B64C27/14 , F02B73/00 , F16H7/02 , F02B75/16 , F16H37/06 , F16H1/22 , B64C39/02 , F02B67/06
CPC分类号： F02B61/04 , B64C27/08 , B64C27/12 , B64C27/14 , B64C27/59 , B64C39/024 , B64C2201/027 , B64C2201/044 , B64C2201/108 , B64D35/04 , F02B67/06 , F02B73/00 , F02B75/16 , F16H1/222 , F16H7/02 , F16H37/065
摘要： The present invention discloses a multi-shaft power source unmanned flight equipment, and belongs to the technical field of unmanned aerial vehicles. The multi-shaft power source unmanned flight equipment comprises a frame (1), a plurality of rotor sets (2) and a power device (3). The plurality of rotor sets (2) are rotatably fixed on the frame (1), and the power device (3) is correspondingly movably connected with each rotor set (2) respectively. Power is provided for flight of the unmanned flight equipment by the power device (3) with oil drive characteristics, mechanical kinetic energy is generated by burning a combustion material pre-injected in the power device (3), and rotors (21) in each rotor set (2) correspondingly connected with the power device are driven to rotate, thereby replacing the traditional electric multi-rotor unmanned aerial vehicle structure adopting electric modes such as batteries, electronic speed controllers and the like to supply power and provide power for the rotation of the rotors (21); and the unmanned flight equipment has the characteristics of long duration and strong loading capacity.
-
搜索结果
2 条记录 (耗时 0.016 秒)
