The invention provides a tilting propeller unmanned aerial vehicle. The tilting propeller unmanned aerial vehicle comprises a fuselage, main wings, main wing propeller thrust unit, a propeller tilting mechanism and a tail propeller thrust unit; the main wings are arranged on the two sides of the fuselage, the propeller tilting mechanism is connected to the main wings, the main wing propeller thrust unit is connected to the propeller tilting mechanism, and the tail propeller thrust unit is connected to the position, located at the tail of the fuselage, of the fuselage; and the propeller tilting mechanism comprises a shell, a driving part, a first swing arm, a connecting rod and a second swing arm, the main wing propeller thrust unit is hinged to the shell, the driving part is connected to one end of the first swing arm, the other end of the first swing arm is hinged to one end of the connecting rod, the other end of the connecting rod is hinged to the second swing arm, and the second swing arm is connected to the main wing propeller thrust unit. The tilting propeller unmanned aerial vehicle can take off and land vertically and has the advantages of being high in speed and large in load.
本发明提供了一种倾转螺旋桨无人机,该倾转螺旋桨无人机包括:机身、主翼、主翼螺旋桨推力单元、螺旋桨倾转机构和机尾螺旋桨推力单元;其中,主翼设置在机身的两侧,螺旋桨倾转机构连接于主翼,主翼螺旋桨推力单元连接于螺旋桨倾转机构,机尾螺旋桨推力单元连接于机身位于机身的尾部;其中,螺旋桨倾转机构包括壳体、驱动件、第一摆臂、连杆、第二摆臂,主翼螺旋桨推力单元铰接于壳体,驱动件连接于第一摆臂的一端,第一摆臂的另一端铰接于连杆的一端,连杆的另一端铰接于第二摆臂,第二摆臂连接于主翼螺旋桨推力单元,该倾转螺旋桨无人机能够垂直起降且具备速度快、载重大。
Tilting propeller unmanned aerial vehicle
倾转螺旋桨无人机
2021-09-14
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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