公开(公告)号：US08561937B2

公开(公告)日：2013-10-22

申请号：US12906096

申请日：2010-10-17

Applicant: Hosein Goodarzi

Inventor： Hosein Goodarzi

IPC: B64C27/00 ,  B64C29/00

CPC classification number: B64C39/024 ,  B64C39/064 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/146

Abstract: The various embodiments of the present invention provide an unmanned aerial vehicle comprising a hemispherical body, a brushless type electrical, a propeller, a plurality of wingtip devices, a plurality of servo motors and each of the plurality of the servo motors is connected to each of the plurality of the wingtip devices respectively, a plurality of carbon rods, and a casing. The brushless type electrical motor provides a lifting force for a vertical take-off and landing (VTOL) and the plurality of wing tip devices are classified into three types of wing tip devices and the three types of wing tip devices are controlled by the respective servo motors to control yaw, pitch and roll movements thereby stabilizing and controlling the movement of an aircraft.

Abstract translation: 本发明的各种实施例提供一种无人驾驶飞行器，其包括半球体，无刷电，螺旋桨，多个翼尖装置，多个伺服马达，多个伺服马达中的每一个连接到 多个翼尖装置，多个碳棒，以及壳体。 无刷式电动机为垂直起降提供提升力（VTOL），并且多个翼尖装置分为三种类型的翼尖装置，三种类型的翼尖装置由相应的伺服机构 用于控制偏航，俯仰和滚动运动的电机，从而稳定和控制飞行器的运动。

公开(公告)号：US20120091284A1

公开(公告)日：2012-04-19

申请号：US12906096

申请日：2010-10-17

Applicant: Hosein Goodarzi

Inventor： Hosein Goodarzi

IPC: B64C29/00 ,  G01C21/00 ,  G05D1/00

CPC classification number: B64C39/024 ,  B64C39/064 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/146

Abstract: The various embodiments of the present invention provide an unmanned aerial vehicle comprising a hemispherical body, a brushless type electrical, a propeller, a plurality of wingtip devices, a plurality of servomotors and each of the plurality of the servomotors is connected to each of the plurality of the wingtip devices respectively, a plurality of carbon rods, and a casing. The brushless type electrical motor provides a lifting force for a Vertical take-off and landing (VTOL) and the plurality of wing tip devices are classified into three types of wing tip devices and the three types of wing tip devices are controlled by the respective servomotors to control yaw, pitch and roll movements thereby stabilizing and controlling the movement of an aircraft.

Abstract translation: 本发明的各种实施例提供一种无人驾驶飞行器，其包括半球体，无刷电，螺旋桨，多个翼尖装置，多个伺服马达，多个伺服马达中的每一个连接到多个 的翼尖装置，多个碳棒和壳体。 无刷式电动机为垂直起降（VTOL）提供提升力，多个翼尖装置分为三种翼尖装置，三种翼尖装置由各自的伺服电机控制 以控制偏航，俯仰和侧倾运动，从而稳定和控制飞行器的运动。