公开(公告)号：WO2010005202A2

公开(公告)日：2010-01-14

申请号：PCT/KR2009003595

申请日：2009-07-01

Applicant: CHOI KEY NAM

Inventor： CHOI KEY NAM

IPC: B64C27/54

CPC classification number: B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/127

Abstract: Conventional bottom blade type trefoil flight vehicles have composite structures wherein a plurality of pairs of fixing plates, forward/backward adjustment blades, and left and right rotation adjustment blades are separately mounted and adjusted, and thus have difficulties in scouting and surveillance in an indoor area due to the heavy weights and the large volumes of said flight vehicles. Another conventional flight vehicle has drawbacks in that flight in the left and right directions is difficult, and an adjustment blade and a fixing plate are arranged adjacent to each other to cause mutual influences of wind and non-uniformity in the flow of wind. The present invention provides a flight vehicle characterized in that three pairs of fixing plates with fixed pitch propellers and adjustment blades are installed at an angle of 120 degrees. The present invention allows for anti-torque, stoppage, forward/backward advancing, left and right rotation, and flight in the left and right direction of flight vehicles, and scouting and surveillance in a narrow space. The flight vehicle of the present invention is simple in structure and control, lightweight, and small in size, thereby improving power efficiency.

Abstract translation: 传统的底叶型三叶飞行器具有复合结构，其中多对固定板，前/后调节叶片和左右旋转调节叶片分别安装和调节，因此在室内区域中的侦察和监视困难 由于重型和大量的所述飞行车辆。 另一种常规的飞行器具有这样的缺点：在左右方向上的飞行是困难的，并且调节叶片和固定板彼此相邻布置，以引起风的相互影响和风的不均匀性。 本发明提供一种飞行器车，其特征在于，具有固定俯仰螺旋桨和调整叶片的三对固定板以120度的角度安装。 本发明允许在飞行器的左右方向进行反扭矩，停止，前进/后退前进，左右旋转和飞行，并且在狭窄的空间中进行侦察和监视。 本发明的飞行器结构简单，重量轻，体积小，提高了电力效率。

公开(公告)号：WO2012030076A3

公开(公告)日：2012-05-03

申请号：PCT/KR2011005702

申请日：2011-08-03

Applicant: SUNTECH ENTPR ,  CHOI KEY DONG ,  CHOI KEY NAM

Inventor： CHOI KEY DONG ,  CHOI KEY NAM

IPC: B64C27/20 ,  A63H27/133 ,  B64C39/02 ,  B64D47/08

CPC classification number: A63H27/12 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108

Abstract: The present invention relates to a rotor driven flight vehicle incorporating small bottom wings for use as a type of unmanned aircraft. Lower wing type flight vehicles of the prior art need complicated structures which are formed by combining various elements including a servo, an adjusting plate, a hinge, and the like so as to continually adjust rotor pitch and operate a control wing for flight control. However, the present invention comprises an adjusting motor mounted at a lower part of a shaft of a power rotor mounted on a central shaft thereof, in which the adjusting motor has an adjusting rotor and is mounted on a fixing plate, enables the flight vehicle to ascend and descend by operating the power rotors, rotates the adjusting rotors mounted at three adjusting motors to perform stops, left turns, right turns, forward movement, backward movement, left movement flight, and right movement flight functions of the flight vehicle using the wind power generated thereby, and is composed of a structure and a device in which components are arranged to enable the center of gravity of the flight vehicle to be in the vicinity of the center shaft.

Abstract translation: 本发明涉及一种转子驱动的飞行器，其结合了用作无人飞机类型的小底翼。 现有技术的下翼式飞行器需要通过组合包括伺服机构，调节板，铰链等等的各种元件形成的复杂结构，以连续地调节转子间距并操作用于飞行控制的控制翼。 然而，本发明包括安装在安装在其中心轴上的动力转子的轴的下部的调节马达，其中调节马达具有调节转子并安装在固定板上，使得飞行器能够 通过操作动力转子上升和下降，使安装在三个调节马达上的调节转子旋转以执行使用风的飞行器的停止，左转，右转，前进，后退，左移动飞行和右移动飞行功能 由此产生的动力，并且由结构和装置构成，其中部件布置成使飞行器的重心能够位于中心轴附近。

公开(公告)号：WO2010005203A3

公开(公告)日：2010-04-22

申请号：PCT/KR2009003597

申请日：2009-07-01

Applicant: SUNTECH ENTPR ,  CHOI KEY NAM

Inventor： CHOI KEY NAM

IPC: B64C27/54

CPC classification number: B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/127

Abstract: Conventional bottom blade type flight vehicles have composite structures and composite flying controls in that a plurality of pairs of fixing plates, forward/backward adjustment blades, and left and right rotation adjustment blades are separately mounted and adjusted to remove an anti-torque of the flight vehicle caused by the rotation of propellers and to fly the vehicles, and thus have difficulties in scouting and surveillance in an indoor area due to the heavy weight and large volume of said flight vehicles. The present invention provides a flight vehicle characterized in that an anti-torque of the flight vehicle is not removed, and the flight vehicle continuously rotates by one adjustment blade and stops, rotates in the forward and backward directions, and flies in the left and right directions. The flight vehicle of the present invention is simple in structure and control, lightweight, and small in size, thus allowing for flight in a narrow space and scouting and surveillance in an indoor area, and improving power efficiency.

Abstract translation: 传统的底部叶片型飞行器具有复合结构和复合飞行控制装置，其中多对固定板，前/后调节叶片以及左右旋转调节叶片分别安装并调节以去除飞行的反扭矩 车辆由于螺旋桨的旋转而引起并且飞行，并且由于所述飞行器的重量大和体积庞大而难以在室内区域进行搜索和监视。 本发明提供了一种飞行器，其特征在于，飞行器的反扭矩没有被去除，并且飞行器通过一个调节片连续旋转并停止，沿前后方向旋转，并且在左右飞行 方向。 本发明的飞行器结构和控制简单，重量轻，体积小，可以在狭窄的空间飞行，在室内进行侦察和监视，提高了电力使用效率。

公开(公告)号：WO2011152614A3

公开(公告)日：2012-03-08

申请号：PCT/KR2011003295

申请日：2011-05-03

Applicant: SUNTECH ENTPR ,  CHOI KEY DONG ,  CHOI KEY NAM

Inventor： CHOI KEY DONG ,  CHOI KEY NAM

IPC: B64C27/20 ,  A63H27/127 ,  B64C29/00 ,  B64C39/02

CPC classification number: B64C27/82 ,  A63H27/12 ,  B64C27/20 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/165

Abstract: The present invention relates to a flying object having small bottom blades, which is one type of unmanned rotor craft. A conventional bottom blade type flying object needs an apparatus having a complex configuration constituted by the combination of various components, such as servo, control plate, hinge, and so forth to control the rotor pitch at every instant and operate a control blade for flight control. However, the present invention provides a bottom-adjustable propeller-type flying object, wherein a circular frame with a fixing plate and a protective plate mounted thereto is installed at a lower part of an axis of a power propeller mounted to the center axis, and a control motor having a control propeller installed thereto is mounted to the protective plate. Accordingly, the flying object performs upward and downward flights using wind force generated by rotation of the power propeller, and performs hovering, and leftward, rightward, forward and rearward flights using wind force generated by rotation of the control propellers that are installed on two control motors. Further, components are arranged in such a manner as to locate a weight center of the flying object near the center axis.

Abstract translation: 本发明涉及一种具有小底片的飞行物体，它是一种无人转子飞行器。 常规的底刃型飞行物体需要具有由诸如伺服机构，控制板，铰链等各种部件的组合构成的复杂结构的装置，以便在每一瞬间控制转子间距，并且操作用于飞行控制的控制叶片 。 然而，本发明提供一种底部可调螺旋桨式飞行物体，其中安装有固定板和保护板的圆形框架安装在安装在中心轴线上的动力螺旋桨的轴的下部，并且 具有安装在其上的控制螺旋桨的控制马达安装在保护板上。 因此，飞行物体使用由动力推进器的旋转产生的风力进行上下飞行，并且使用由安装在两个控制器上的控制螺旋桨的旋转产生的风力进行悬停，左右，向前和向后飞行 电机。 此外，部件被布置成使得飞行物体的重心位于中心轴附近。

公开(公告)号：WO2011102611A2

公开(公告)日：2011-08-25

申请号：PCT/KR2011000643

申请日：2011-01-31

Applicant: CHOI KEY NAM

Inventor： CHOI KEY NAM

IPC: A63H27/133 ,  A63H27/20 ,  B64C27/04 ,  B64C27/12

CPC classification number: A63H27/12

Abstract: Disclosed is a structure for a flying apparatus that facilitates the operation, assembly, and repair of a power switch, charging device, etc. of a small unmanned rotary wing aircraft. The structure comprises: a cylindrical motor operated by electric power and having a motor gear installed thereon; a substrate having an electronic circuit and electronic device built therein, for controlling the flying apparatus; a battery power source mounted on the substrate, for supplying power to the motor; a driving propeller provided with a plurality of wings and having a propeller gear installed thereon in engagement with the motor gear; a hollow axis pipe that is a rotation axis for the driving propeller; two fixing frames configured as hollow cylinders having the motor and axis pipe inserted therein, respectively, and defining a slot in an outside thereof to mount the substrate thereto; a coil plate inserted over the outer periphery of the axis pipe; and control wings installed on the coil plate to control the direction of the flying body.

Abstract translation: 公开了一种便于小型无人转翼飞行器的电源开关，充电装置等的操作，组装和维修的飞行装置的结构。 该结构包括：由电力操作并具有安装在其上的马达齿轮的圆柱形马达; 具有内置电子电路和电子装置的基板，用于控制飞行装置; 电池电源，安装在所述基板上，用于向所述电动机供电; 驱动螺旋桨，其设置有多个翼，并且安装有与所述马达齿轮接合的螺旋桨齿轮; 作为驱动螺旋桨的旋转轴的中空轴管; 两个固定框架被构造成中空圆柱体，其中分别插入有马达和轴线管，并且在其外部限定一个狭槽以将基板安装到其上; 线轴板，其插入在所述轴线管的外周上; 并安装在线圈板上的控制翼来控制飞行体的方向。