公开(公告)号：KR101343246B1

公开(公告)日：2013-12-18

申请号：KR1020130113467

申请日：2013-09-24

Applicant: (주)한국유에이브이

Inventor： 김무선 ,  홍용준

IPC: B64F1/04

CPC classification number: B64F1/06 ,  B64C2201/084

Abstract: The present invention relates to a launcher for an unmanned aerial vehicle. The present invention includes a moving rail, an airplane transfer unit, a unit for propelling the transfer unit, and a unit for locking the transfer unit. A traction wire includes an elastic wire applying an elastic force to the airplane transfer unit. The unit for locking the transfer unit includes a pair of locking arms and a locking arm driving unit. The airplane transfer unit includes an upper guide shaft, a lower guide shaft, a plurality of horizontal support shafts, and a shock absorbing member. The locking arm includes an insertion bearing, a rotary shaft, and a rotary bearing. [Reference numerals] (350) Wrench switch;(440) Firing switch

Abstract translation: 本发明涉及一种无人机的发射器。 本发明包括移动导轨，飞机传送单元，用于推动传送单元的单元和用于锁定传送单元的单元。 牵引线包括向飞机传送单元施加弹性力的弹性线。 用于锁定传送单元的单元包括一对锁定臂和锁定臂驱动单元。 飞机传送单元包括上引导轴，下引导轴，多个水平支撑轴和减震构件。 锁定臂包括插入轴承，旋转轴和旋转轴承。 （参考号）（350）扳手开关;（440）点火开关

公开(公告)号：KR1020050023002A

公开(公告)日：2005-03-09

申请号：KR1020030060003

申请日：2003-08-28

Applicant: 김주은

Inventor： 노항배 ,  김태민 ,  김주은

IPC: B64C39/02

CPC classification number: B64C39/024 ,  B64C3/00 ,  B64C2001/0081 ,  B64C2201/021 ,  B64C2201/084 ,  B64C2201/185 ,  B64D17/80 ,  B64D47/00 ,  B64F1/06

Abstract: PURPOSE: A radio control miniature aircraft is provided to facilitate carriage in consideration of work conditions and to enable the miniature aircraft to take-off and land even in a limited space. CONSTITUTION: A radio control miniature aircraft comprises a body part(10) and wing parts(20) made of a lightweight material. The radio control miniature aircraft is capable of flying by utilizing power supplied from an engine. The radio control miniature aircraft has a line dropping device where an air drop(100) to which a pilot line is connected is mounted and detached. Flying and line dropping control action wherein the air drop is detached from the line dropping device are possible by worker's wireless remote control.

Abstract translation: 目的：提供无线电遥控微型飞机，以便考虑到工作条件的运输，并使小型飞机即使在有限的空间内起飞和降落。 构成：无线电控制微型飞机包括主体部分（10）和由轻质材料制成的翼部件（20）。 无线电控制微型飞机能够通过利用从发动机提供的动力来飞行。 无线电控制微型飞机具有线路降落装置，其中连接有先导线路的空气滴（100）被安装和拆卸。 通过员工的无线遥控器可以进行空气滴脱离设备的飞行和线路落下控制动作。

公开(公告)号：KR1019890000530B1

公开(公告)日：1989-03-20

申请号：KR1019820003604

申请日：1982-08-11

Applicant: 레이테온 이-시스템즈 인코포레이티드

Inventor： 찰스에이취.터버주니어 ,  프레데릭에이.베렌스 ,  존에이취.헌튼

IPC: B64C39/02

CPC classification number: F41G7/22 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/046 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/208 ,  B64F1/06 ,  F41G7/007

Abstract: The remotely piloted aircraft has control surfaces asymmetrical in the pitch and yaw planes, a sensor, and a guidance system operative in the terminal portions of the flight of the aircraft in a yaw-to- turn mode with a zero roll rate. The system has a directional sensor for providing azimuth and elevation error signals. A device provides guidance signals indicative of the rate of change of the azimuth and elevation signals. A guidance programmer responds to the guidance signals for providing pitch control and yaw control signals. An altitude sensor provides an altitude control signal. Roll, pitch and yaw rate gyros provide a rate control signal and a three axis autopilot.

Abstract translation: 遥控飞行器具有在俯仰和偏航平面中不对称的控制表面，传感器和在零滚动速率的偏航 - 转弯模式下在飞行器的飞行的终端部分中操作的引导系统。 该系统具有用于提供方位角和仰角误差信号的方向传感器。 装置提供指示方位角和仰角信号变化率的指导信号。 指导程序员响应用于提供俯仰控制和偏航控制信号的引导信号。 高度传感器提供高度控制信号。 滚动，俯仰和偏航率陀螺仪提供速率控制信号和三轴自动驾驶仪。