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公开(公告)号：KR1020110068599A
公开(公告)日：2011-06-22
申请号：KR1020090125630
申请日：2009-12-16
Applicant: 한국항공우주연구원
Abstract: PURPOSE: A wire holder for soldering is provided to fix a wire on a wire holder and to conveniently perform a soldering operation. CONSTITUTION: A compression unit(142) of a first plate(142a) and a second plate(142b) is connected to a pincer unit(141). An isolation unit(160) is formed in the first plate and the second plate to a traverse direction. The isolation unit isolates the first plate and the second plate at predetermined interval. One end of a position fixing unit is connected to one side of the isolation unit. The isolation unit is connected to the other end of the position fixing unit.
Abstract translation: 目的：提供用于焊接的电线架，用于将电线固定在电线架上，并方便地执行焊接操作。 构成：第一板（142a）和第二板（142b）的压缩单元（142）连接到钳子单元（141）。 隔离单元（160）形成在第一板和第二板中的横向上。 隔离单元以预定间隔隔离第一板和第二板。 位置固定单元的一端连接到隔离单元的一侧。 隔离单元连接到位置固定单元的另一端。
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公开(公告)号：KR101753645B1
公开(公告)日：2017-07-04
申请号：KR1020150156778
申请日：2015-11-09
Applicant: 한국항공우주연구원
Abstract: 본발명에따르면, 비행체(10)의동체일측에장착되는베이스부(110); 상기베이스부(110)의하부에수평방향으로회동가능하게장착되는수평회동부(120); 복수의링크(133,135,137)와복수의관절부(132,134,136)를포함하는다관절구조로이루어져상단이상기수평회동부(120)에연결되고, 각관절부(132,134,136)는제어신호에따라회전구동하면서각 링크(133,135,137)를소정각도로회동시키며, 하단에배치된종단링크(137)의단부에는제어신호에따라파지동작하는집게부(139)가장착된로봇암부(130); 상기종단링크(137)의일측에장착되어공중영상을촬영하는카메라부(140); 상기종단링크(137)의타측에장착되어가속도를측정하는가속도센서부(150); 및상기가속도센서부(150)의측정신호를기초로하여상기종단링크(137)에서의진동발생을판단하며진동발생시진동을감소시킬수 있는방향으로각 링크(133,135,137)가회동하도록관절부(132,134,136)를구동제어하는제어부(160);를포함하는카메라안정화기능이구비된다목적로봇팔장치를개시한다.
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公开(公告)号：KR100740115B1
公开(公告)日：2007-07-16
申请号：KR1020050125908
申请日：2005-12-20
Applicant: 한국항공우주연구원
IPC: G01S13/04
Abstract: 본 발명은 레이저를 이용하여 장애물을 식별하는 방식에 의해 헬리콥터의 야간비행이 가능하도록 하는 헬리콥터 야간비행을 위한 레이저를 이용한 장애물 인식 시스템에 관한 것으로, 장애물 인식을 위한 레이저 빔이 주사되는 복수개의 레이저 포인터로 구성된 레이저 발생장치; 및 상기 레이저 발생장치를 고속으로 회전시키기 위한 회전장치를 포함하여 구성된다.
헬리콥터, 야간비행, 레이저 포인터, 장애물, 회전장치-
公开(公告)号：KR1020070065470A
公开(公告)日：2007-06-25
申请号：KR1020050125908
申请日：2005-12-20
Applicant: 한국항공우주연구원
IPC: G01S13/04
Abstract: An obstacle recognition system using a laser for night flight of a helicopter is provided to increase the obstacle recognition distance 10 times longer than the existing headlight and to increase the survival rate of pilots and thus secure a safe flight by realizing night lifesaving and high-speed flight. An obstacle recognition system installed in a helicopter to assist night flight of the helicopter is composed of a laser generator(100) comprising a plurality of laser pointers for irradiating the laser beam for recognition of an obstacle, and a rotating device(200) for turning the laser generator at high speed. The laser generator is a semiconductor laser oscillator. The output of each laser pointer is 40mW. The rotating device is a pan/tilter for performing a vertical tilting motion and a horizontal panning motion.
Abstract translation: 提供一种使用激光进行直升机夜间飞行的障碍物识别系统，以增加距现有车前灯的10倍以上的障碍物识别距离，提高飞行员的存活率，从而实现夜间救生和高速飞行 飞行。 安装在直升机中以辅助直升机夜间飞行的障碍物识别系统由激光发生器（100）组成，激光发生器（100）包括用于照射激光束以识别障碍物的多个激光指示器和用于转动的旋转装置（200） 激光发生器高速。 激光发生器是半导体激光振荡器。 每个激光指示器的输出为40mW。 旋转装置是用于执行垂直倾斜运动和水平摇摄运动的摇摄/倾斜器。
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公开(公告)号：KR1020170054074A
公开(公告)日：2017-05-17
申请号：KR1020150156778
申请日：2015-11-09
Applicant: 한국항공우주연구원
Abstract: 본발명에따르면, 비행체(10)의동체일측에장착되는베이스부(110); 상기베이스부(110)의하부에수평방향으로회동가능하게장착되는수평회동부(120); 복수의링크(133,135,137)와복수의관절부(132,134,136)를포함하는다관절구조로이루어져상단이상기수평회동부(120)에연결되고, 각관절부(132,134,136)는제어신호에따라회전구동하면서각 링크(133,135,137)를소정각도로회동시키며, 하단에배치된종단링크(137)의단부에는제어신호에따라파지동작하는집게부(139)가장착된로봇암부(130); 상기종단링크(137)의일측에장착되어공중영상을촬영하는카메라부(140); 상기종단링크(137)의타측에장착되어가속도를측정하는가속도센서부(150); 및상기가속도센서부(150)의측정신호를기초로하여상기종단링크(137)에서의진동발생을판단하며진동발생시진동을감소시킬수 있는방향으로각 링크(133,135,137)가회동하도록관절부(132,134,136)를구동제어하는제어부(160);를포함하는카메라안정화기능이구비된다목적로봇팔장치를개시한다.
Abstract translation: 根据本发明，安装在飞行器10的车体的一侧上的基座单元110; 水平旋转单元120，其安装在基座单元110的下部上以能够沿水平方向旋转; 它由所述铰接结构包括多个连接件（133 135 137）和多个接合部（132 134 136）中的每一个连接至所述移相器的顶部水平旋转部分（120），每个接头（132 134 136）是一个转动连杆（133 135 137，而驱动根据控制信号 ）sikimyeo以预定角度旋转时，终端137的链接部分uidan，握持操作放置在底部单元139，根据控制信号的臂（安装机器人的130）镊子; 摄像机单元140，其安装在端部连杆137的一侧以捕获空中图像; 加速度传感器单元150安装在端部连杆137的侧面上以测量加速度; 和加速度传感器150的测量信号的基础上，终端链路137，确定振动发生eseoui和在一个方向，可以降低振动振荡的情况下，接合部分（132 134 136），每个链节（133 135 137）以嘉会洞驱动控制 以及用于控制机器人手臂的控制单元（160）。
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Patent Agency Ranking
公开(公告)号：KR101264179B1
公开(公告)日：2013-05-15
申请号：KR1020110131847
申请日：2011-12-09
Applicant: 한국항공우주연구원
IPC: H01R31/06 , H01R13/646
Abstract: PURPOSE: An RS232 serial cable converter module and an RS232 serial cable converter including the module are provided to prevent entanglement of cables and the waste of time to find a proper cable. CONSTITUTION: A 9 pin female D-Sub connector 1-1(101-FF) is installed on the front of a serial cable converter module. A 9 pin male D-Sub connector 1-1(101-FM) is installed on the front, and is connected to the 9 pin female D-Sub connector 1-1 by one to one. A 9 pin female D-Sub connector 1-2(101-RF) is installed on the rear of the module, and is connected to the 9 pin female D-Sub connector. A 9 pin male D-Sub connector 1-2(101-RM) is installed in the rear, and is connected to the 9 pin female D-Sub connector 1-2 by one to one. [Reference numerals] (AA) Front panel; (BB) Rear panel
Abstract translation: 目的：提供RS232串行电缆转换器模块和包括该模块的RS232串行电缆转换器，以防止电缆缠结，浪费时间找到合适的电缆。 构成：在串行电缆转换器模块的前部安装了9针母D-Sub连接器1-1（101-FF）。 前面安装了9针公头D-Sub连接器1-1（101-FM），并通过一对一连接到9针母D-Sub连接器1-1。 模块后部安装了9针母D-Sub连接器1-2（101-RF），并连接到9针母D-Sub连接器。 后部安装了9针公头D-Sub连接器1-2（101-RM），并通过一对一连接到9针母D-Sub连接器1-2。 （附图标记）（AA）前面板; （BB）后面板
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公开(公告)号：KR1020100061946A
公开(公告)日：2010-06-10
申请号：KR1020080120314
申请日：2008-12-01
Applicant: 한국항공우주연구원
Abstract: PURPOSE: A fault diagnosis system for a healthy sensor of a fly-by-wire control input system is provided to enable safe flying even in case it is unable to find a normal value due to the malfunction of a displacement sensor during aviation. CONSTITUTION: A fault diagnosis system for a healthy sensor of a fly-by-wire control input system comprises a control input apparatus and a controller. The control input apparatus includes three displacement sensors. The controller comprises a flight control module which drives an actuator(4) using a signal transmitted from the control input apparatus, a voting module which extracts the most exact signal from the signals of the three displacement sensors, a detection module which detects a normal sensor in case the voting module determines the failure of two or more sensors, and a fly control module which drives the actuator according to a control input apparatus displacement sensor signal or automatic flight control algorithm.
Abstract translation: 目的：提供一种用于线控控制输入系统的健康传感器的故障诊断系统，以便在航空中由于位移传感器故障而无法找到正常值时能够安全飞行。 构成：用于线控控制输入系统的健康传感器的故障诊断系统包括控制输入装置和控制器。 控制输入装置包括三个位移传感器。 控制器包括使用从控制输入装置发送的信号驱动致动器（4）的飞行控制模块，从三个位移传感器的信号中提取最精确信号的投票模块，检测模块 在投票模块确定两个或更多个传感器的故障的情况下，以及根据控制输入装置位移传感器信号或自动飞行控制算法来驱动致动器的飞行控制模块。
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公开(公告)号：KR100832067B1
公开(公告)日：2008-05-27
申请号：KR1020060133998
申请日：2006-12-26
Applicant: 한국항공우주연구원
Abstract: A stability augmentation unit and a tilt rotor aircraft having the same are provided to return an instable flight state into a stable flight state by driving a moment wheel in case of a change of a flight posture. A tilt rotor aircraft(100) includes a body(110), a pair of fixed wing units, a pair of rotary blade units(130), and a stability augmentation unit. The body is loaded with a pilot seat and various kinds of equipment. A surface of the body is designed in a streamline shape to reduce resistance of air. The fixed wing units are formed on both sides of the body and provide a lift to float the tilt rotor aircraft. The rotary blade units are formed on both sides of the body to provide a thrust corresponding to a drag of the tilt rotor aircraft. The stability augmentation unit includes a momentum wheel(140). The momentum wheel is vertically mounted at a Y-axis of the tilt rotor aircraft to increase stability of a pitch axis of the tilt rotor aircraft.
Abstract translation: 提供了一种稳定性增强装置和具有该稳定装置的倾斜转子飞机，以便在飞行姿态改变的情况下通过驱动力矩轮来将不稳定的飞行状态返回到稳定的飞行状态。 倾斜转子飞机（100）包括主体（110），一对固定翼单元，一对旋转叶片单元（130）和稳定性增强单元。 身体装有飞行员座椅和各种设备。 身体的表面设计成流线形状，以减少空气的阻力。 固定翼单元形成在主体的两侧，并提供升降机以使倾斜转子飞机浮起。 旋转叶片单元形成在主体的两侧，以提供对应于倾斜转子飞机的阻力的推力。 稳定性增强单元包括动量轮（140）。 动量轮垂直安装在倾斜转子飞行器的Y轴上，以增加倾斜转子飞机的俯仰轴的稳定性。
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公开(公告)号：KR101388082B1
公开(公告)日：2014-04-22
申请号：KR1020130010309
申请日：2013-01-30
Applicant: 한국항공우주연구원
Inventor： 이장호
Abstract: The present invention relates to an auxiliary landing apparatus for an unmanned aircraft and a method for operating the same, includes: a case which is installed on the bottom side of an aircraft which is installed with a linear motor inside; a landing unit which includes first and second landing plates which are installed inside on both sides and which is deployed to the outside of the case by the operation of the linear motor; a detection sensor which is installed on the landing wheels of the unmanned aircraft in order to sense the contact between the landing wheels and the ground; and a control unit which operates the linear motor according to the sensed result of the detection sensor. According to the present invention, the landing unit is deployed to both sides of the unmanned aircraft by the linear motor, which is installed on the bottom of the unmanned aircraft. Thereby, when the unmanned aircraft lands, the fuselage of the aircraft can be prevented from overturning, and damages to the aircraft can be prevented.
Abstract translation: 无人飞机辅助着陆装置及其操作方法技术领域本发明涉及一种无人驾驶飞机的辅助着陆装置及其操作方法，包括：安装在内装有线性马达的飞机底部的壳体; 一个着陆单元，包括第一和第二登陆板，它们安装在两侧的内侧，并通过线性马达的操作而部署到壳体外部; 检测传感器，其安装在无人驾驶飞机的着陆车轮上，以便感测着陆车轮与地面之间的接触; 以及控制单元，其根据检测传感器的感测结果操作线性电动机。 根据本发明，通过安装在无人驾驶飞机底部的线性马达将着陆单元部署到无人驾驶飞机的两侧。 因此，当无人飞机降落时，可以防止飞机的机身翻倒，可以防止对飞机的损坏。
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公开(公告)号：KR101063437B1
公开(公告)日：2011-09-08
申请号：KR1020090125630
申请日：2009-12-16
Applicant: 한국항공우주연구원
Abstract: 본 발명은 커넥터 및 와이어 연결을 위한 납땜시 납땜을 할 와이어를 고정되게 잡아 주어 보다 쉽게 납땜을 수행할 수 있도록 하는 납땜용 와이어 홀더에 관한 것이다.
이 납땜용 와이어 홀더는, 집게 형상의 집게부와, 상기 집게부를 벌리거나 오므리게 상기 집게부와 연결되는 제 1 플레이트와 제 2 플레이트의 압착부와, 상기 제 1 플레이트와 제 2 플레이트의 일단에 횡방향으로 형성되어 상기 제 1 플레이트와 제 2 플레이트를 소정 간격으로 이격시키는 간격부와, 일단이 상기 간격부의 일측에 연결되는 위치 고정부와, 상기 위치 고정부의 타단에 연결되는 착탈식 연결 수단을 포함한다.
본 발명에 따르면, 한 손에는 솔더를 다른 손에는 납을 잡고 와이어는 소형 바이스에 장착할 수 있는 와이어 홀더가 고정해주어 납땜을 보다 편리하고 정확하게 할 수 있다.
납땜 홀더, 와이어홀더, 납땜보조장치, 소형바이스, 자석
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