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61. 发明授权

KR101621142B1 무인 항공기 회수 장치 및 회수 방법 有权
标题翻译：撤离无人驾驶飞行器的装置及其撤离方法
公开(公告)号：KR101621142B1
公开(公告)日：2016-05-16
申请号：KR1020140074917
申请日：2014-06-19
申请人： 포항공과대학교 산학협력단
发明人： 유선철 , 구정회 , 조한길 , 조현우 , 표주현
IPC分类号： B64F1/02 , B64C39/02 , B64C19/02 , B64F3/02
摘要： 무인항공기회수장치및 방법이제공된다. 본발명의일 측면에따르면, 무인항공기를회수하기위한장치에있어서, 상기무인항공기를보관하는수납공간을갖는본체; 상기본체의상부측에서펼쳐져목표물인상기무인항공기를공중에서포획하는그물망; 상기그물망을본체의상부측으로이송하고서로일정간격이격배치되어상기그물망을펼치는복수개의소형비행체; 및일단이상기그물망에연결되고타단이상기본체에연결되어상기그물망을통해포획된무인항공기를상기수납공간측으로견인하는견인와이어;를포함하는무인항공기회수장치를제공한다.

62. 发明公开

KR1020130081275A 이동식 항공기 회복 시스템 审中-实审
标题翻译：移动飞机恢复系统
公开(公告)号：KR1020130081275A
公开(公告)日：2013-07-16
申请号：KR1020137000536
申请日：2011-05-03
申请人： 에이에이아이 코포레이션
发明人： 밀러,스티븐,더블유. , 폭스,스티븐,제이. , 쉴,그레이엄,더블유. , 아스케,브라이언,에이.
IPC分类号： B64F1/02 , B64C39/02 , F16F9/00 , F16F1/36 , F16F15/02
CPC分类号： B64F1/02 , B64C2201/182 , F41H11/02 , F41J13/00 , B64C39/024 , F16F1/36 , F16F9/00 , F16F15/02
摘要： 항공기 회복 장치는 포획 장치와 제 1 및 제 2 버팀대 쌍을 포함한다. 제 1 및 제 2 버팀대 쌍은 각각 상부 및 하부 버팀대를 포함한다. 제 1 버팀대 쌍은 상기 버팀대 쌍이 상기 항공기를 포획하기 위하여 상기 포획 장치를 개방 위치에서 지지하는 제 1 위치로부터, 상기 버팀대 쌍이 상기 포획 장치에 상기 항공기가 충돌한 이후에 포획된 상기 항공기를 보유하기 위하여 상기 포획 장치를 폐쇄 위치에서 지지하는 제 2 위치로 움직인다. 제 2 버팀대 쌍 또한 상기 제 1 위치로부터 제 2 위치로 움직인다. 일 단이 상기 포획 장치의 각 상부 영역 또는 하부 영역과 각각 연결되고 타 단이 각 상부 버팀대 또는 하부 버팀대와 각각 연결되는 에너지 요소들은 상기 항공기의 충돌력을 흡수한다.

63. 发明授权

KR101214971B1 항공기 이착륙 성능향상장치 有权
标题翻译：一种提高飞机起降性能的装置
公开(公告)号：KR101214971B1
公开(公告)日：2012-12-24
申请号：KR1020100096659
申请日：2010-10-05
申请人： 김춘산
发明人： 김춘산
IPC分类号： B64F1/02 , E01H3/04 , B64F1/36
摘要： 본발명은항공기이착륙성능향상장치에대한것으로, 더욱상세하게는활주로또는/및활주로주변의대기에물을분사하는물공급장치와상기물공급장치로부터분사된물에의해다습해진공기를흡입하여냉각제습시킨후 냉각제습된공기를활주로의대기에분사하는공기공급장치를포함하고, 상기물공급장치는물을저장하는물탱크와상기물탱크의수온을감지하는온도센서와상기물탱크에저장된물을냉각시키는냉각기와상기물탱크에저장된물을공급받아활주로와활주로주변의대기에물을분사하는물분사부를포함하고, 상기공기공급장치는활주로또는/및활주로주변의공기를흡입하여냉각제습시키는냉각제습부와상기냉각제습부에서냉각제습된공기를압축하는공기압축부와상기공기압축부에서압축된공기를활주로의대기에분사하는공기분사부를포함하여, 활주로또는/및활주로주변대기의온도와습도를낮추어공기의밀도를높여항공기의이착륙거리를단축시킬수 있는항공기이착륙성능향상장치를제공하고자한다.

64. 发明授权

KR101140763B1 무인 비행체 착륙기 有权
标题翻译：着陆装置是无人驾驶飞机
公开(公告)号：KR101140763B1
公开(公告)日：2012-07-12
申请号：KR1020090051195
申请日：2009-06-09
申请人： 정운규
发明人： 정운규
IPC分类号： B64F1/02 , B64C25/68 , B64F1/36 , B64F1/04
摘要： 본 발명은 무인 비행체를 착륙시키기 위한 착륙기에 관한 것으로서, 구체적으로는 바닥에 고정하도록 형성된 베이스; 상기 베이스 양측에 설치된 한 쌍의 암; 상기 베이스 양측에 설치된 한 쌍의 실린더; 상기 양측 암 사이에 설치된 그물망; 및 상기 베이스 양측에 설치된 이완장치;로 구성됨에 따라, 하강하는 비행체를 그물망으로 받아 안전하게 착륙시킬 수 있도록 한 무인 비행체 착륙기를 제공하게 된다.
무인비행체, 착륙기

65. 发明公开

KR1020120035275A 항공기 이착륙 성능향상장치 有权
标题翻译：提高飞机起飞和着陆性能的装置
公开(公告)号：KR1020120035275A
公开(公告)日：2012-04-16
申请号：KR1020100096659
申请日：2010-10-05
申请人： 김춘산
发明人： 김춘산
IPC分类号： B64F1/02 , E01H3/04 , B64F1/36
摘要： PURPOSE: An apparatus for enhancing take-off and landing performance of an aircraft is provided to reduce take-off and landing distance of an aircraft by decreasing temperature and humidity in a landing strip and/or around the landing strip to increase air density and to become extinct wake turbulence in early stages by spraying cooled and dehumidified air to the atmosphere on the landing strip. CONSTITUTION: An apparatus for enhancing take-off and landing performance of an aircraft includes a water supply unit and an air supply unit. The water supply unit sprays water to decrease atmosphere temperature on a landing strip and increase air density, thereby reducing take-off and landing distance. After the air supply unit sucks air which is humid by the water sprayed from the water supply unit and cools and dehumidifies, the cooled and dehumidified air is sprayed in the atmosphere or one the ground of the landing strip.
摘要翻译：目的：提供一种用于增强飞机的起飞和着陆性能的装置，以通过降低着陆带和/或着陆带周围的温度和湿度来降低飞机的起飞和着陆距离，以增加空气密度，并且在早期阶段通过将冷却和除湿的空气喷洒到着陆带上的大气中而成为灭绝的尾流湍流。构成：用于增强飞机起飞和着陆性能的装置包括供水单元和空气供应单元。供水单元喷洒水以降低着陆带上的气氛温度，增加空气密度，从而减少起飞和着陆距离。空气供应单元吸入由供水单元喷射的水分潮湿的空气，冷却并除湿后，将冷却和除湿的空气喷洒在大气层或着陆条的一侧。

66. 发明公开

KR1020100133809A 무인항공기의 착륙 유도 장치 및 방법 无效
标题翻译：用于引导不客气的车辆着陆的装置和方法
公开(公告)号：KR1020100133809A
公开(公告)日：2010-12-22
申请号：KR1020090052534
申请日：2009-06-12
申请人： (주)엔에스에이치
发明人： 노우현
IPC分类号： B64F1/02 , B64F1/22 , B64D45/04 , B64F1/36
摘要： PURPOSE: An apparatus and method for guiding the landing of an unmanned aerial vehicle are provided to land a flying unmanned aerial vehicle using a net in the place difficult for an unmanned aerial vehicle to land using a landing gear. CONSTITUTION: An apparatus for guiding the landing of an unmanned aerial vehicle comprises a landing guide(10), a plurality of transmitters(21,22,23,24), a receiver(30), and a controller. The landing guide comprises a net(13) in which a unmanned aerial vehicle is settled. The transmitters lead the unmanned aerial vehicle to the net of the landing guide. The receiver receives signals transmitted from the transmitters. The controller compares the value obtained through the receiver and the transmitters with the preset reference value and adjusts the flight path of the unmanned aerial vehicle.
摘要翻译：目的：提供一种用于引导无人驾驶飞机着陆的装置和方法，以便在无人驾驶飞机难以使用起落架降落的地方使用网的飞行无人驾驶飞机着陆。构成：用于引导无人机的着陆的装置包括着陆引导件（10），多个发射器（21,22,23,24），接收器（30）和控制器。着陆引导件包括其中无人驾驶飞行器沉降的网（13）。发射机将无人驾驶飞机引导到着陆导轨的网。接收机接收从发射机发射的信号。控制器通过接收机和发射机获得的值与预设参考值进行比较，并调整无人机的飞行路径。

67. 发明公开

KR1020100132395A 무인 비행체 착륙기 有权
标题翻译：无线平面设备
公开(公告)号：KR1020100132395A
公开(公告)日：2010-12-17
申请号：KR1020090051195
申请日：2009-06-09
申请人： 정운규
发明人： 정운규
IPC分类号： B64F1/02 , B64C25/68 , B64F1/36 , B64F1/04
摘要： PURPOSE: A landing apparatus for an unmanned aircraft using a mesh net is provided to prevent a landed aircraft and a mesh net by buffering an impact when receiving the aircraft with the mesh net. CONSTITUTION: A landing apparatus for an unmanned aircraft comprises a base(100) which is fixed on the surface, a pair of arms(200) which are installed on both sides of the base and each formed with a rotary shaft(210), a pair of cylinders(300) which are respectively connected to the top of the rotary shafts of the arms, a mesh net(400) which is installed between the arms, and a release mechanism(500) which keeps straps(510), connected to the mesh net, tight and unwinds the straps when an impact is applied to the mesh net.
摘要翻译：目的：提供一种使用网状网的无人驾驶飞机的着陆装置，以便在用网状网接收飞机时，通过缓冲撞击来防止着陆飞机和网状网。构成：用于无人驾驶飞机的着陆装置包括固定在表面上的基座（100），一对臂（200），其安装在基座的两侧并且各自形成有旋转轴（210），分别连接到臂的旋转轴的顶部的一对气缸（300），安装在臂之间的网状网（400）和保持带（510）的释放机构（500），连接到网状网，当对网状网施加冲击时，紧紧并展开带子。

68. 发明公开

KR1020100070685A 무인항공기의 회수시스템 无效
标题翻译：非机动车辆恢复系统
公开(公告)号：KR1020100070685A
公开(公告)日：2010-06-28
申请号：KR1020080129340
申请日：2008-12-18
申请人： 한국항공우주연구원
发明人： 구삼옥
IPC分类号： B64F1/02 , B64D1/22
摘要： PURPOSE: A recovery system for an unmanned aircraft is provided to allow a flying unmanned aircraft to safely return to a place without a runway by hanging a latch of a recovery cable attached to the unmanned aircraft on a recovery cable of the ground. CONSTITUTION: A recovery system for an unmanned aircraft comprises a first recovery unit(10), a second recovery unit(20), and a supporting part(30). The first recovery unit is installed and allows the position change thereof with respect to an unmanned aircraft body(F) and includes a first recovery cable and a latch(13). The second recovery unit is interconnected with the first recovery unit and clinches the flying unmanned aircraft body. The supporting unit supports and controls the height of the second recovery unit. The first recovery cable is wound in a first winder(12) of the unmanned aircraft body and selectively released.
摘要翻译：目的：提供无人驾驶飞机的恢复系统，使飞行的无人驾驶飞机能够安全地返回到没有跑道的地方，将连接在无人驾驶飞机上的回收缆线的闩锁悬挂在地面的回收缆线上。构成：无人飞行器的回收系统包括第一回收单元（10），第二回收单元（20）和支撑部分（30）。第一恢复单元被安装并且允许其相对于无人驾驶飞机主体（F）的位置改变，并且包括第一恢复缆索和闩锁（13）。第二回收单元与第一回收单元相互连接，并与飞行的无人机体抵接。支撑单元支撑并控制第二回收单元的高度。第一恢复电缆被卷绕在无人机体的第一络纱机（12）中并选择性地释放。

69. 发明授权

KR100941297B1 무인 항공기용 그물 회수 장치 有权
标题翻译：用于无人驾驶车辆的网络恢复系统
公开(公告)号：KR100941297B1
公开(公告)日：2010-02-11
申请号：KR1020090033682
申请日：2009-04-17
申请人： 한국항공우주산업 주식회사
发明人： 강재일 , 구충서 , 강인원 , 우종응 , 김임수
IPC分类号： B64F1/02 , B64F1/36 , B64C25/68 , B64F1/00
摘要： PURPOSE: A net collecting device for a pilotless aircraft is provided to safely collect the pilotless aircraft in case there are no runways or runway facilities. CONSTITUTION: Supports(20,21) are coupled on the both ends of a main frame(10). A net(30) is installed between the supports. The ends of a first string and a second string(41) are connected to both ends of the net respectively. A brake wheel(50) is connected to the other end of the first string and the second string. A brake(60) connects the central axis of the brake wheel. The brake releases the first string and the second string when the pilotless aircraft collides with the net.
摘要翻译：目的：提供无人驾驶飞机的净收集装置，以便在没有跑道或跑道设施的情况下安全收集无人驾驶飞机。构成：支架（20,21）连接在主框架（10）的两端。网（30）安装在支架之间。第一串和第二串（41）的端部分别连接到网的两端。制动轮（50）连接到第一串和第二串的另一端。制动器（60）连接制动轮的中心轴线。当无人驾驶飞机与网络碰撞时，制动器释放第一弦和第二弦。

70. 发明授权

KR100929484B1 무인 항공기용 제동 장치 有权
标题翻译：无人驾驶车辆的制动装置
公开(公告)号：KR100929484B1
公开(公告)日：2009-12-02
申请号：KR1020090065411
申请日：2009-07-17
申请人： 한국항공우주산업 주식회사
发明人： 김재혁 , 강인원 , 구충서 , 우종응 , 김임수
IPC分类号： B64F1/02 , B64C25/68 , B64F1/36
摘要： PURPOSE: A braking device for an unmanned aircraft is provided to safely return an unmanned aircraft to its original position by predicting a stop point of an unmanned aircraft seized with wire or mesh and direct it. CONSTITUTION: A braking device for an unmanned aircraft(1) comprises a wire(10) and a braking device(20). The braking device is attached to both ends of the wire respectively. The braking device comprises an upper frame, a sub-frame, a rotary shaft, a wheel, a brake disk, a caliper, a braking power adjusting screw. The upper frame and the sub-frame are fixed on the ground. The rotary shaft is bearing-joined between the upper frame and the sub-frame. One end of the wire is attached to the rotary shaft, and wound around it. The wheel is attached to the rotary shaft. The brake disk is attached to the rotary shaft, turning with the wheel. The caliper is equipped with a clamping part. The periphery of the brake disk is inserted into the clamping portion and turns inside. The braking power adjusting screw joined with the clamping part of the caliper is tightened or released to adjust the gap of the clamping part.
摘要翻译：目的：提供无人驾驶飞机的制动装置，通过预测用电线或网状物检获的无人驾驶飞机的停靠点并将其引导，将无人驾驶飞机安全地返回到其原始位置。构成：用于无人驾驶飞机（1）的制动装置包括线（10）和制动装置（20）。制动装置分别连接到电线的两端。制动装置包括上框架，副框架，旋转轴，车轮，制动盘，卡钳，制动力调节螺钉。上框架和子框架固定在地面上。旋转轴在上框架和子框架之间承载。线的一端连接到旋转轴上，并缠绕在其上。车轮连接到旋转轴。制动盘安装在旋转轴上，与车轮一起转动。卡钳配有夹紧部件。制动盘的周边插入到夹紧部分内部。与卡钳的夹紧部接合的制动力调节螺钉被紧固或松开以调节夹紧部的间隙。

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