公开(公告)号：KR20180045646A

公开(公告)日：2018-05-04

申请号：KR20160140243

申请日：2016-10-26

IPC: B64C31/00 ,  B64C11/28 ,  B64C39/02 ,  B64D47/08

CPC classification number: B64C39/02 ,  B64C2201/08 ,  B64C2201/123 ,  B64D19/02 ,  F42B10/14 ,  F42B10/58 ,  F42B30/006

Abstract: 본발명의실시예에따른관측용무동력형비행유닛은발사장비에장착되어상기발사장비의작동시 미리설정된목표방향을향하여날아간후 상사점(TDP:Top Dead Point, 上死點)의위치에서자중에의해지상을향하여낙하되는몸체부, 상기몸체부에결합되어상기몸체부의낙하시 상기몸체부에작용하는항력에의하여자동으로회전력을발생시켜상기몸체부의낙하속도를지연시키는프로펠러부, 그리고상기몸체부에설치되어상기몸체부의낙하시 상기지상에대한영상정보를취득하는영상부를포함한다. 본발명에의하면, 재난, 치안등의긴급상황시 총알또는소형로켓등과같이발사장비에장착되어높은고도를향하여발사된후, 항력에의해자동적으로회전력을발생시켜지면을향하여서서히낙하되면서지상에대한영상정보를취득할수 있는구조로형성됨으로써, 사용이간단하고비행시에도별도의조작이필요치않으므로운행시 준비시간이필요하지않고, 신속히긴급상황발생지역주변을관측할수 있다.

公开(公告)号：KR1020160112252A

公开(公告)日：2016-09-28

申请号：KR1020150037581

申请日：2015-03-18

Applicant: 엘지전자 주식회사

Inventor： 조태훈 ,  신충환

IPC: B64C39/02 ,  B64D45/00 ,  B64D47/00

CPC classification number: B64C39/024 ,  A62C3/0242 ,  B60P3/11 ,  B60Q7/00 ,  B60Q7/005 ,  B64C2201/027 ,  B64C2201/08 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/141 ,  B64C2201/208 ,  B64F1/222 ,  G05D1/0088 ,  G05D1/101 ,  G08G1/04 ,  G08G1/09 ,  G08G1/0955 ,  G08G1/16 ,  G08G1/162 ,  G08G1/205 ,  G08G7/00 ,  B64C39/02 ,  B64C2201/127 ,  B64D45/00 ,  B64D47/00

Abstract: 본발명은상기차량에장착되며내부공간을구비하며, 발사부를구비하는하우징, 상기하우징에수납된상태에서상기차량의주행상태가기 설정된조건에만족되는경우, 상기하우징으로부터발사되는무인항공체, 상기하우징으로부터발사되는것에근거하여, 상공을비행하도록상기무인항공체에장착되는날개부, 상기무인항공체에장착되는출력부및 상기무인항공체가발사된발생된때의상기주행상태에관한정보에의하여설정된위치로, 상기무인항공체를이동시키도록상기날개부를제어하고, 상기주행상태와관련된경고정보를출력하도록상기출력부를제어하는제어부를포함하는무인항공장치를제공한다.

Abstract translation: 本发明提供一种无人驾驶空气装置，其包括：安装在车辆中的壳体，具有内部空间，并具有发射单元; 当车辆的行驶状态满足预定条件时被存储在所述壳体中的从所述壳体发射的无人驾驶飞行器; 安装在无人驾驶飞行器中的翼单元，以便在从壳体发射的基础上在天空中飞行; 安装在无人驾驶飞行器中的输出单元; 以及控制单元，其控制所述机翼单元，通过相对于所述无人驾驶飞行器的驾驶状态的信息，将所述无人机移动到预定位置，并且控制所述输出单元输出相对于所述驾驶状态的警告信息。

公开(公告)号：KR1020150130512A

公开(公告)日：2015-11-23

申请号：KR1020157029113

申请日：2014-03-05

Applicant: 리퀴드 로보틱스, 아이엔씨.

Inventor： 하인,로저지. ,  하인,데렉엘.

IPC: B63B35/50 ,  B64F1/04 ,  B64F1/22 ,  B63H19/02 ,  B64C39/02

CPC classification number: B63B35/50 ,  B63B35/00 ,  B63H19/02 ,  B64C19/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/08 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/141 ,  B64C2201/201 ,  B64C2201/205 ,  B64F1/04 ,  B64F1/221 ,  Y02T70/59

Abstract: 파력운송기구와무인항공운송기구(UAV들또는드론들)의용도를조합한장치및 방법들이개시된다. UAV는파력운송기구로부터발사될수 있으며, 다른선박을관찰하며, 그의관찰결과들을파력운송기구에보고하며, 파력운송기구는관찰의결과들을원격위치에보고할수 있다. UAV는수중에착륙할수 있으며그 후에파력운송기구에의해복원될수 있다.

公开(公告)号：KR1020020081608A

公开(公告)日：2002-10-30

申请号：KR1020010020981

申请日：2001-04-19

Applicant: 명대명

Inventor： 명대명

IPC: A63H27/14

CPC classification number: A63H27/14 ,  A63H27/002 ,  B64C2201/08 ,  B64F1/04

Abstract: PURPOSE: A launching device for a glider is provided to enable a user to fly the glider by oneself while freely adjusting the width and an angle between support pieces according to a direction or strength of wind and a size of the glider. CONSTITUTION: A stay member(3) having a glider fastening boss(4) is coupled to the rear ends of length adjustable support pieces(1,2). A triangular height adjustable support legs(5) is installed beneath the center of the support pieces to adjust a height of an ascending/descending rod(6). The rod is formed with bolt holes(7,8) on the upper end thereof, a bolt(9) and a nut(10) are fastened into the bolt holes and a guide bore(12) formed at the lower end of a fixing rod so as to adjust an inclination angle between the rods. Actuating rods(14,16) are coupled between the support pieces and the fixing rod via the engagement of racks and a pinion. Also, a wind bag(21) is attached to the upper end of a fixing piece(19) having a bolt portion(20) to be fitted into a screw bore(18) formed at the rear end of one of the support pieces.

Abstract translation: 目的：提供一种用于滑翔机的发射装置，使用户能够根据风的方向或强度以及滑翔机的大小自由地调节支撑件之间的宽度和角度，自己飞行滑翔机。 构成：具有滑动件紧固凸台（4）的支撑构件（3）联接到长度可调支撑件（1,2）的后端。 三角高度可调节支撑腿（5）安装在支撑件中心的下方，以调节上升/下降杆（6）的高度。 杆在其上端形成有螺栓孔（7,8），螺栓（9）和螺母（10）紧固到螺栓孔中，并且导向孔（12）形成在固定件的下端 杆，以调节杆之间的倾斜角度。 致动杆（14,16）经由齿条和小齿轮的接合而联接在支撑件和固定杆之间。 此外，风袋（21）附接到具有螺栓部分（20）的固定件（19）的上端，以将其装配到形成在一个支撑件的后端上的螺钉孔（18）中。

公开(公告)号：US20240067357A1

公开(公告)日：2024-02-29

申请号：US17895193

申请日：2022-08-25

Applicant: Martin Daniel Holmes

Inventor： Martin Daniel Holmes

IPC: B64F1/08 ,  B64C39/02 ,  B64F5/10

CPC classification number: B64F1/08 ,  B64C39/022 ,  B64C39/024 ,  B64F5/10 ,  B64C2201/08 ,  B64C2201/128 ,  B64C2201/20

Abstract: A system for airborne storage, assembly and launch of aircraft and spacecraft.

公开(公告)号：US20230400855A1

公开(公告)日：2023-12-14

申请号：US17838338

申请日：2022-06-13

Applicant: Taylor Montgomery Mantick

Inventor： Taylor Montgomery Mantick

IPC: G05D1/00 ,  G05D1/10 ,  B64C39/02 ,  B64D47/00 ,  B64F1/22 ,  B64D25/00

CPC classification number: G05D1/0094 ,  G05D1/104 ,  B64C39/024 ,  B64D47/00 ,  B64F1/222 ,  B64D25/00 ,  B64C2201/08 ,  B64C2201/146 ,  B64C2201/122

Abstract: A system and method for land management using a remote monitoring network including a plurality of sensor operation towers that utilize renewably sustained stationary and mobile sensors, including vertical takeoff and landing remotely piloted aircraft (VTOL RPA), that are autonomously launched, recovered, stored, and maintained by the sensor operation towers to autonomously and remotely acquire environmental, electro-optic, infrared, and light detection and ranging sensor data which is then organized via computer programs encoded on a storage medium and then communicated via a network in a manner that updates and enhances the short-term and long-term situational awareness and decision making capabilities of modern land management entities and thereby aids in land management practices.

公开(公告)号：US11645922B2

公开(公告)日：2023-05-09

申请号：US17148403

申请日：2021-01-13

Applicant: Guardian Robotics, Inc.

Inventor： Andrew Magdaleno

IPC: G08G5/00 ,  B64C39/02 ,  G05D1/00 ,  G05D1/04

CPC classification number: G08G5/003 ,  B64C39/024 ,  G05D1/0022 ,  G05D1/0027 ,  G05D1/042 ,  B64C2201/042 ,  B64C2201/08 ,  B64C2201/108 ,  B64C2201/121 ,  B64C2201/127

Abstract: An active shooter response system is disclosed. The system utilizes a system of sensors and drones which may receive data at a base station. The base station may centrally process the data from the drones and the sensors so that a coordinated attack on the active shooter can be formulated either automatically without human intervention or manually at the base station by an operator of the system.

公开(公告)号：US20190185161A1

公开(公告)日：2019-06-20

申请号：US16323704

申请日：2017-08-08

Applicant: CLEO ROBOTICS INC.

Inventor： Omar ELERYAN ,  Szymon CZARNOTA

IPC: B64C39/02 ,  B64C13/16 ,  B64D47/08

CPC classification number: B64C39/024 ,  B64C13/16 ,  B64C27/08 ,  B64C29/00 ,  B64C39/00 ,  B64C39/02 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/08 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2201/18 ,  B64C2201/20 ,  B64D47/08

Abstract: A lightweight, pocket-sized unmanned aerial vehicle (UAV) that can be held in an outstretched hand by a user for take-off and landing of the UAV. The UAV comprises a semi-toroidal or a substantially toroidal hollow body that defines a duct. The UAV further comprises a motor for rotating a fan that directs air into and out of the duct enabling the UAV to take flight. The UAV comprises a flight-control system that comprises at least two flight control surfaces that can alter the directed air as it flows through the duct for controlling the roll and pitch and optionally the yaw of the UAV during flight. The flight control system may be controlled by a microprocessor controller. The UAV further comprises a payload, with at least a wireless transmitter and receiver unit.

公开(公告)号：US20180281939A1

公开(公告)日：2018-10-04

申请号：US15941133

申请日：2018-03-30

Applicant: The Government of the United States of America, as represented by the Secretary of the Navy

Inventor： Steven K. Tayman

IPC: B64C27/50 ,  B64C27/10 ,  B64C39/02

CPC classification number: B64C27/50 ,  B64C27/10 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/042 ,  B64C2201/08 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/18 ,  B64C2201/201

Abstract: An expendable rotary wing unmanned aircraft capable of storage in a cylindrical housing includes a longitudinally extending body having an upper end and a lower end; and a pair of counter-rotating coaxial rotors each located at respective ends of longitudinally-extending body, wherein each rotor includes two or more blades, each blade rotatably coupled to a remainder of the rotor at a hinged joint and thereby extending along a length of the body in a storage configuration and extending radially outward from the body in a flight configuration.

公开(公告)号：US20180129208A1

公开(公告)日：2018-05-10

申请号：US15807191

申请日：2017-11-08

Applicant: Digital Aerolus, Inc.

Inventor： Thomas D. Williams ,  Ian J. McEwan ,  Jeffery J. Alholm

IPC: G05D1/00 ,  B64C39/02 ,  G08G5/04

CPC classification number: G05D1/0088 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/08 ,  B64C2201/108 ,  B64C2201/141 ,  B64C2201/145 ,  G05D1/0016 ,  G06F1/1694 ,  G06F3/017 ,  G06F2200/1637 ,  G06F2203/04105 ,  G08G5/0013 ,  G08G5/0052 ,  G08G5/0069 ,  G08G5/045

Abstract: An autonomous or semi-autonomous device or vehicle, such as a drone, and method for controlling the same, the method including sensing a physical manipulation or an aspect of a physical manipulation of the autonomous or semi-autonomous device or vehicle, selecting an action and/or modifying an aspect of the action according to the sensed physical manipulation or physical manipulation aspect, and instructing the autonomous or semi-autonomous device or vehicle to perform the action.