KR20210096708A - Drone operating system - Google Patents

Drone operating system Download PDF

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KR20210096708A
KR20210096708A KR1020200009648A KR20200009648A KR20210096708A KR 20210096708 A KR20210096708 A KR 20210096708A KR 1020200009648 A KR1020200009648 A KR 1020200009648A KR 20200009648 A KR20200009648 A KR 20200009648A KR 20210096708 A KR20210096708 A KR 20210096708A
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South Korea
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drone
hangar
opened
containment
operating system
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KR1020200009648A
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Korean (ko)
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KR102317955B1 (en
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오인선
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주식회사 숨비
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/22—Ground or aircraft-carrier-deck installations installed for handling aircraft
    • B64F1/222—Ground or aircraft-carrier-deck installations installed for handling aircraft for storing aircraft, e.g. in hangars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
    • B60L53/14—Conductive energy transfer
    • B60L53/18—Cables specially adapted for charging electric vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
    • B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
    • B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
    • B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/007—Helicopter portable landing pads
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F3/00—Ground installations specially adapted for captive aircraft
    • B64F3/02—Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U80/00—Transport or storage specially adapted for UAVs
    • B64U80/80—Transport or storage specially adapted for UAVs by vehicles
    • B64U80/86—Land vehicles
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05F15/00—Power-operated mechanisms for wings
    • E05F15/60—Power-operated mechanisms for wings using electrical actuators
    • E05F15/603—Power-operated mechanisms for wings using electrical actuators using rotary electromotors
    • E05F15/632—Power-operated mechanisms for wings using electrical actuators using rotary electromotors for horizontally-sliding wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00—Type of vehicles
    • B60L2200/10—Air crafts
    • B64C2201/042—
    • B64C2201/146—
    • B64C2201/208—
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls
    • E05Y2999/00—
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/70—Energy storage systems for electromobility, e.g. batteries
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10—Technologies relating to charging of electric vehicles
    • Y02T90/14—Plug-in electric vehicles

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Power Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)
  • Power-Operated Mechanisms For Wings (AREA)

Abstract

The present invention relates to a drone operating system installed in a pickup truck having a front row seat and a rear row seat in the interior and a cargo box at the tail side with the upper part opened and used to operate a drone. The drone operating system according to the present invention comprises: a ground control device installed in the rear row seat to output a control signal for controlling flight of a drone and showing an image transmitted by the drone on a display (310); and a hangar including a hangar body having an inner room for accommodating the drone, wherein the upper part of the inner room is opened to form a path where the drone accommodated enters or exits and the lower part thereof is inserted into the cargo box to be mounted and fixed, a hangar cover mounted on the upper part of the hangar body to close or open the opened path while sliding or rotating, and an opening/closing driving unit for providing driving force needed to enable the hangar cover to perform opening/closing operation. Accordingly, the drone operating system installed in a pickup truck can be rapidly moved to some places such as mountains and a rough road, where an ordinary vehicle can't go near easily, thereby functioning as a control tower for an emergency state, an accident, and a disaster.

Description

드론운용 시스템{DRONE OPERATING SYSTEM}Drone operation system {DRONE OPERATING SYSTEM}

본 발명은 드론운용 시스템에 관한 것으로, 보다 상세하게는 실내공간에 전열좌석과 후열좌석이 마련되고 후미에 상향 개구된 적재함이 마련된 픽업트럭에 설치되어 드론을 운용하는데 이용되는 드론운용 시스템에 관한 것이다.The present invention relates to a drone operation system, and more particularly, to a drone operation system installed in a pickup truck equipped with a front row seat and a rear row seat in an indoor space and a loading box opened upward at the rear and used to operate a drone.

일반적으로 해변이나 강가 또는 산림과 같이 익수자 발생이나 산불 등의 안전사고 발생이 우려되는 장소에는 이를 감시하기 위한 감시요원을 운용하거나 CCTV를 설치하여 안전사고에 대비하고 있다. 그러나 감시영역이 넓은 경우 다수의 감시요원이나 CCTV가 운용되어야 하기 때문에 과도한 감시운용비용이 발명하는 문제점이 있었다.In general, in places where safety accidents such as drowning people or forest fires are likely to occur, such as beaches, rivers, or forests, monitoring personnel are operated to monitor them or CCTVs are installed to prepare for safety accidents. However, when the monitoring area is wide, there is a problem that excessive monitoring operation cost is invented because a large number of monitoring personnel or CCTV must be operated.

최근에는 드론에 카메라를 장착하고 이를 감시영역에서 비행시켜 촬영된 영상을 지상에서 모니터링함으로써 상대적으로 넓은 감시영역을 감시하면서도 감시운용비용을 대폭 절감할 수 있었다. 이러한 드론의 경우 지상에 위치한 지상통제장치와 RF 통신방식의 신호교환으로 비행제어되고 촬영된 영상을 지상으로 전송하는데, 종래에는 지상통제장치가 감시영역 상의 일위치에 설치된 상태에서 드론을 비행제어하는 방식으로 운용되어 드론과 지상통제장치 간의 최대 통달거리까지만 감시영역에 대한 감시영상을 촬영할 수 있었다.Recently, by installing a camera on a drone and flying it in the surveillance area to monitor the captured images from the ground, it was possible to significantly reduce the surveillance operation cost while monitoring a relatively wide surveillance area. In the case of such a drone, flight control is performed by exchanging signals of an RF communication method with a ground control device located on the ground, and the captured image is transmitted to the ground. In this way, it was possible to shoot surveillance images for the surveillance area up to the maximum distance between the drone and the ground control system.

또한, 일반적으로 드론은 내장된 배터리의 충전전원으로 비행하기 때문에 수분 내지 수십분 주기로 배터리를 교체하거나 배터리가 충분한 드론과 임무교대해야 하는데 이로 인해 감시공백이 발생할 수 밖에 없는 문제점이 있었다.In addition, in general, drones fly with the charging power of the built-in battery, so the battery must be replaced every few minutes to several tens of minutes or the mission must be shifted with a drone with sufficient battery, which inevitably causes a monitoring gap.

더불어, 상기 지상통제장치의 경우 휴대용으로 구비되어 감시영역에 설치하기 위해서는 케이스에서 각 장비들을 꺼내어 제위치에 비치하고 각 장비들을 사용가능하도록 셋팅하기까지 상당한 대기시간이 소요되었다. 더욱이 야외에서 운용되는 지상통제장치는 가격이 고가이기 때문에 장기간 감시영역에 대한 감시가 이루어지는 경우 감시시작시와 감시종료시마다 매번 지상통제장치를 셋팅하고 철거하는 절차를 반복해야 하는 번거로움이 있었다.In addition, in the case of the ground control device, since it is portable and installed in the monitoring area, it took a considerable amount of waiting time to take out each device from the case, put it in place, and set each device to be usable. Moreover, since the ground control device operated outdoors is expensive, when monitoring the monitoring area for a long period of time, it is inconvenient to repeat the procedure of setting and removing the ground control device every time the monitoring starts and at the end of the monitoring.

그리고, 종래에는 감시영역을 촬영한 감시영상을 지상통제장치에 장착되거나 케이블 연결된 디스플레이를 통해서만 모니터링할 수 있어 각 감시영역에서 획득된 감시영상에 대한 통합적인 모니터링이나 관리가 제한되는 문제점이 있었다.And, in the related art, there is a problem in that the integrated monitoring or management of the surveillance images acquired in each surveillance area is limited because the surveillance image captured in the surveillance area can be monitored only through the display mounted on the ground control device or connected to the cable.

등록특허공보 제10-1535401호(2015.07.02), 드론방식 구명장비 투하장치.Registered Patent Publication No. 10-1535401 (2015.07.02), Drone-type lifesaving equipment delivery device.

본 발명은 상술한 문제점을 해결하기 위하여 창출된 것으로, 본 발명의 목적은 드론을 운용하기 위한 시스템이 픽업트럭에 설치되어 산악 및 험로 등 일반 차량의 접근이 쉽지 않은 곳까지 신속하게 이동 가능하여 응급, 재난 재해의 컨트롤 타워의 임무를 수행할 수 있는 드론운용 시스템을 제공하는 것에 있다.The present invention was created to solve the above-mentioned problems, and an object of the present invention is to enable a system for operating a drone to be installed in a pickup truck so that it can be quickly moved to places that are not easy to access by general vehicles, such as mountains and rough roads, so that emergency , to provide a drone operation system that can perform the mission of a control tower in disasters and disasters.

본 발명의 특징에 따르면, 실내공간에 전열좌석(11)과 후열좌석(12)이 마련되고 후미에 상향 개구된 적재함(13)이 마련된 픽업트럭(10); 상기 후열좌석(12)에 배치되고 드론(20)을 비행제어하기 위한 제어신호를 출력하고 드론(20)으로부터 전송되는 영상을 디스플레이(310)에 표시하는 지상통제장치(300); 및 드론(20)을 수용하기 위한 내부공간이 마련되고 상기 내부공간의 상부는 개구되어 수용된 드론(20)이 출입하는 통로를 형성하며 하부가 상기 적재함(13)에 고정장착되는 격납본체(110)와, 상기 격납본체(110)의 상부에 장착되고 슬라이딩하거나 회동하면서 개구된 통로를 개폐하는 격납커버(120) 및, 상기 격납커버(120)가 개폐동동작하는데 필요한 구동력을 제공하는 개폐구동부(130)를 포함하는 드론격납고(100);를 포함하는 드론운용 시스템이 제공된다.According to a feature of the present invention, a pickup truck 10 having a front row seat 11 and a rear row seat 12 provided in an indoor space and a loading box 13 opened upward at the rear; a ground control device 300 disposed in the rear row seat 12 and outputting a control signal for flight control of the drone 20 and displaying an image transmitted from the drone 20 on the display 310; And an inner space for accommodating the drone 20 is provided, the upper portion of the inner space is opened to form a passage through which the accommodated drone 20 enters and exits, and the lower portion is fixedly mounted on the loading box 13. The containment body 110 and a containment cover 120 mounted on the upper portion of the containment body 110 and sliding or rotating to open and close the opened passage, and an opening/closing drive unit 130 that provides a driving force necessary for the containment cover 120 to open and close. ), including a drone hangar 100; is provided a drone operating system comprising.

본 발명의 다른 특징에 따르면, 상기 드론격납고(100)는, 상기 드론(20)의 중앙부에 배치되고 수직으로 하향 연장된 수직바(240) 및, 상기 격납본체(110) 내에 수평배치되며 중앙부에는 상하로 개구되어 상기 수직바(240)가 하향 관통 삽입되기 위한 삽입공(212)이 형성되고 상기 삽입공(212)의 둘레에는 상부로 갈수록 점차 직경이 확대되는 형상으로 이루어진 가이드홈(211)이 형성되어 가이드홈(211)의 표면에 접촉된 수직바(240)의 하단이 삽입공(212)의 상단을 향해 슬라이딩하도록 가이드하는 안착판(210)을 더 포함하는 것을 특징으로 하는 픽업트럭용 드론운용 시스템이 According to another feature of the present invention, the drone hangar 100 is a vertical bar 240 disposed in the center of the drone 20 and extending vertically downward, and is horizontally disposed in the containment body 110 and in the central part The vertical bar 240 is opened up and down to form an insertion hole 212 through which the vertical bar 240 is downwardly inserted, and a guide groove 211 is formed around the insertion hole 212, the diameter of which gradually increases toward the top. The drone for pickup truck, characterized in that it further includes a seating plate 210 that guides the lower end of the vertical bar 240 that is formed and in contact with the surface of the guide groove 211 to slide toward the upper end of the insertion hole 212 . the operating system

본 발명의 또 다른 특징에 따르면, 상기 드론격납고(100)는, 상기 격납본체(110) 내에서 상하로 연장배치되어 상기 안착판(210)의 승하강 경로를 형성하는 승강가이드바(220) 및, 상기 안착판(210)이 승강가이드바(220)를 따라 승하강하는데 필요한 구동력을 제공하는 승강구동부(230)를 더 포함하는 것을 특징으로 하는 드론운용 시스템이 제공된다.According to another feature of the present invention, the drone hangar 100 is arranged extending up and down in the containment body 110 to form an elevating path of the seating plate 210. An elevating guide bar 220 and , There is provided a drone operating system, characterized in that it further comprises a lift driving unit 230 for providing a driving force necessary for the seating plate 210 to move up and down along the elevating guide bar 220 .

한편. 본 발명의 또 다른 특징에 따르면, 상기 드론격납고(100)는, 전기에너지를 생성하는 발전기(420) 및, 상기 격납본체(110)의 내부에 배치되어 발전기(420)로부터 생성된 전기에너지를 공급받으며, 일측은 드론(20)에 연결되고 타측은 내부에 권취되는 전원케이블(412)이 구비되어 발전기(420)에서 생성된 전기에너지를 전원케이블(412)을 통해 드론(20)에 공급하는 유선전원공급기(410)를 더 포함하는 것을 특징으로 하는 픽업트럭용 드론운용 시스템이 제공된다.Meanwhile. According to another feature of the present invention, the drone hangar 100 is a generator 420 that generates electrical energy, and is disposed inside the containment body 110 to supply the electrical energy generated from the generator 420 . Received, one side is connected to the drone 20 and the other side is provided with a power cable 412 wound inside, so that the electric energy generated by the generator 420 is supplied to the drone 20 through the power cable 412. Wired There is provided a drone operating system for a pickup truck, characterized in that it further comprises a power supply (410).

이상에서와 같이 본 발명에 의하면,As described above, according to the present invention,

첫째, 후열좌석(12)에 배치되는 지상통제장치(300)는 드론(20)을 비행제어하기 위한 제어신호를 출력하고 드론(20)으로부터 전송되는 영상을 디스플레이(310)에 표시하며, 격납고(100)는 드론(20)을 수용하기 위한 내부공간이 마련되고 상기 내부공간의 상부는 개구되어 수용된 드론(20)이 출입하는 통로를 형성하며 하부가 적재함(13)에 삽입되어 고정장착되는 격납본체(110)와, 상기 격납본체(110)의 상부에 장착되고 슬라이딩하거나 회동하면서 개구된 통로를 개폐하는 격납커버(120) 및, 상기 격납커버(120)가 개폐동동작하는데 필요한 구동력을 제공하는 개폐구동부(130)를 포함하는 것과 같이, 드론(20)을 운용하기 위한 시스템이 픽업트럭(10)에 설치되어 산악 및 험로 등 일반 차량의 접근이 쉽지 않은 곳까지 신속하게 이동 가능하여 재난 재해의 컨트롤 타워의 임무를 수행할 수 있다. 또한, 드론(20)이 수용된 격납고(100)의 상부를 자동으로 개폐할 수 있어 필요시 드론(20)의 신속한 전개 및 철수가 가능하며 드론(20)을 외부로부터 안전하게 보호한 상태로 이동할 수 있다.First, the ground control device 300 disposed in the rear row seat 12 outputs a control signal for flight control of the drone 20 and displays the image transmitted from the drone 20 on the display 310, and the hangar ( 100) is provided with an internal space for accommodating the drone 20, the upper part of the internal space is opened to form a passage through which the accommodated drone 20 enters and exits, and the lower part is inserted into the loading box 13 to be fixedly mounted. (110), a containment cover 120 mounted on the upper portion of the containment body 110 and sliding or rotating to open and close the opened passage, and an opening/closing opening providing a driving force necessary for the containment cover 120 to open and close. As including the eastern part 130, a system for operating the drone 20 is installed in the pickup truck 10 so that it can be quickly moved to places that are not easy to access by general vehicles, such as mountains and rough roads, so that the control of disasters and disasters You can do the tower's mission. In addition, the upper part of the hangar 100 in which the drone 20 is accommodated can be automatically opened and closed, so that the drone 20 can be quickly deployed and withdrawn when necessary, and the drone 20 can be safely moved from the outside. .

둘째, 수직바(240)는 드론(20)의 중앙부에 배치되고 수직으로 하향 연장되며, 안착판(210)은 격납본체(110) 내에 수평배치되며 중앙부에는 상하로 개구되어 상기 수직바(240)가 하향 관통 삽입되기 위한 삽입공(212)이 형성되고 안착판(210) 상에서 상기 삽입공(212)의 둘레에는 상부로 갈수록 점차 직경이 확대되는 형상으로 이루어진 가이드홈(211)이 형성되어 가이드홈(211)의 표면에 접촉된 수직바(240)의 하단이 삽입공(212)의 상단을 향해 슬라이딩하도록 가이드함으로써, 가이드홈(211)의 표면에 접촉된 수직바(240)의 하단이 삽입공(212)의 상단을 향해 슬라이딩하도록 가이드하여 안착판(210)에 드론(20)이 착륙하거나 착륙한 드론(20)이 이륙할 때 강풍이 불거나 픽업트럭(10)에 큰 움직임이 가해지더라도 안정적으로 착륙 및 이륙이 가능할 수 있다.Second, the vertical bar 240 is disposed in the center of the drone 20 and extends vertically downward, and the seating plate 210 is horizontally disposed in the containment body 110 and is opened up and down in the center of the vertical bar 240 . An insertion hole 212 for downward penetration is formed, and a guide groove 211 having a shape that gradually increases in diameter toward the top is formed around the insertion hole 212 on the seating plate 210 to form a guide groove. By guiding the lower end of the vertical bar 240 in contact with the surface of the 211 to slide toward the upper end of the insertion hole 212 , the lower end of the vertical bar 240 in contact with the surface of the guide groove 211 is the insertion hole. Stable even when a strong wind blows or a large movement is applied to the pickup truck 10 when the drone 20 is landed on the landing plate 210 by guiding it to slide toward the top of the 212 or the landed drone 20 takes off. landing and take-off may be possible.

셋째, 승강가이드바(220)는 적재함(13) 내에서 상하로 연장배치되어 상기 안착판(210)의 승하강 경로를 형성하고, 승강구동부(230)는 안착판(210)이 승강가이드바(220)를 따라 승하강하는데 필요한 구동력을 제공함으로써, 드론(20)이 이륙할때 주변 구성품과 충돌하는 것을 방지할 수 있으며 격납고(100)의 격납커버(120)를 슬림하게 할 수 있다.Third, the elevating guide bar 220 is vertically extended in the loading box 13 to form an elevating path of the mounting plate 210, and the elevating drive unit 230 is the mounting plate 210 is the elevating guide bar ( By providing the driving force required to ascend and descend along 220 , it is possible to prevent the drone 20 from colliding with surrounding components when taking off, and to make the containment cover 120 of the hangar 100 slim.

넷째, 발전기(420)는 전기에너지를 생성하고, 유선전원공급기(410)는 상기 발전기(420)로부터 생성된 전기에너지를 공급받으며 상기 적재함(13) 내부에 배치되고 일측은 드론(20)에 연결되며 타측은 내부에 권취되는 전원케이블(412)이 구비되어 발전기(420)에서 생성된 전기에너지를 전원케이블(412)을 통해 드론(20)에 공급함으로써, 비행중에 지속적인 전원공급이 가능하여 장시간 감시 관제 임무를 수행할 수 있다.Fourth, the generator 420 generates electrical energy, and the wired power supply 410 receives the electrical energy generated from the generator 420 and is disposed inside the loading box 13 , and one side is connected to the drone 20 . The other side is provided with a power cable 412 wound therein, and by supplying the electric energy generated by the generator 420 to the drone 20 through the power cable 412, continuous power supply during flight is possible and monitoring for a long time. Able to perform control tasks.

도 1은 본 발명의 바람직한 실시예에 따른 드론격납고가 폐쇄된 상태를 나타낸 사시도,
도 2는 본 발명의 바람직한 실시예에 따른 드론격납고가 개방된 상태를 나타낸 사시도,
도 3은 본 발명의 바람직한 실시예에 따른 드론격납고의 내부구성을 나타낸 측면도,
도 4는 본 발명의 바람직한 실시예에 따른 드론운용 시스템이 픽업트럭에 설치된 상태를 나타낸 평면도,
도 5는 본 발명의 바람직한 실시예에 따른 드론격납고가 픽업트럭의 적재함에 설치되는 구성을 나타낸 측면도,
도 6은 본 발명의 바람직한 실시예에 따른 드론격납고의 개폐구조를 나타낸 사시도,
도 7은 본 발명의 바람직한 실시예에 따른 격납커버의 저면 구성을 나타낸 사시도,
도 8은 본 발명의 바람직한 실시예에 따른 드론격납고의 개폐구조를 나타낸 정단면도,
도 9는 본 발명의 바람직한 실시예에 따른 드론격납고가 폐쇄된 상태를 나타낸 측단면도,
도 10은 본 발명의 바람직한 실시예에 따른 드론격납고가 개방된 상태를 나타낸 측단면도,
도 11 및 도 12는 본 발명의 바람직한 실시예에 따른 드론격납고의 내부구성을 나타낸 측단면도,
도 13은 본 발명의 바람직한 실시예에 따른 안착판의 구성을 나타낸 사시도,
도 14 및 도 15는 본 발명의 바람직한 실시예에 따른 안착판의 오목골 구조를 나타낸 측단면도,
도 16은 본 발명의 바람직한 실시예에 따른 전자석에 의해 안착판에 안착한 드론이 록킹되는 구성을 나타낸 측단면도,
도 17은 본 발명의 바람직한 실시예에 따른 드론격납고의 유선전원공급 구조를 나타낸 측단면도,
도 18은 본 발명의 바람직한 실시예에 따른 유선전원공급기의 구성을 나타낸 개략도이다.1 is a perspective view showing a closed state of a drone hangar according to a preferred embodiment of the present invention;
2 is a perspective view showing an open state of a drone hangar according to a preferred embodiment of the present invention;
3 is a side view showing the internal configuration of a drone hangar according to a preferred embodiment of the present invention;
4 is a plan view showing a state in which a drone operating system according to a preferred embodiment of the present invention is installed in a pickup truck;
5 is a side view showing a configuration in which a drone hangar according to a preferred embodiment of the present invention is installed in a loading box of a pickup truck;
6 is a perspective view showing the opening and closing structure of a drone hangar according to a preferred embodiment of the present invention;
7 is a perspective view showing a bottom configuration of a containment cover according to a preferred embodiment of the present invention;
8 is a front sectional view showing the opening and closing structure of a drone hangar according to a preferred embodiment of the present invention;
9 is a side cross-sectional view showing a closed state of a drone hangar according to a preferred embodiment of the present invention;
10 is a side cross-sectional view showing an open state of a drone hangar according to a preferred embodiment of the present invention;
11 and 12 are side cross-sectional views showing the internal configuration of a drone hangar according to a preferred embodiment of the present invention;
13 is a perspective view showing the configuration of a seating plate according to a preferred embodiment of the present invention;
14 and 15 are side cross-sectional views showing the concave structure of the seating plate according to a preferred embodiment of the present invention;
16 is a side cross-sectional view showing a configuration in which a drone seated on a seating plate by an electromagnet according to a preferred embodiment of the present invention is locked;
17 is a side cross-sectional view showing a wired power supply structure of a drone hangar according to a preferred embodiment of the present invention;
18 is a schematic diagram showing the configuration of a wired power supply according to a preferred embodiment of the present invention.

상술한 본 발명의 목적, 특징들 및 장점은 다음의 상세한 설명을 통하여 보다 분명해질 것이다. 이하, 본 발명의 바람직한 실시예를 첨부한 도면에 의거하여 설명하면 다음과 같다.The objects, features and advantages of the present invention described above will become more apparent through the following detailed description. Hereinafter, preferred embodiments of the present invention will be described based on the accompanying drawings.

본 발명의 바람직한 실시예에 따른 드론운용 시스템은 드론(20)의 비행제어, 운반 및 보관과 같이 드론(20)을 운용하는데 이용되는 시스템으로서, 픽업트럭(10), 지상통제장치(300) 및 드론격납고(100)를 포함한다.The drone operating system according to a preferred embodiment of the present invention is a system used to operate the drone 20 such as flight control, transport and storage of the drone 20, and includes a pickup truck 10, a ground control device 300 and It includes a drone hangar (100).

먼저, 상기 픽업트럭(10)은 시스템 운용에 필요한 기동력을 제공하는 차량으로서, 실내공간에 전열좌석(11)과 후열좌석(12)이 마련되고 후미에 상향 개구된 적재함(13)이 마련된다. 이와 같이, 드론(20)을 운용하기 위한 시스템이 픽업트럭(10)에 설치되어 산악 및 험로 등 일반 차량의 접근이 쉽지 않은 곳까지 신속하게 이동 가능하여 응급, 재난 재해의 컨트롤 타워의 임무를 효과적으로 수행할 수 있다.First, the pickup truck 10 is a vehicle that provides maneuverability necessary for system operation. A front row seat 11 and a rear row seat 12 are provided in an indoor space, and a loading box 13 opened upward at the rear is provided. In this way, the system for operating the drone 20 is installed in the pickup truck 10 so that it can be quickly moved to places that are not easy to access by general vehicles, such as mountains and rough roads, so that the mission of the control tower in emergency and disaster disasters can be effectively performed. can be done

상기 지상통제장치(300)는 드론(20)을 비행제어하기 위한 조종수단으로서 상기 후열좌석(12)에 배치되고 드론(20)을 비행제어하기 위한 제어신호를 출력하며 드론(20)으로부터 전송되는 영상을 디스플레이(310)에 표시한다.The ground control device 300 is a control means for flight control of the drone 20, which is disposed in the rear row seat 12, outputs a control signal for flight control of the drone 20, and is transmitted from the drone 20 An image is displayed on the display 310 .

상기 드론격납고(100)는 드론(20)을 수용하는 함체로서 도 1 내지 도 5에 도시된 바와 같이 격납본체(110), 격납커버(120) 및 개폐구동부(130)를 포함한다. 또한, 도 5에 도시된 바와 같이 후열좌석(12)에는 지상통제장치(300)를 운용하는데 필요한 각종 통신장치 및 제어장치 등을 수납하는 수납프레임(330)이 구비되고 이 수납프레임(330)의 상부에 디스플레이(310)가 거치되어 협소한 실내공간을 효율적으로 사용할 수 있다.The drone hangar 100 includes a containment body 110 , a containment cover 120 and an opening/closing drive unit 130 as shown in FIGS. 1 to 5 as a housing for accommodating the drone 20 . In addition, as shown in FIG. 5 , the rear seat 12 is provided with a storage frame 330 for accommodating various communication devices and control devices necessary for operating the ground control device 300 , and Since the display 310 is mounted on the upper part, it is possible to efficiently use a narrow indoor space.

상기 격납본체(110)는 드론(20)을 수용하기 위한 내부공간이 마련되고 상기 내부공간의 상부는 개구되어 수용된 드론(20)이 출입하는 통로를 형성하며 하부가 상기 적재함(13)에 삽입되어 고정장착된다.The containment body 110 has an internal space for accommodating the drone 20, and the upper part of the internal space is opened to form a passage through which the accommodated drone 20 enters and exits, and the lower part is inserted into the loading box 13. is fixedly mounted

여기서, 도 3에 도시된 바와 같이 상기 격납본체(110)는 복수의 골조프레임(111)이 사각형태로 조립되어 골조를 형성하고 각 골조프레임(111) 사이에 장착되어 측부를 커버하는 측판으로 이루어지며, 골조프레임(111)의 하부만이 적재함(13)에 삽입되어 고정되거나 필요시 측판까지 함께 적재함(13)에 삽입되어 고정될 수 있다.Here, as shown in FIG. 3 , the containment body 110 is a plurality of frame frames 111 assembled in a rectangular shape to form a frame, and is mounted between each frame frame 111 to cover the side parts. , and only the lower part of the frame frame 111 may be inserted and fixed in the loading box 13 or inserted into the loading box 13 together to the side plate if necessary.

상기 격납커버(120)는 격납본체(110)의 상부에 장착되고 슬라이딩하거나 회동하면서 개구된 통로를 개폐한다. 여기서, 격납커버(120)는 격납본체(110)의 상부에 수평배치된 상태에서 일측단부가 격납본체(110)에 힌지결합되어 여닫이 방식으로 개폐될 수 있으며, 도면에서와 같이 상기 격납커버(120)는 격납본체(110)의 상부에서 전후방으로 슬라이딩하면서 격납본체(110)의 개구된 통로를 개폐할 수 있다. 이하에서는 격납커버(120)가 전후방으로 슬라이딩하면서 격납본체(110)의 통로를 개폐하는 것을 예시하여 설명하기로 한다.The containment cover 120 is mounted on the upper portion of the containment body 110 and opens and closes the opened passage while sliding or rotating. Here, the containment cover 120 can be opened and closed in an opening and closing manner by being hinged to the containment body 110 in a state in which the containment cover 120 is horizontally disposed on the upper side of the containment body 110 , and as shown in the drawing, the containment cover 120 ) may open and close the opened passage of the containment body 110 while sliding forward and backward from the upper portion of the containment body 110 . Hereinafter, an example in which the containment cover 120 opens and closes the passage of the containment body 110 while sliding forward and backward will be described.

상기 개폐구동부(130)는 격납커버(120)가 개폐동작하는데 필요한 구동력을 제공한다. 따라서, 운전자나 드론조종자가 픽업트럭(10) 내부에서 격납커버(120)를 자동 개폐시킬 수 있다.The opening/closing driving unit 130 provides a driving force necessary for opening and closing the containment cover 120 . Accordingly, a driver or a drone operator can automatically open and close the containment cover 120 inside the pickup truck 10 .

한편, 상기 픽업트럭(10)의 루프(14) 상에서 후열좌석(12)의 상부 위치에는 수평배치되는 연장부(112)가 구비되고, 상기 개폐구동부(130)는 연장부(112)의 상부에 배치되어 격납커버(120)가 전후방으로 슬라이딩하는데 필요한 구동력을 제공함으로써, 격납커버(120)가 전방으로 슬라이딩하면서 후방에 배치된 격납본체(110)의 개구된 통로공간을 충분하게 확보하면서 동시에 전방으로 슬라이딩된 격납커버(120)가 자중에 의해 하부로 쳐지면서 훼손되거나 전열좌석(11)에 착석한 운전자의 시야를 가리는 것을 방지할 수 있다.On the other hand, on the roof 14 of the pickup truck 10 , an extension part 112 arranged horizontally is provided at an upper position of the rear seat 12 , and the opening/closing driving part 130 is located on the upper part of the extension part 112 . By providing a driving force required for the containment cover 120 to slide forward and backward, the containment cover 120 slides forward while sufficiently securing the open passage space of the containment body 110 arranged at the rear while simultaneously moving forward. It is possible to prevent the sliding containment cover 120 from being damaged by being struck downward by its own weight or from blocking the view of the driver seated in the front row seat 11 .

여기서, 도 6 내지 도 8에 도시된 바와 같이, 상기 격납커버(120)는 저면의 중앙에 전후방으로 연장되고 연장된 길이를 따라 하부에 기어가 연이어 형성된 랙바(121)가 배치되고, 저면의 양측에는 전후방으로 연장된 가이드바(122)가 각각 배치되며, 상기 개폐구동부(130)는, 회전력을 제공하는 구동모터(131)와, 구동모터(131)의 구동축에 축결된 구동기어(132)와, 상기 구동기어(132)에 연결되어 수평배치된 회전축(135)을 회전시키는 피동기어(133)와, 상기 회전축(135) 상에 축결되며 상기 랙바(121)의 기어와 맞물려 회전하는 피니언기어(134) 및, 각 가이드바(122)와 대응되는 위치에 수평축으로 회전가능하게 배치되어 가이드바(122)의 저면을 지지하는 지지롤러(136)를 포함할 수 있다.Here, as shown in FIGS. 6 to 8, the containment cover 120 extends forward and backward in the center of the bottom surface and the rack bars 121 in which gears are continuously formed in the lower part along the extended length are disposed, both sides of the bottom surface Each of the guide bars 122 extending in the front and rear are arranged, and the opening/closing driving unit 130 includes a driving motor 131 providing a rotational force, and a driving gear 132 condensed on the driving shaft of the driving motor 131 and , a driven gear 133 connected to the driving gear 132 to rotate the horizontally arranged rotation shaft 135, and a pinion gear condensed on the rotation shaft 135 and rotating in engagement with the gear of the rack bar 121 ( 134) and a support roller 136 that is rotatably disposed on a horizontal axis at a position corresponding to each guide bar 122 to support the bottom surface of the guide bar 122 .

따라서, 구동모터(131)가 정회전 구동하면 구동기어(132)가 일방향으로 회전하면서 피동기어(133)를 회전시키고 회전축(135)이 함께 회전하면서 피니언기어(134)를 회전시켜 이 피니언기어(134)에 치합되어 있는 랙바(121)가 전방으로 이동하면서 도 10과 같이 격납커버(120)가 전방으로 슬라이딩 이동하여 격납본체(110)의 통로를 개방시키게 된다. 이때, 격납커버(120)의 하중은 양측의 가이드바(122)를 통해 지지롤러(136)에 지지되어 분산되기 때문에 보다 작은 구동력으로도 격납커버(120)를 이동시킬 수 있다.Therefore, when the driving motor 131 is driven to rotate forward, the driving gear 132 rotates in one direction to rotate the driven gear 133, and the rotation shaft 135 rotates with the pinion gear 134 to rotate the pinion gear ( As the rack bar 121 meshed with 134) moves forward, the containment cover 120 slides forward as shown in FIG. 10 to open the passage of the containment body 110 . At this time, since the load of the containment cover 120 is supported and distributed by the support rollers 136 through the guide bars 122 on both sides, it is possible to move the containment cover 120 even with a smaller driving force.

또한, 이와 같이 격납커버(120)가 개방된 상태에서 구동모터(131)가 역회전 구동하면 구동기어(132)가 타방향으로 회전하면서 피동기어(133)를 회전시키고 회전축(135)이 함께 회전하면서 피니언기어(134)를 회전시켜 랙바(121)가 후방으로 이동하면서 도 9와 같이 격납커버(120)가 후방으로 슬라이딩이동하여 격납본체(110)의 통로를 폐쇄시키게 된다.In addition, when the driving motor 131 is driven to rotate in the reverse direction in the state in which the containment cover 120 is opened as described above, the driving gear 132 rotates in the other direction to rotate the driven gear 133 and the rotating shaft 135 rotates together. While the pinion gear 134 is rotated, the rack bar 121 moves rearward, and the containment cover 120 slides backward as shown in FIG. 9 to close the passage of the containment body 110 .

더불어, 도 6에서와 같이 상기 격납본체(110)의 상단 폭방향(W) 양측에는 각각 전후방(L)으로 연장되게 수평배치되는 가이드레일(113)이 배치되고, 상기 격납커버(120) 상에서 각 가이드레일(113)과 대응되는 위치에는 전후방(L)으로 연장되게 수평배치되어 가이드레일(113)에 지지되면서 전후방으로 슬라이딩 이동하는 슬라이딩바(123)가 배치됨으로써, 격납커버(120)가 자중에 의해 하부로 쳐지는 현상으로 더욱 견고하게 지지할 수 있다. In addition, as shown in FIG. 6 , guide rails 113 horizontally arranged to extend in the front and rear directions (L) are disposed on both sides of the upper end in the width direction (W) of the containment body (110), and on the containment cover (120), each At a position corresponding to the guide rail 113, a sliding bar 123 that is horizontally arranged to extend forward and backward (L) and slides forward and backward while being supported by the guide rail 113 is disposed, so that the containment cover 120 loses its own weight. It can be supported more firmly by the phenomenon of being sagged downward.

상술한 바와 같은 격납본체(110), 격납커버(120) 및 개폐구동부(130)의 조합된 구성을 통해 드론(20)이 수용된 격납고(100)의 상부를 자동으로 개폐할 수 있어 필요시 드론(20)의 신속한 전개 및 철수가 가능하며 드론(20)을 외부로부터 안전하게 보호한 상태로 이동할 수 있다.Through the combined configuration of the containment body 110, the containment cover 120 and the opening/closing drive unit 130 as described above, the upper part of the hangar 100 in which the drone 20 is accommodated can be automatically opened and closed, so that when necessary, the drone ( 20) can be rapidly deployed and withdrawn, and the drone 20 can be safely moved while being protected from the outside.

한편, 상기 드론격납고(100)는 도 9 내지 도 13에 도시된 바와 같이 수직바(240) 및 안착판(210)을 더 포함한다.Meanwhile, the drone hangar 100 further includes a vertical bar 240 and a seating plate 210 as shown in FIGS. 9 to 13 .

상기 수직바(240)는 드론(20)의 중앙부에 배치되고 수직으로 하향 연장된다.The vertical bar 240 is disposed in the center of the drone 20 and extends vertically downward.

상기 수직바(240)는 상하로 길이가 조절되는 신축구조로 이루어져 드론(20)의 비행시에는 최소길이로 줄어들어 외부장애물과 간섭되지 않도록 하고 착륙시에는 하부방향으로 길이가 길어져 가이드될 수 있도록 구비되는 것이 바람직하다. 또한, 상기 수직바(240)는 내부에 중공이 형성되어 이 중공에 전원케이블(412)이 관통삽입되어 드론(20)의 전원회로에 연결될 수 있다. 따라서, 드론(20)이 안착판(210)에 착륙시 삽입공(212)을 통해 외부로 권출되는 전원케이블(412)이 줄어들게 되면 수직바(240)의 단부가 삽입공(212)을 향해 당겨지게 되면서 삽입공(212)을 관통하도록 가이드할 수 있다.The vertical bar 240 is made of a telescopic structure whose length is adjusted up and down, so that it is reduced to a minimum length during flight of the drone 20 so that it does not interfere with external obstacles, and is lengthened in the lower direction during landing so that it can be guided It is preferable to be In addition, the vertical bar 240 has a hollow formed therein, and the power cable 412 is inserted through the hollow to be connected to the power circuit of the drone 20 . Therefore, when the drone 20 lands on the seating plate 210 , when the power cable 412 unwound to the outside through the insertion hole 212 is reduced, the end of the vertical bar 240 is pulled toward the insertion hole 212 . It can be guided so as to penetrate the insertion hole 212 while being removed.

상기 안착판(210)은 상기 적재함(13) 내에 수평배치되며 중앙부에는 상하로 개구되어 상기 가이드바(122)가 하향 관통 삽입되기 위한 삽입공(212)이 형성되고 상기 안착판(210) 상에서 삽입공(212)의 둘레에는 상부로 갈수록 점차 직경이 확대되는 형상으로 이루어진 가이드홈(211)이 형성되어 가이드홈(211)의 표면에 접촉된 가이드바(122)의 하단이 삽입공(212)의 상단을 향해 슬라이딩하도록 가이드한다. 또한, 상기 삽입공(212)에는 일정길이로 하향 연장된 연장관(219)이 형성되어 삽입된 수직바(240)가 수직방향으로 하향 하도록 가이드할 수 있다.The seating plate 210 is horizontally arranged in the loading box 13 and is opened up and down in the central portion to form an insertion hole 212 for the guide bar 122 to be inserted downwardly, and is inserted on the seating plate 210 . A guide groove 211 having a shape gradually increasing in diameter is formed around the ball 212 so that the lower end of the guide bar 122 in contact with the surface of the guide groove 211 is the insertion hole 212 . Guide it to slide towards the top. In addition, an extension tube 219 extending downward to a predetermined length may be formed in the insertion hole 212 to guide the inserted vertical bar 240 downward in the vertical direction.

이러한 수직바(240)와 안착판(210)의 조합된 구성으로 가이드홈(211)의 표면에 접촉된 가이드바(122)의 하단이 삽입공(212)의 상단을 향해 슬라이딩하도록 가이드하여 안착판(210)에 드론(20)이 착륙하거나 착륙한 드론(20)이 이륙할 때 강풍이 불거나 픽업트럭(10)에 큰 움직임이 가해지더라도 안정적으로 착륙 및 이륙이 가능할 수 있다.By guiding the lower end of the guide bar 122 in contact with the surface of the guide groove 211 to slide toward the upper end of the insertion hole 212 in the combined configuration of the vertical bar 240 and the seating plate 210 , the seating plate Even if a strong wind blows or a large motion is applied to the pickup truck 10 when the drone 20 is landed on the 210 or the landed drone 20 takes off, landing and take-off may be stably possible.

여기서, 상기 적재함(13) 내에서 상하로 연장배치되는 승강가이드바(220)는 상기 안착판(210)의 승하강 경로를 형성하고, 승강구동부(230)는 상기 안착판(210)이 승강가이드바(220)를 따라 승하강하는데 필요한 구동력을 제공함으로써, 드론(20)이 이륙할때 격납본체 통로와 같은 주변 구성품과 충돌하는 것을 방지할 수 있으며 격납고(100)의 격납커버(120)를 슬림하게 할 수 있다. 상기 승강가이드바(220)는 복수 개의 프레임이 신축되면서 길이가 조절되는 구조로 이루어져 승강구동부(230)의 구동력으로 신축동작한다. 상기 승강구동부(230)로는 도면에서와 같이 공압이나 유압의 액추에이터를 이용할 수 있으며 이 밖에 구동모터를 이용하여 승강구동에 필요한 구동력을 제공할 수도 있다.Here, the elevating guide bar 220 vertically extended in the loading box 13 forms an elevating path of the seating plate 210 , and the elevating drive unit 230 is the seating plate 210 is the elevating guide. By providing the driving force required to ascend and descend along the bar 220, it is possible to prevent the drone 20 from colliding with surrounding components such as the containment passageway when taking off, and the containment cover 120 of the hangar 100 can be slimmed down. can do it The elevating guide bar 220 has a structure in which the length is adjusted as a plurality of frames are stretched and contracted, so that the elevating guide bar 220 expands and contracts with the driving force of the elevating driving unit 230 . As the elevating driving unit 230, a pneumatic or hydraulic actuator may be used as shown in the drawing, and in addition, a driving force required for elevating driving may be provided by using a driving motor.

또한, 도 14 및 도 15에 도시된 바와 같이 상기 가이드홈(211)의 내면에는 평단면이 가이드홈(211)의 중앙을 향해 측방으로 개구된 호형상이면서 상기 가이드홈(211)의 상단에서 하단으로 상향 연장된 다수의 오목골(215)이 둘레를 따라 연이어 형성되되, 상기 가이드홈(211)의 둘레를 따라 각 오목골(215)이 밀착되게 연이어 배치되면서 인접된 두 오목골(215) 사이에는 뾰족하게 융기된 골구획산(214)이 형성됨으로써, 드론(20)이 하강하면서 수직바(240)의 하단이 가이드홈(211)의 내면과 접촉하면서 측방으로 슬립되어 드론(20)이 전복되는 것을 미연에 방지할 수 있다.In addition, as shown in FIGS. 14 and 15 , the inner surface of the guide groove 211 has a flat cross-section in the shape of an arc opened laterally toward the center of the guide groove 211 and from the top to the bottom of the guide groove 211 . A plurality of concave troughs 215 extending upwardly are formed successively along the periphery, and each concave trough 215 is arranged in close contact with each other along the perimeter of the guide groove 211 between two adjacent concave troughs 215 . A sharply raised bone compartment 214 is formed, so that as the drone 20 descends, the lower end of the vertical bar 240 comes into contact with the inner surface of the guide groove 211 and slips laterally, causing the drone 20 to overturn. can be prevented in advance.

더불어, 도 14 및 도 16에 도시된 바와 같이 상기 수직바(240)는 자성체 재질로 이루어지며 둘레에는 측방으로 오목하게 함몰된 고정홈(243)이 형성되고, 상기 삽입공(212) 상에서 삽입된 수직바(240)의 고정홈(243)과 대응되는 위치에는 측방으로 개구된 인출공(216)이 형성되며, 상기 삽입공(212)의 둘레에는 인출공(216)을 통해 측방으로 인출 가능하게 장착되는 전자석(217)이 배치되고, 상기 전자석(217)은 탄성부재(218)에 의해 외측방으로 당겨져 인출공(216)의 외부에 배치되다 구동전원이 인가되어 자기장이 형성되면 인출공(216)을 통해 상기 수직바(240)에 부착되면서 고정홈(243)에 삽입되어 수직바(240)의 삽입된 상태를 선택적으로 록킹하여 안착판(210)에 착륙한 드론(20)이 강풍이나 외부 가압에 의해 이탈되는 것을 방지할 수 있다.In addition, as shown in FIGS. 14 and 16 , the vertical bar 240 is made of a magnetic material, and a fixing groove 243 concave laterally is formed around it, and is inserted on the insertion hole 212 . At a position corresponding to the fixing groove 243 of the vertical bar 240, a laterally open withdrawal hole 216 is formed, and around the insertion hole 212, it can be drawn out laterally through the extraction hole 216. A mounted electromagnet 217 is disposed, and the electromagnet 217 is pulled outward by the elastic member 218 to be disposed outside the drawing hole 216. When driving power is applied to form a magnetic field, the drawing hole 216 is formed. ) while being attached to the vertical bar 240 while being inserted into the fixing groove 243 to selectively lock the inserted state of the vertical bar 240, the drone 20 that landed on the seating plate 210 is not exposed to strong winds or the outside. It can be prevented from being separated by pressurization.

한편, 상기 드론격납고(100)는 도 11, 도 12 및 도 17에 도시된 바와 같이 발전기(420) 및 유선전원공급기(410)를 더 포함한다.On the other hand, the drone hangar 100 further includes a generator 420 and a wired power supply 410 as shown in FIGS. 11, 12 and 17 .

상기 발전기(420)는 전기에너지를 생성한다. 여기서 상기 발전기(420)로 픽업트럭(10)의 동력계통에 연결되어 제공되는 회전력으로 전기에너지를 생성하는 PTO(Power Take Off) 발전기를 이용함으로써, 발전기를 구동하는데 필요한 화석연료를 대폭 절감할 수 있으며 일반 발전기로 구현할 수 없는 고출력의 전원을 생성할 수 있다. 이러한 PTO 발전기는 동력을 전달받기 위한 픽업트럭(10)의 동력계통의 위치에 따라 도면에서와 같이 차량하부에 장착될 수 있으며, 필요에 따라 드론격납고(100) 내부에 배치될 수도 있다. 또한, 도 17에 도시된 바와 같이 발전기(420)가 차량하부에 장착되는 경우 드론격납고(100) 내부에 설치되는 유선전원공급기(410)로 전원을 공급할 수 있도록 격납본체(110)의 내부에는 발전기(420)와 전원라인으로 연결된 콘센트(421)가 장착되고 이 콘센트(421)에 유선전원공급기(410)의 전원플러그를 삽입하여 생성된 전기에너지를 공급받을 수 있다.The generator 420 generates electrical energy. Here, by using a PTO (Power Take Off) generator that is connected to the power system of the pickup truck 10 as the generator 420 and generates electric energy with the rotational force provided, the fossil fuel required to drive the generator can be significantly reduced. And it can generate high-output power that cannot be implemented with general generators. Such a PTO generator may be mounted under the vehicle as shown in the drawing according to the location of the power system of the pickup truck 10 for receiving power, and may be disposed inside the drone hangar 100 as necessary. In addition, as shown in FIG. 17 , when the generator 420 is mounted on the lower part of the vehicle, the generator 420 is located inside the containment body 110 so as to supply power to the wired power supply 410 installed inside the drone hangar 100 . The outlet 421 connected to the 420 and the power line is mounted, and the electric energy generated by inserting the power plug of the wired power supply 410 into the outlet 421 may be supplied.

상기 유선전원공급기(410)는 드론(20)이 비행하는데 필요한 전원을 전달하는 구성으로서, 상기 발전기(420)로부터 생성된 전기에너지를 공급받으며 상기 적재함(13) 내부에 배치되고 일측은 드론(20)에 연결되며 타측은 내부에 권취되는 전원케이블(412)이 구비되어 발전기(420)에서 생성된 전기에너지를 전원케이블(412)을 통해 드론(20)에 공급한다. 따라서, 도 17에서와 같이 비행중에 지속적인 전원공급이 가능하여 장시간 감시 관제 임무를 수행할 수 있다.The wired power supply 410 is a configuration that delivers the power required for the drone 20 to fly, and receives the electrical energy generated from the generator 420 and is disposed inside the loading box 13, and one side of the drone 20 ) and the other side is provided with a power cable 412 wound therein to supply electric energy generated by the generator 420 to the drone 20 through the power cable 412 . Therefore, as shown in FIG. 17, continuous power supply during flight is possible, so that a long-term monitoring and control mission can be performed.

여기서, 도 18에 도시된 바와 같이 상기 유선전원공급기(410)는, 발전기(420)의 전기에너지를 공급받아 상기 드론(20)이 비행구동하는데 필요한 구동전원의 형태로 변환하는 전원변환부(413)와, 회전동작하며 상기 전원케이블(412)을 둘레에 권취하거나 둘레로부터 권출하는 권취롤(414) 및, 상기 권취롤(414)이 회전동작하는데 필요한 구동력을 제공하는 구동모터(415)를 포함함으로써, 드론(20)의 비행가능고도를 임의로 조절할 수 있다. 그리고 상기 전원변환부(413), 권취롤(414) 및 구동모터(415)는 케이스(418) 내부에 일체로 장착되어 외부 오염물질로부터 보호될 수 있고 설치 및 운반이 용이하도록 할 수 있다.Here, as shown in FIG. 18 , the wired power supply 410 receives the electric energy of the generator 420 and converts it into a form of driving power required to drive the drone 20 in flight. ), a winding roll 414 that rotates and winds or unwinds the power cable 412 from the circumference, and a driving motor 415 that provides a driving force necessary for the winding roll 414 to rotate. By including, it is possible to arbitrarily adjust the flight height of the drone 20 . And the power conversion unit 413, the winding roll 414, and the driving motor 415 are integrally mounted inside the case 418 to be protected from external contaminants, and to facilitate installation and transportation.

또한, 상기 유선전원공급기(410)는, 드론(20)과 권취롤(414) 사이에 연장된 전원케이블(412)의 텐션크기를 감지하는 텐션감지부(417) 및, 상기 텐션감지부(417)의 감지신호에 따라 전원케이블(412)이 설정된 크기의 텐션이 유지되도록 상기 구동모터(131)를 구동제어하는 제어부(416)를 더 포함함으로써, 드론(20)이 상승할 때 자동으로 전원케이블(412)을 연장시켜 요구되는 비행가능고도로 비행할 수 있도록 하며, 드론(20)이 하강할 때 느슨해진 전원케이블(412)이 드론(20)에 감기는 현상을 미연에 방지할 수 있다.In addition, the wired power supply 410 includes a tension detection unit 417 for detecting the tension size of the power cable 412 extended between the drone 20 and the winding roll 414, and the tension detection unit 417 ) by further comprising a control unit 416 for driving and controlling the driving motor 131 so that the tension of the power cable 412 of the set size is maintained according to the detection signal of the It is possible to extend the 412 so that it can fly to a required flight altitude, and it is possible to prevent the loosening of the power cable 412 from being wound around the drone 20 when the drone 20 descends.

더불어, 상기 유선전원공급기(410)는 드론(20)을 비행제어하는 지상통제장치(300)와 신호연결되는 통신부(419)를 더 포함하고, 상기 제어부(416)는 통신부(419)를 통해 지상통제장치(300)로부터 드론(20)을 하강시키기 위한 제어신호가 입력되면 전원케이블(412)이 권취롤(414)에 권취되도록 하고 드론(20)을 상승시키기 위한 제어신호가 입력되면 전원케이블(412)이 권취롤(414)로부터 권출되도록 구동모터(131)를 구동제어함으로써, 드론(20)의 비행고도가 변화되면 동시에 전원케이블(412)의 길이가 자동조절되어 드론(20)이 상승하면서 전원케이블(412)을 잡아당겨야 하는데 필요한 전력을 절감할 수 있으며, 드론(20)이 빠른 속도로 하강하더라도 동시에 전원케이블(412)을 줄여 드론(20)이 전원케이블(412)에 감기는 현상을 방지할 수 있다.In addition, the wired power supply 410 further includes a communication unit 419 signal-connected to the ground control device 300 for flight control of the drone 20, and the control unit 416 is connected to the ground through the communication unit 419. When a control signal for lowering the drone 20 is input from the control device 300, the power cable 412 is wound on the winding roll 414, and when a control signal for raising the drone 20 is inputted, the power cable ( By controlling the drive motor 131 so that the 412 is unwound from the winding roll 414, when the flight altitude of the drone 20 is changed, the length of the power cable 412 is automatically adjusted at the same time as the drone 20 rises. The power required to pull the power cable 412 can be reduced, and even if the drone 20 descends at a high speed, the power cable 412 is reduced at the same time to prevent the drone 20 from being wound around the power cable 412 . can be prevented

이상에서 설명한 본 발명은 전술한 실시예 및 첨부된 도면에 의해 한정되는 것이 아니고, 본 발명의 기술적 사상을 벗어나지 않는 범위 내에서 여러가지 치환, 변형 및 변경이 가능함은 본 발명이 속하는 기술분야에서 통상의 지식을 가진 자에게 명백할 것이다.The present invention described above is not limited by the above-described embodiments and the accompanying drawings, and it is common in the art to which the present invention pertains that various substitutions, modifications and changes are possible within the scope without departing from the technical spirit of the present invention. It will be clear to those who have knowledge.

100...드론격납고
110...격납본체 112...연장부
113...가이드레일 120...격납커버
121...렉바 122...가이드바
123...슬라이딩바 130...개폐구동부
210...안착판 240...수직바
300...지상통제장치 410...유선전원공급기
412...전원케이블 413...전원변환부
414...권취롤 415...구동모터
416...제어부 417...텐션감지부
419...통신부 420...발전기100...Drone hangar
110...containment body 112...extension
113...guide rail 120...storage cover
121...leg bar 122...guide bar
123...Sliding bar 130...Opening and closing drive part
210...Seating plate 240...Vertical bar
300...Ground Control 410...Wired Power Supply
412...Power cable 413...Power conversion part
414...winding roll 415...drive motor
416...control unit 417...tension sensing unit
419...Ministry of Communications 420...Generator

Claims (4)

실내공간에 전열좌석(11)과 후열좌석(12)이 마련되고 후미에 상향 개구된 적재함(13)이 마련된 픽업트럭(10);
상기 후열좌석(12)에 배치되고 드론(20)을 비행제어하기 위한 제어신호를 출력하고 드론(20)으로부터 전송되는 영상을 디스플레이(310)에 표시하는 지상통제장치(300); 및
드론(20)을 수용하기 위한 내부공간이 마련되고 상기 내부공간의 상부는 개구되어 수용된 드론(20)이 출입하는 통로를 형성하며 하부가 상기 적재함(13)에 고정장착되는 격납본체(110)와, 상기 격납본체(110)의 상부에 장착되고 슬라이딩하거나 회동하면서 개구된 통로를 개폐하는 격납커버(120) 및, 상기 격납커버(120)가 개폐동동작하는데 필요한 구동력을 제공하는 개폐구동부(130)를 포함하는 드론격납고(100);를 포함하는 드론운용 시스템.
a pickup truck 10 having a front row seat 11 and a rear row seat 12 provided in an indoor space and a loading box 13 opened upward at the rear;
a ground control device 300 disposed in the rear row seat 12 and outputting a control signal for flight control of the drone 20 and displaying an image transmitted from the drone 20 on the display 310; and
An internal space for accommodating the drone 20 is provided, and the upper part of the internal space is opened to form a passage through which the accommodated drone 20 enters and exits, and the lower part is fixedly mounted to the loading box 13. A containment body 110 and , a containment cover 120 mounted on the upper portion of the containment body 110 and sliding or rotating to open and close the opened passage, and an opening/closing drive unit 130 that provides a driving force necessary for the containment cover 120 to open and close operation. A drone hangar (100) comprising a; drone operating system including.
 청구항 1에 있어서,
상기 드론격납고(100)는,
상기 드론(20)의 중앙부에 배치되고 수직으로 하향 연장된 수직바(240) 및,
상기 격납본체(110) 내에 수평배치되며 중앙부에는 상하로 개구되어 상기 수직바(240)가 하향 관통 삽입되기 위한 삽입공(212)이 형성되고 상기 삽입공(212)의 둘레에는 상부로 갈수록 점차 직경이 확대되는 형상으로 이루어진 가이드홈(211)이 형성되어 가이드홈(211)의 표면에 접촉된 수직바(240)의 하단이 삽입공(212)의 상단을 향해 슬라이딩하도록 가이드하는 안착판(210)을 더 포함하는 것을 특징으로 하는 픽업트럭용 드론운용 시스템.
The method according to claim 1,
The drone hangar 100,
A vertical bar 240 disposed in the center of the drone 20 and extending vertically downward, and,
It is horizontally arranged in the containment body 110 and is opened up and down in the central portion to form an insertion hole 212 for the vertical bar 240 to be inserted downwardly, and the circumference of the insertion hole 212 gradually increases toward the top. A guide groove 211 having this enlarged shape is formed, so that the lower end of the vertical bar 240 in contact with the surface of the guide groove 211 slides toward the upper end of the insertion hole 212 . Drone operation system for pickup trucks, characterized in that it further comprises a.
 청구항 2에 있어서,
상기 드론격납고(100)는,
상기 격납본체(110) 내에서 상하로 연장배치되어 상기 안착판(210)의 승하강 경로를 형성하는 승강가이드바(220) 및,
상기 안착판(210)이 승강가이드바(220)를 따라 승하강하는데 필요한 구동력을 제공하는 승강구동부(230)를 더 포함하는 것을 특징으로 하는 드론운용 시스템.
3. The method according to claim 2,
The drone hangar 100,
An elevating guide bar 220 which is vertically extended in the containment body 110 to form an elevating path of the seating plate 210, and;
Drone operating system, characterized in that the seating plate 210 further comprises a lift drive unit 230 for providing a driving force necessary for elevating and lowering along the elevating guide bar (220).
 청구항 3에 있어서,
상기 드론격납고(100)는,
전기에너지를 생성하는 발전기(420) 및,
상기 격납본체(110)의 내부에 배치되어 발전기(420)로부터 생성된 전기에너지를 공급받으며, 일측은 드론(20)에 연결되고 타측은 내부에 권취되는 전원케이블(412)이 구비되어 발전기(420)에서 생성된 전기에너지를 전원케이블(412)을 통해 드론(20)에 공급하는 유선전원공급기(410)를 더 포함하는 것을 특징으로 하는 픽업트럭용 드론운용 시스템.4. The method according to claim 3,
The drone hangar 100,
A generator 420 that generates electrical energy, and
It is disposed inside the containment body 110 and receives the electric energy generated from the generator 420, one side is connected to the drone 20 and the other side is provided with a power cable 412 wound inside the generator 420 .
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115991296A (en) * 2023-03-17 2023-04-21 成都纵横大鹏无人机科技有限公司 Unmanned aerial vehicle hangar with foldable hangar door

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KR102614226B1 (en) 2022-05-26 2023-12-15 아트원 주식회사 Drone station that can be driven with one operation

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20130119633A (en) * 2012-04-24 2013-11-01 유콘시스템 주식회사 Unmanned aerial vehicle system with cable connection equipment
KR101535401B1 (en) 2015-04-01 2015-07-08 오인선 Drone type life ring dropping device

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20130119633A (en) * 2012-04-24 2013-11-01 유콘시스템 주식회사 Unmanned aerial vehicle system with cable connection equipment
KR101535401B1 (en) 2015-04-01 2015-07-08 오인선 Drone type life ring dropping device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115991296A (en) * 2023-03-17 2023-04-21 成都纵横大鹏无人机科技有限公司 Unmanned aerial vehicle hangar with foldable hangar door

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