KR102189039B1 - Drone hangar for pickup truck with opening and closing function and, drone operating system including the same - Google Patents

Drone hangar for pickup truck with opening and closing function and, drone operating system including the same Download PDF

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KR102189039B1
KR102189039B1 KR1020200009643A KR20200009643A KR102189039B1 KR 102189039 B1 KR102189039 B1 KR 102189039B1 KR 1020200009643 A KR1020200009643 A KR 1020200009643A KR 20200009643 A KR20200009643 A KR 20200009643A KR 102189039 B1 KR102189039 B1 KR 102189039B1
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South Korea
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drone
opening
pickup truck
disposed
vertical bar
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KR1020200009643A
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Korean (ko)
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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 for handling aircraft
    • B64F1/222—Ground or aircraft-carrier-deck installations for handling aircraft for storing aircraft, e.g. in hangars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K17/00—Arrangement or mounting of transmissions in vehicles
    • B60K17/28—Arrangement or mounting of transmissions in vehicles characterised by arrangement, location, or type of power take-off
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K35/00—Instruments specially adapted for vehicles; Arrangement of instruments in or on vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K35/00—Instruments specially adapted for vehicles; Arrangement of instruments in or on vehicles
    • B60K35/20—Output arrangements, i.e. from vehicle to user, associated with vehicle functions or specially adapted therefor
    • B60K35/21—Output arrangements, i.e. from vehicle to user, associated with vehicle functions or specially adapted therefor using visual output, e.g. blinking lights or matrix displays
    • B60K35/22—Display screens
    • 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
    • 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; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam 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
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00—Suspension arrangements for wings
    • E05D15/06—Suspension arrangements for wings for wings sliding horizontally more or less in their own plane
    • E05D15/0621—Details, e.g. suspension or supporting guides
    • E05D15/066—Details, e.g. suspension or supporting guides for wings supported at the bottom
    • E05D15/0686—Tracks
    • 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
    • E05F15/635—Power-operated mechanisms for wings using electrical actuators using rotary electromotors for horizontally-sliding wings operated by push-pull mechanisms, e.g. flexible or rigid rack-and-pinion arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H19/00—Gearings comprising essentially only toothed gears or friction members and not capable of conveying indefinitely-continuing rotary motion
    • F16H19/02—Gearings comprising essentially only toothed gears or friction members and not capable of conveying indefinitely-continuing rotary motion for interconverting rotary or oscillating motion and reciprocating motion
    • F16H19/04—Gearings comprising essentially only toothed gears or friction members and not capable of conveying indefinitely-continuing rotary motion for interconverting rotary or oscillating motion and reciprocating motion comprising a rack
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G11/00—Arrangements of electric cables or lines between relatively-movable parts
    • H02G11/02—Arrangements of electric cables or lines between relatively-movable parts using take-up reel or drum
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60Y—INDEXING SCHEME RELATING TO ASPECTS CROSS-CUTTING VEHICLE TECHNOLOGY
    • B60Y2200/00—Type of vehicle
    • B60Y2200/10—Road Vehicles
    • B60Y2200/14—Trucks; Load vehicles, Busses
    • B60Y2200/141—Light trucks
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60Y—INDEXING SCHEME RELATING TO ASPECTS CROSS-CUTTING VEHICLE TECHNOLOGY
    • B60Y2200/00—Type of vehicle
    • B60Y2200/50—Aeroplanes, Helicopters
    • B60Y2200/51—Aeroplanes
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2201/00—Constructional elements; Accessories therefor
    • E05Y2201/40—Motors; Magnets; Springs; Weights; Accessories therefor
    • E05Y2201/43—Motors
    • E05Y2201/434—Electromotors; Details thereof
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2201/00—Constructional elements; Accessories therefor
    • E05Y2201/60—Suspension or transmission members; Accessories therefor
    • E05Y2201/622—Suspension or transmission members elements
    • E05Y2201/684—Rails; Tracks
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2201/00—Constructional elements; Accessories therefor
    • E05Y2201/60—Suspension or transmission members; Accessories therefor
    • E05Y2201/622—Suspension or transmission members elements
    • E05Y2201/71—Toothed gearing
    • E05Y2201/716—Pinions
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2201/00—Constructional elements; Accessories therefor
    • E05Y2201/60—Suspension or transmission members; Accessories therefor
    • E05Y2201/622—Suspension or transmission members elements
    • E05Y2201/71—Toothed gearing
    • E05Y2201/722—Racks
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2999/00—Subject-matter not otherwise provided for in this subclass
    • 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)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Power Engineering (AREA)
  • Remote Sensing (AREA)
  • Power-Operated Mechanisms For Wings (AREA)

Abstract

The present invention relates to a drone storage for a pickup truck with an opening/closing function. The drone storage is installed in a pickup truck (10) having a front row seat (11) and a rear row seat (12) in an indoor space and a tail on the rear side with a loading box (13) having an opened upper side, and used to drive a drone (20). The drone storage for the pick truck (10) comprises: a storage main frame (110) which has an inner space for accommodating a drone (20), wherein an upper side of the inner space is opened to form a passage, through which the accommodated drone (20) enters and exits, and has a lower side fixed to and mounted on the loading box (13); a storage cover (120) mounted on an upper side of the storage main frame (110) to slide or rotate, thereby opening/closing the opened passage; and an opening/closing driving unit (130) which provides driving force needed for opening/closing the storage cover (120). The drone storage for a pickup truck with the opening/closing function is able to be rapidly moved and to serve as a control tower in case of a disaster.

Description

개폐기능이 구비된 픽업트럭용 드론격납고 및 이를 포함하는 드론운용 시스템{DRONE HANGAR FOR PICKUP TRUCK WITH OPENING AND CLOSING FUNCTION AND, DRONE OPERATING SYSTEM INCLUDING THE SAME}A drone hangar for pickup trucks equipped with an open/close function and a drone operation system including the same {DRONE HANGAR FOR PICKUP TRUCK WITH OPENING AND CLOSING FUNCTION AND, DRONE OPERATING SYSTEM INCLUDING THE SAME}

본 발명은 개폐기능이 구비된 픽업트럭용 드론격납고 및 이를 포함하는 드론운용 시스템에 관한 것으로, 보다 상세하게는 실내공간에 전열좌석과 후열좌석이 마련되고 후미에 상향 개구된 적재함이 마련된 픽업트럭에 설치되어 드론을 운용하는데 이용되는 픽업트럭용 드론격납고 및 이를 포함하는 드론운용 시스템에 관한 것이다.The present invention relates to a drone hangar for a pickup truck equipped with an opening/closing function and a drone operating system including the same, and more particularly, to a pickup truck having a front row seat and a rear row seat provided in an indoor space and a loading box opened upward at the rear It relates to a drone hangar for a pickup truck used to operate a drone and a drone operation system including the same.

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 there is a risk of accidents such as drowning or forest fires, such as beaches, rivers, or forests, surveillance personnel are operated or CCTVs are installed to prepare for safety accidents. However, when the surveillance area is wide, there is a problem that excessive surveillance operation costs are invented because a large number of surveillance 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 attaching a camera to a drone and flying it in the surveillance area to monitor the captured image on 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 through signal exchange with a ground control device located on the ground and the captured image is transmitted to the ground. Conventionally, the drone is flight-controlled while the ground control device is installed at a location in the surveillance area. It was operated in a way that it was possible to shoot surveillance images for the surveillance area only up to the maximum distance between the drone and the ground control device.

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, since drones generally fly with a charged power source from a built-in battery, the batteries must be replaced every few minutes to tens of minutes, or missions must be switched with a drone with sufficient batteries, which inevitably causes a surveillance blank.

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, in order to be equipped with a portable device to be installed in the surveillance area, it took considerable waiting time to take out each device from the case, put it in place, and set each device to be usable. Moreover, since ground control devices operated outdoors are expensive, there is a hassle of repeating the procedure of setting and removing the ground control devices at the start of monitoring and at the end of each time when monitoring for a long-term surveillance area is performed.

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.In addition, conventionally, since a surveillance image captured in a surveillance area can be monitored only through a display mounted on a ground control device or connected to a cable, there is a problem in that integrated monitoring or management of the surveillance image acquired in each surveillance area is limited.

등록특허공보 제10-1535401호(2015.07.02), 드론방식 구명장비 투하장치.Registered Patent Publication No. 10-1535401 (2015.07.02), drone type lifesaving equipment dropping 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 개폐기능이 구비된 픽업트럭용 드론격납고 및 이를 포함하는 드론운용 시스템을 제공하는 것에 있다.The present invention was created to solve the above-described problems, and an object of the present invention is that a system for operating a drone is installed on a pickup truck, so that it is possible to quickly move to places where access by general vehicles such as mountains and rough roads is difficult. It is to provide a drone hangar for a pickup truck equipped with an opening and closing function capable of performing the mission of a control tower in a disaster disaster, and a drone operation system including the same.

본 발명의 다른 목적은 드론이 수용된 격납고의 상부를 자동으로 개폐할 수 있어 필요시 드론의 신속한 전개 및 철수가 가능하며 드론을 외부로부터 안전하게 보호한 상태로 이동할 수 있는 개폐기능이 구비된 픽업트럭용 드론격납고 및 이를 포함하는 드론운용 시스템을 제공하는 것에 있다.Another object of the present invention is for a pickup truck equipped with an opening/closing function capable of automatically opening and closing the top of the hangar in which the drone is accommodated, enabling rapid deployment and withdrawal of the drone if necessary, and moving the drone in a state that is safely protected from the outside. It is to provide a drone hangar and a drone operation system including the same.

본 발명의 특징에 따르면, 실내공간에 전열좌석(11)과 후열좌석(12)이 마련되고 후미에 상향 개구된 적재함(13)이 마련된 픽업트럭(10)에 설치되어 드론(20)을 운용하는데 이용되는 개폐기능이 구비된 픽업트럭용 드론격납고에 있어서, 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); 상기 격납본체(110)의 상부에 장착되어 슬라이딩하거나 회동하면서 개구된 통로를 개폐하는 격납커버(120); 및 상기 격납커버(120)가 개폐동작하는데 필요한 구동력을 제공하는 개폐구동부(130);를 포함하는 개폐기능이 구비된 픽업트럭용 드론격납고가 제공된다.According to a feature of the present invention, it is installed in the pickup truck 10 provided with the front row seat 11 and the rear row seat 12 in the indoor space and the loading box 13 opened upward in the rear, and used to operate the drone 20 In the drone hangar for a pickup truck equipped with an opening and closing function, 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 received drone 20 enters and exits, and the lower part is the The storage body 110 fixedly mounted on the loading box 13; A storage cover 120 mounted on an upper portion of the storage body 110 to open and close the opened passage while sliding or rotating; And an opening/closing driving unit 130 for providing a driving force necessary for the storage cover 120 to open and close. A drone hangar for a pickup truck including an opening/closing function is provided.

본 발명의 다른 특징에 따르면, 상기 격납커버(120)는 격납본체(110)의 상부에서 전후방으로 슬라이딩하면서 격납본체(110)의 개구된 통로를 개폐하고, 상기 픽업트럭(10)의 루프(14) 상에서 후열좌석(12)의 상부 위치에 수평배치되는 연장부(112);를 더 포함하고, 상기 개폐구동부(130)는 연장부(112)의 상부에 배치되어 격납커버(120)가 전후방으로 슬라이딩하는데 필요한 구동력을 제공하는 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고가 제공된다.According to another feature of the present invention, the storage cover 120 slides forward and backward from the top of the storage body 110 to open and close the opened passage of the storage body 110, and the roof 14 of the pickup truck 10 ), the extension part 112 horizontally disposed at the upper position of the rear row seat 12; and the opening/closing drive part 130 is disposed above the extension part 112 so that the storage cover 120 moves forward and backward. There is provided a drone hangar for a pickup truck equipped with an opening/closing function, characterized in that it provides a driving force required for sliding.

본 발명의 또 다른 특징에 따르면, 상기 격납커버(120)는 저면의 중앙에 전후방(L)으로 연장되고 연장된 길이를 따라 하부에 기어가 연이어 형성된 랙바(121)가 배치되고, 저면의 폭방향(W) 양측에는 전후방(L)으로 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 포함하는 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고가 제공된다.According to another feature of the present invention, the storage cover 120 extends in the front and rear (L) at the center of the bottom surface, and the rack bar 121 is formed in a row of gears at the bottom along the extended length, and the width direction of the bottom surface (W) Guide bars 122 extending forward and backward (L) are respectively disposed on both sides, and the opening/closing drive unit 130 is condensed on a drive motor 131 that provides rotational force and a drive shaft of the drive motor 131 And a driven gear 133 connected to the driving gear 132 to rotate the horizontally arranged rotation shaft 135, and the gear of the rack bar 121 being condensed on the rotation shaft 135 It characterized in that it comprises a pinion gear 134 that rotates in engagement with, and a support roller 136 that is rotatably disposed in a horizontal axis at a position corresponding to each of the guide bars 122 to support the bottom of the guide bar 122 A drone hangar for a pickup truck with an opening and closing function is provided.

본 발명의 또 다른 특징에 따르면, 상기 격납본체(110)의 상단 폭방(W)향 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 전후방(L)으로 슬라이딩 이동하는 슬라이딩바(123)가 배치된 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고가 제공된다.According to another feature of the present invention, guide rails 113 horizontally disposed to extend in the front and rear (L) are disposed on both sides of the upper width (W) side of the storage body 110, and the storage cover 120 It characterized in that the sliding bar 123 that slides in the front and rear (L) while being supported by the guide rail 113 is disposed horizontally at a position corresponding to each guide rail 113 A drone hangar for a pickup truck equipped with an opening and closing function is provided.

본 발명의 또 다른 특징에 따르면, 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 포함하는 개폐기능이 구비된 픽업트럭용 드론격납고가 제공된다.According to another feature of the present invention, the generator 420 for generating electric energy; And a power cable 412 disposed inside the containment body 110 to receive electric energy generated from the generator 420, and one side is connected to the drone 20 and the other side is provided with a power cable 412 wound therein. A wired power supply 410 for supplying the electric energy generated in 420 to the drone 20 through a power cable 412; a drone hangar for a pickup truck having an opening/closing function is provided.

본 발명의 또 다른 특징에 따르면, 상기 유선전원공급기(410)는, 상기 발전기(420)의 전기에너지를 공급받아 상기 드론(20)이 비행구동하는데 필요한 구동전원의 형태로 변환하는 전원변환부(413)와, 정역회전하며 상기 전원케이블(412)을 둘레에 권취하거나 둘레로부터 전원케이블(412)을 권출하는 권취롤(414) 및, 상기 권취롤(414)이 회전동작하는데 필요한 구동력을 제공하는 구동모터(415)를 포함하는 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고가 제공된다.According to another feature of the present invention, the wired power supply 410 receives the electric energy of the generator 420 and converts the drone 20 into a form of driving power required to drive the flight ( 413), a take-up roll 414 that rotates forward and backward and winds the power cable 412 around or unwinds the power cable 412 from the periphery, and a driving force required for the take-up roll 414 to rotate. There is provided a drone hangar for a pickup truck with an opening and closing function, characterized in that it comprises a driving motor 415 to.

본 발명의 또 다른 특징에 따르면, 상기 유선전원공급기(410)는, 상기 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(415)를 구동제어하는 제어부(416)를 더 포함하는 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고가 제공된다.According to another feature of the present invention, the wired power supply 410 is a tension sensing unit 417 that detects the tension size of the power cable 412 extended between the drone 20 and the winding roll 414 And a control unit 416 for driving and controlling the driving motor 415 so that the tension of the set size of the power cable 412 is maintained according to the detection signal of the tension sensing unit 417. A drone hangar for pickup trucks equipped with functions is provided.

본 발명의 또 다른 특징에 따르면, 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 지상통제장치로(300)부터 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(415)를 구동제어하는 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고가 제공된다.According to another feature of the present invention, the wired power supply 410 further includes a communication unit 419 signal-connected to the ground control device 300 for controlling the flight of the drone 20, and the control unit 416 When a control signal for lowering the drone 20 is input from 300 to the ground control device through the communication unit 419, the power cable 412 is wound around the winding roll 414 and the drone 20 is raised. When a control signal is input, a drone hangar for a pickup truck with an opening/closing function, characterized in that the driving motor 415 is controlled so that the power cable 412 is unwound from the winding roll 414 is provided.

본 발명의 또 다른 특징에 따르면, 상기 발전기(420)는 픽업트럭의 동력계통에 연결되어 제공되는 회전력으로 전기에너지를 생성하는 PTO(Power Take Off) 발전기인 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고가 제공된다.According to another feature of the present invention, the generator 420 is a pickup equipped with an open/close function, characterized in that the generator 420 is a PTO (Power Take Off) generator that generates electric energy with rotational force provided by being connected to the power system of the pickup truck. A drone hangar for trucks is provided.

한편. 본 발명의 또 다른 특징에 따르면, 실내공간에 전열좌석(11)과 후열좌석(12)이 마련되고 후미에 상향 개구된 적재함(13)이 마련된 픽업트럭(10)에 설치되어 드론(20)을 운용하는데 이용되는 픽업트럭용 드론운용 시스템에 있어서, 상기 후열좌석(12)에 배치되고 드론(20)을 비행제어하기 위한 제어신호를 출력하고 드론(20)으로부터 전송되는 영상을 디스플레이(310)에 표시하는 지상통제장치; 및 드론(20)을 수용하기 위한 내부공간이 마련되고 상기 내부공간의 상부는 개구되어 수용된 드론(20)이 출입하는 통로를 형성하며 하부가 상기 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 개폐동작하는데 필요한 구동력을 제공하는 개폐구동부(130)를 포함하는 드론격납고(100);를 포함하는 픽업트럭용 드론운용 시스템이 제공된다.Meanwhile. According to another feature of the present invention, a front row seat 11 and a rear row seat 12 are provided in an indoor space and installed on a pickup truck 10 provided with an upwardly opened loading box 13 at the rear to operate the drone 20 In the drone operating system for a pickup truck used to output a control signal for flight control of the drone 20, which is disposed in the rear seat 12, and an image transmitted from the drone 20 is displayed on the display 310 Ground control device; And an internal space for accommodating the drone 20 is provided, the upper part of the internal space is opened to form a passage through which the received drone 20 enters and exits, and the lower part is inserted into the loading box 13 to be fixedly mounted. 110), a storage cover 120 that is mounted on the upper portion of the storage body 110 and opens and closes an opened passage while sliding or rotating, and an opening/closing drive unit that provides a driving force required for the opening and closing operation of the storage cover 120 ( A drone hangar 100 including 130); a drone operating system for a pickup truck is provided.

이상에서와 같이 본 발명에 의하면,According to the present invention as above,

첫째, 격납본체(110)는 드론(20)을 수용하기 위한 내부공간이 마련되고 상기 내부공간의 상부는 개구되어 수용된 드론(20)이 출입하는 통로를 형성하며 하부가 적재함(13)에 삽입되어 고정장착되고, 격납커버(120)는 격납본체(110)의 상부에 장착되어 슬라이딩하거나 회동하면서 개구된 통로를 개폐하며, 개폐구동부(130)는 격납커버(120)가 개폐동작하는데 필요한 구동력을 제공함으로써, 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 storage body 110 is provided with an internal space for accommodating the drone 20, and the upper part of the internal space is opened to form a passage for the received drone 20 to enter and exit, and the lower part is inserted into the loading box 13 It is fixedly mounted, and the storage cover 120 is mounted on the upper part of the storage body 110 to open and close the opened passage while sliding or rotating, and the opening/closing drive unit 130 provides the driving force necessary for the storage cover 120 to open and close. By doing so, it is possible to automatically open and close the top of the hangar 100 in which the drone 20 is accommodated, so that the drone 20 can be quickly deployed and withdrawn if necessary, and the drone 20 can be moved in a state that is safely protected from the outside. .

둘째, 상기 격납커버(120)는 격납본체(110)의 상부에서 전후방으로 슬라이딩하면서 격납본체(110)의 개구된 통로를 개폐하고, 연장부(112)는 상기 픽업트럭(10)의 루프(14) 상에서 후열좌석(12)의 상부 위치에 수평배치되며, 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 통로 공간을 충분하게 확보하면서 동시에 전방으로 슬라이딩된 격납커버(120)가 자중에 의해 하부로 쳐지면서 훼손되거나 전열좌석(11)에 착석한 운전자의 시야를 가리는 것을 방지할 수 있다.Second, the storage cover 120 opens and closes the opened passage of the storage body 110 while sliding from the top of the storage body 110 to the front and rear, and the extension part 112 is a roof 14 of the pickup truck 10. ) Is disposed horizontally at the upper position of the rear seat 12, and the opening/closing drive unit 130 is disposed above the extension unit 112 to provide the driving force necessary for the storage cover 120 to slide forward and backward, and the storage cover As the 120 slides forward, the opened passage space of the storage body 110 disposed at the rear is sufficiently secured, and at the same time, the storage cover 120 sliding forward is struck downward by its own weight and is damaged or damaged or the front row seat ( 11) can be prevented from obstructing the view of the driver seated in the car.

셋째, 상기 격납커버(120)는 저면의 중앙에 전후방(L)으로 연장되고 연장된 길이를 따라 하부에 기어가 연이어 형성된 랙바(121)가 배치되고, 저면의 폭방향(W) 양측에는 전후방(L)으로 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 포함함으로써, 격납커버(120)의 하중을 안정적으로 지지하면서도 격납커버(120)의 안정적인 슬라이딩 이동을 가이드할 수 있다.Third, the storage cover 120 is extended to the front and rear (L) at the center of the bottom surface, and the rack bar 121 is arranged in a row of gears at the bottom along the extended length, and the front and rear ( Each of the guide bars 122 extending to L) is disposed, and the opening/closing drive unit 130 includes a drive motor 131 providing a rotational force, a drive gear 132 condensed on a drive shaft of the drive 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 rotated by meshing with the gear of the rack bar 121 ( 134) And, by including a support roller 136 that is rotatably disposed in a horizontal axis at a position corresponding to each guide bar 122 to support the bottom surface of the guide bar 122, the load of the storage cover 120 is stabilized. While supporting it, it is possible to guide the stable sliding movement of the storage cover 120.

넷째, 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.Fourth, guide rails 113 are disposed horizontally to extend in the front and rear (L) on both sides of the upper width direction (W) of the storage body 110, and each guide rail 113 on the storage cover 120 A sliding bar 123 that is horizontally disposed to extend to the front and rear (L) so as to be extended to the front and rear (L) and is supported by the guide rail 113 and slides back and forth is disposed, so that the storage cover 120 is struck downward by its own weight. It can be supported more firmly as a phenomenon.

도 1은 본 발명의 바람직한 실시예에 따른 드론격납고가 폐쇄된 상태를 나타낸 사시도,
도 2는 본 발명의 바람직한 실시예에 따른 격납커버가 생략된 상태를 나타낸 사시도,
도 3은 본 발명의 바람직한 실시예에 따른 드론격납고의 내부구성을 나타낸 측면도,
도 4는 본 발명의 바람직한 실시예에 따른 픽업트럭용 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 drone hangar according to a preferred embodiment of the present invention,
2 is a perspective view showing a state in which the storage cover is omitted according to a preferred embodiment of the present invention;
Figure 3 is a side view showing the internal configuration of the 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 for a pickup truck according to a preferred embodiment of the present invention is installed in the 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 the drone hangar according to a preferred embodiment of the present invention,
7 is a perspective view showing a bottom configuration of a storage cover according to a preferred embodiment of the present invention,
Figure 8 is a front sectional view showing the opening and closing structure of the drone hangar according to a preferred embodiment of the present invention,
9 is a side cross-sectional view showing a closed state of the drone hangar according to a preferred embodiment of the present invention;
10 is a side cross-sectional view showing an open state of the 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 sectional views showing the concave bone 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 is locked by an electromagnet according to a preferred embodiment of the present invention;
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.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 with reference to the accompanying drawings.

본 발명의 바람직한 실시예에 따른 픽업트럭용 드론운용 시스템은 실내공간에 전열좌석(11)과 후열좌석(12)이 마련되고 후미에 상향 개구된 적재함(13)이 마련된 픽업트럭(10)에 설치되어 드론(20)을 운용하는데 이용되는 드론운용 시스템으로서, 지상통제장치(300) 및 드론격납고(100)를 포함한다.The drone operating system for a pickup truck according to a preferred embodiment of the present invention is installed on a pickup truck 10 in which a front row seat 11 and a rear row seat 12 are provided in an indoor space, and a loading box 13 opened upwardly at the rear is provided. As a drone operation system used to operate the drone 20, it includes a ground control device 300 and a drone hangar 100.

먼저, 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. 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.First, the ground control device 300 is a control means for controlling the flight of the drone 20 and is disposed in the rear row seat 12 and outputs a control signal for controlling the flight of the drone 20. The transmitted image is displayed on the display 310. In addition, as shown in Fig. 5, the rear seat 12 is provided with a storage frame 330 for storing various communication devices and control devices necessary for operating the ground control device 300, and the storage frame 330 Since the display 310 is mounted on the upper part, a narrow indoor space can be efficiently used.

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.The drone hangar 100 is a housing housing the drone 20 and includes a storage body 110, a storage cover 120, and an opening/closing drive unit 130 as shown in FIGS. 1 to 5.

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 is provided with an internal space for accommodating the drone 20, the upper part of the internal space is opened to form a passage for the received drone 20 to enter and exit, and the lower part is inserted into the loading box 13 It 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 Figure 3, the storage body 110 is composed of a plurality of frame frames 111 are assembled in a rectangular shape to form a frame, and is mounted between each frame frame 111 to cover the side. And, only the lower portion of the frame 111 may be inserted into the loading box 13 and fixed or, if necessary, inserted into the loading box 13 together with a side plate and fixed.

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 storage cover 120 is mounted on the upper portion of the storage body 110 and opens and closes the opened passage while sliding or rotating. Here, the storage cover 120 may be hinged to the storage body 110 in a state horizontally disposed on the top of the storage body 110 to be opened and closed in an opening and closing manner, and as shown in the drawing, the storage cover 120 ) May open and close the opened passage of the storage body 110 while sliding from the top of the storage body 110 forward and backward. Hereinafter, it will be described by exemplifying opening and closing the passage of the storage body 110 while the storage cover 120 slides forward and backward.

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 driver 130 provides a driving force required for the storage cover 120 to open and close. Accordingly, a driver or a drone operator can automatically open and close the storage 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 that is horizontally disposed is provided at an upper position of the rear row seat 12, and the opening/closing driving part 130 is located on the upper part of the extension part 112. By providing the driving force necessary for the storage cover 120 to slide forward and backward, the storage cover 120 slides forward and secures a sufficient open passage space of the storage body 110 disposed at the rear while simultaneously moving forward. It is possible to prevent the sliding storage cover 120 from being damaged by being struck downward by its own weight or obstructing the view of the driver seated in the front seat 11.

여기서, 도 6 내지 도 8에 도시된 바와 같이, 상기 격납커버(120)는 저면의 중앙에 전후방(L)으로 연장되고 연장된 길이를 따라 하부에 기어가 연이어 형성된 랙바(121)가 배치되고, 저면의 폭방향(W) 양측에는 전후방(L)으로 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 storage cover 120 extends in the front and rear (L) at the center of the bottom surface, and the rack bar 121 is arranged in a row of gears at the bottom along the extended length, Guide bars 122 extending in the front and rear directions (L) are respectively disposed on both sides of the bottom in the width direction (W), and the opening/closing drive unit 130 includes a driving motor 131 providing rotational force and a driving motor 131 The driving gear 132 condensed to the drive shaft of the, and a driven gear 133 connected to the drive gear 132 to rotate the horizontally arranged rotation shaft 135, and the rack bar ( 121, a pinion gear 134 that rotates in engagement with the gear of the guide bar 122, and a support roller 136 that is rotatably disposed in a horizontal axis at a position corresponding to each guide bar 122 to support the bottom of the guide bar 122 can do.

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 forward rotation, the driven gear 133 is rotated while the driving gear 132 rotates in one direction, and the pinion gear 134 is rotated while the rotation shaft 135 rotates together to rotate the pinion gear ( As the rack bar 121 engaged with the 134 moves forward, the storage cover 120 slides forward as shown in FIG. 10 to open the passage of the storage body 110. At this time, since the load of the storage cover 120 is supported and distributed by the support rollers 136 through the guide bars 122 on both sides, the storage cover 120 can be moved 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 a reverse rotation while the storage cover 120 is opened in this way, the driving gear 132 rotates in the other direction to rotate the driven gear 133 and the rotation shaft 135 rotates together. While rotating the pinion gear 134 to move the rack bar 121 to the rear, the storage cover 120 slides backwards as shown in FIG. 9 to close the passage of the storage 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 disposed to extend in the front and rear (L) are disposed on both sides of the upper width direction (W) of the storage body 110, respectively, on the storage cover 120 At a position corresponding to the guide rail 113, a sliding bar 123 that is horizontally disposed to extend in the front and rear (L) and supported by the guide rail 113 and slides in the front and rear is disposed, so that the storage cover 120 is It can be supported more firmly due to the phenomenon of being struck 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.The upper portion of the hangar 100 in which the drone 20 is accommodated can be automatically opened and closed through the combination of the storage body 110, the storage cover 120 and the opening/closing drive unit 130 as described above. 20) can be quickly deployed and withdrawn, and the drone 20 can be moved safely from the outside.

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

상기 수직바(240)는 드론(20)의 중앙부에 배치되고 수직으로 하향 연장된다. 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, 도 11에서와 같이 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 disposed at the center of the drone 20 and extends vertically downward. The vertical bar 240 is made of an extension structure whose length is adjusted up and down, and when the drone 20 is in flight, it is reduced to the minimum length so that it does not interfere with external obstacles, and when landing, the length of the vertical bar is extended in the downward direction so that it can be guided. It is desirable to be. In addition, as shown in FIG. 11, the vertical bar 240 has a hollow formed therein, and a 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 mounting 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 As it is lost, it may be guided through the insertion hole 212.

상기 안착판(210)은 상기 적재함(13) 내에 수평배치되며 중앙부에는 상하로 개구되어 상기 수직바(240)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 mounting plate 210 is horizontally disposed in the loading box 13 and is opened up and down in the central portion to form an insertion hole 212 through which the vertical bar 240 is inserted downwardly, and is inserted on the mounting plate 210 Around the circumference of the ball 212, a guide groove 211 formed in a shape that gradually increases in diameter toward the top is formed, and the lower end of the guide bar 122 in contact with the surface of the guide groove 211 is Guide it to slide toward the top. In addition, an extension pipe 219 extending downward to a predetermined length may be formed in the insertion hole 212 to guide the inserted vertical bar 240 downward in a vertical direction.

이러한 수직바(240)와 안착판(210)의 조합된 구성으로 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.The vertical bar 240 and the seating plate 210 are combined to guide the lower end of the vertical bar 240 in contact with the surface of the guide groove 211 to slide toward the upper end of the insertion hole 212 to guide the seating plate. Even if a strong wind blows or a large movement is applied to the pickup truck 10 when the drone 20 lands at 210 or when the landing drone 20 takes off, it may be possible to stably land and take off.

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 extending vertically 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 as an elevating guide By providing the driving force required to move up and down along the bar 220, it is possible to prevent the drone 20 from colliding with surrounding components such as the storage passageway when taking off, and the storage cover 120 of the hangar 100 is slim I can do it. The elevating guide bar 220 has a structure in which the length is adjusted while a plurality of frames are extended and contracted, so that the elevating guide bar 220 extends and contracts with the driving force of the elevating driver 230. As the lift driving unit 230, a pneumatic or hydraulic actuator may be used as shown in the drawing, and a driving motor may be used to provide a driving force required for the lift drive.

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 an arc shape with a flat cross-section opening laterally toward the center of the guide groove 211, while the upper end to the lower end of the guide groove 211 A plurality of concave bones 215 extending upwardly are formed in succession along the circumference, and each concave bones 215 are arranged in close contact along the circumference of the guide groove 211 and between two adjacent concave bones 215 A sharply raised bone compartment 214 is formed, so that the lower end of the vertical bar 240 is in contact with the inner surface of the guide groove 211 while the drone 20 descends, and the drone 20 is overturned. It 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 recessed in a lateral direction is formed around the periphery, and is inserted into the insertion hole 212. A pull-out hole 216 opened laterally is formed at a position corresponding to the fixing groove 243 of the vertical bar 240, and a pull-out hole 216 is formed around the insertion hole 212 so that it can be pulled out laterally. The electromagnet 217 to be mounted is disposed, and the electromagnet 217 is pulled outward by the elastic member 218 and disposed outside the withdrawal hole 216. When driving power is applied and a magnetic field is formed, the withdrawal hole 216 ), while being attached to the vertical bar 240, inserted into the fixing groove 243, selectively locking the inserted state of the vertical bar 240, and landing on the seating plate 210 It can prevent separation by pressing.

한편, 상기 격납고(100)는 도 11, 도 12 및 도 17에 도시된 바와 같이 발전기(420) 및 유선전원공급기(410)를 더 포함한다.Meanwhile, the 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 electric energy. Here, by using a PTO (Power Take Off) generator that is connected to the power system of the pickup truck 10 by the generator 420 to generate electric energy with the provided rotational force, fossil fuel required to drive the generator can be greatly reduced. And it can generate high-output power that cannot be implemented with a general generator. The PTO generator may be mounted under the vehicle as shown in the drawing according to the position of the power system of the pickup truck 10 for receiving power, and may be disposed inside the drone hangar 100 if necessary. In addition, as shown in FIG. 17, when the generator 420 is mounted on the lower part of the vehicle, a generator inside the containment body 110 so that power can be supplied to the wired power supply 410 installed inside the drone hangar 100 An outlet 421 connected to the power line 420 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 일단은 드론(20)에 연결되며 타단 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 transmits power necessary for the drone 20 to fly, and receives electric energy generated from the generator 420 and is disposed inside the loading box 13 and has one end of the drone 20 ) And is provided with a power cable 412 wound inside the other end to supply electric energy generated by the generator 420 to the drone 20 through the power cable 412. Therefore, as shown in FIG. 17, it is possible to continuously supply power during flight, thereby performing a long-time monitoring and control mission.

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, 정역회전하며 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 is a power conversion unit 413 that receives electric energy from the generator 420 and converts it into a form of driving power required for the drone 20 to fly. ), a winding roll 414 that rotates forward and backward and winds or unwinds the power cable 412 around the periphery, 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 altitude of the drone 20. In addition, 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 facilitate installation and transport.

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 sensing unit 417 for sensing the tension size of the power cable 412 extended between the drone 20 and the winding roll 414, and the tension sensing unit 417 ) In accordance with the detection signal of the power cable 412 to maintain the tension of the set size by further comprising a control unit 416 for driving and controlling the drive motor 131, automatically power cable when the drone 20 rises. By extending 412, it is possible to fly at a required flight altitude, and the phenomenon that the power cable 412, which is loosened when the drone 20 descends, can be prevented from being wound around the drone 20.

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 that is signal-connected to the ground control device 300 for controlling the flight of the drone 20, and the control unit 416 is 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 input, the power cable ( By controlling the driving of the driving motor 131 so that 412 is unwound from the winding roll 414, the length of the power cable 412 is automatically adjusted when the flight altitude of the drone 20 is changed, and 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 various substitutions, modifications and changes are possible within the scope of the technical spirit of the present invention. It will be obvious to those of 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...container body 112... extension
113...guide rail 120...container cover
121...Legbar 122...Guide Bar
123...sliding bar 130...switching drive part
210...seat plate 240...vertical bar
300...ground control device 410...wired power supply
412...power cable 413...power converter
414...winding roll 415...drive motor
416...control part 417...tension detection part
419...Ministry of Communications 420...Generator

Claims (10)

실내공간에 전열좌석(11)과 후열좌석(12)이 마련되고 후미에 상향 개구된 적재함(13)이 마련된 픽업트럭(10)에 설치되어 드론(20)을 운용하는데 이용되는 개폐기능이 구비된 픽업트럭용 드론격납고에 있어서,
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);
상기 격납본체(110)의 상부에 장착되어 슬라이딩하거나 회동하면서 개구된 통로를 개폐하는 격납커버(120);
상기 격납커버(120)가 개폐동작하는데 필요한 구동력을 제공하는 개폐구동부(130);
상기 드론(20)의 중앙부에 배치되고 수직으로 하향 연장된 수직바(240); 및
상기 적재함(13) 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 포함하고,
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 구획산(214)이 형성되며,
상기 수직바(240)는 자성체 재질로 이루어지며 둘레에는 둘레에는 측방으로 오목하게 함몰된 고정홈(243)이 형성되고, 상기 삽입공(212) 상에서 삽입된 수직바(240)의 고정홈과(243) 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 록킹하는 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고.
A pickup equipped with an opening/closing function used to operate the drone 20 by being installed on a pickup truck 10 with a front row seat 11 and a rear row seat 12 provided in the indoor space and a loading box 13 opened upward at the rear. In the drone hangar for trucks,
An internal space for accommodating the drone 20 is provided, an upper portion of the internal space is opened to form a passage through which the received drone 20 enters and exits, and a storage body 110 having a lower portion fixedly mounted on the loading box 13;
A storage cover 120 mounted on an upper portion of the storage body 110 to open and close the opened passage while sliding or rotating;
An opening/closing driving unit 130 for providing a driving force necessary for the storage cover 120 to open and close;
A vertical bar 240 disposed at the center of the drone 20 and extending vertically downward; And
It is disposed horizontally in the loading box 13 and is opened up and down in the central portion to form an insertion hole 212 through which the vertical bar 240 is inserted downwardly, and the diameter gradually increases toward the top around the insertion hole 212. A mounting plate 210 for guiding the lower end of the vertical bar 240 in contact with the surface of the guide groove 211 to slide toward the upper end of the insertion hole 212 by forming a guide groove 211 in an enlarged shape; Including,
On the inner surface of the guide groove 211, a plurality of concave bones 215 extending upward from the top to the bottom of the guide groove 211 while having an arc shape with a flat cross-section opening laterally toward the center of the guide groove 211 Doedoe formed continuously along the circumference, while each concave bone 215 is arranged in close contact along the circumference of the guide groove 211, a sharply raised compartment mountain 214 is formed between the adjacent two concave bones 215 And
The vertical bar 240 is made of a magnetic material, and has a circumferentially concave fixing groove 243 formed therein, and a fixing groove of the vertical bar 240 inserted in the insertion hole 212 ( 243) A pull-out hole 216 opened laterally is formed at a corresponding position, and an electromagnet 217 mounted to be pulled laterally through a pull-out hole 216 is disposed around the insertion hole 212, The electromagnet 217 is pulled outward by the elastic member 218 and disposed outside the withdrawal hole 216. When a driving power is applied and a magnetic field is formed, the electromagnet 217 is applied to the vertical bar 240 through the withdrawal hole 216. A drone hangar for a pickup truck with an open/close function, characterized in that it is inserted into the fixing groove 243 while being attached to selectively lock the inserted state of the vertical bar 240.
 청구항 1에 있어서,
상기 격납커버(120)는 격납본체(110)의 상부에서 전후방으로 슬라이딩하면서 격납본체(110)의 개구된 통로를 개폐하고,
상기 픽업트럭(10)의 루프(14) 상에서 후열좌석(12)의 상부 위치에 수평배치되는 연장부(112);를 더 포함하고,
상기 개폐구동부(130)는 연장부(112)의 상부에 배치되어 격납커버(120)가 전후방으로 슬라이딩하는데 필요한 구동력을 제공하는 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고.
The method according to claim 1,
The storage cover 120 opens and closes the opened passage of the storage body 110 while sliding back and forth from the top of the storage body 110,
The pickup truck 10 includes an extension part 112 horizontally disposed at an upper position of the rear seat 12 on the roof 14 of the pickup truck 10,
The opening and closing driving unit 130 is disposed on the upper portion of the extension unit 112 to provide a driving force necessary for the storage cover 120 to slide forward and backward. A drone hangar for a pickup truck having an opening/closing function.
 청구항 2에 있어서,
상기 격납커버(120)는 저면의 중앙에 전후방(L)으로 연장되고 연장된 길이를 따라 하부에 기어가 연이어 형성된 랙바(121)가 배치되고, 저면의 폭방향(W) 양측에는 전후방(L)으로 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 포함하는 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고.
The method according to claim 2,
The storage cover 120 extends to the front and rear (L) at the center of the bottom surface, and a rack bar 121 is arranged in which gears are continuously formed at the bottom along the extended length, and the front and rear (L) on both sides of the width direction (W) of the bottom surface Guide bars 122 extending into each are disposed,
The opening/closing drive unit 130 includes a drive motor 131 providing rotational force, a drive gear 132 condensed to a drive shaft of the drive motor 131, and a horizontally disposed rotation shaft connected to the drive gear 132 ( A driven gear 133 that rotates 135, a pinion gear 134 that is condensed on the rotation shaft 135 and rotates by meshing with a gear of the rack bar 121, and a position corresponding to each guide bar 122 A drone hangar for a pickup truck with an opening and closing function, characterized in that it includes a support roller 136 that is rotatably disposed in a horizontal axis and supports the bottom surface of the guide bar 122.
 청구항 3에 있어서,
상기 격납본체(110)의 상단 폭방(W)향 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 전후방(L)으로 슬라이딩 이동하는 슬라이딩바(123)가 배치된 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고.
The method of claim 3,
Guide rails 113 horizontally disposed so as to extend in the front and rear (L) are disposed on both sides of the storage body 110 toward the upper width (W),
At a position corresponding to each guide rail 113 on the storage cover 120, there is a sliding bar 123 that is horizontally disposed to extend in the front and rear (L) and supported by the guide rail 113 and slides in the front and rear (L). A drone hangar for a pickup truck equipped with an opening and closing function, characterized in that it is arranged.
 청구항 1에 있어서,
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 포함하는 개폐기능이 구비된 픽업트럭용 드론격납고.
The method according to claim 1,
A generator 420 for generating electric energy; And
It is disposed inside the containment body 110 to receive 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 ) A wired power supply 410 for supplying the electric energy generated by the power cable 412 to the drone 20 through a power cable 412; a drone hangar for a pickup truck having an opening/closing function.
 청구항 5에 있어서,
상기 유선전원공급기(410)는,
상기 발전기(420)의 전기에너지를 공급받아 상기 드론(20)이 비행구동하는데 필요한 구동전원의 형태로 변환하는 전원변환부(413)와,
정역회전하며 상기 전원케이블(412)을 둘레에 권취하거나 둘레로부터 전원케이블(412)을 권출하는 권취롤(414) 및,
상기 권취롤(414)이 회전동작하는데 필요한 구동력을 제공하는 구동모터(415)를 포함하는 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고.
The method of claim 5,
The wired power supply 410,
A power conversion unit 413 that receives electric energy from the generator 420 and converts the drone 20 into a form of driving power required to drive the flight;
A winding roll 414 that rotates forward and backward and winds the power cable 412 around or unwinds the power cable 412 from the periphery, and
A drone hangar for a pickup truck having an opening/closing function, characterized in that it comprises a driving motor 415 that provides a driving force necessary for the winding roll 414 to rotate.
 청구항 6에 있어서,
상기 유선전원공급기(410)는,
상기 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(415)를 구동제어하는 제어부(416)를 더 포함하는 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고.
The method of claim 6,
The wired power supply 410,
A tension sensing unit 417 for sensing the tension size of the power cable 412 extended between the drone 20 and the winding roll 414, and
The opening/closing function further comprises a control unit 416 for driving and controlling the driving motor 415 so that the tension of the set size of the power cable 412 is maintained according to the detection signal of the tension sensing unit 417 Drone hangar for pickup trucks.
 청구항 7에 있어서,
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 지상통제장치로(300)부터 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(415)를 구동제어하는 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고.
The method of claim 7,
The wired power supply 410 further includes a communication unit 419 signal-connected to the ground control device 300 for controlling the flight of the drone 20,
When a control signal for lowering the drone 20 is input from 300 to the ground control device through the communication unit 419, the control unit 416 causes the power cable 412 to be wound around the winding roll 414, and the drone ( 20) A drone hangar for a pickup truck with an opening/closing function, characterized in that when a control signal for lifting is input, the driving motor 415 is driven and controlled so that the power cable 412 is unwound from the winding roll 414.
 청구항 8에 있어서,
상기 발전기(420)는 픽업트럭의 동력계통에 연결되어 제공되는 회전력으로 전기에너지를 생성하는 PTO(Power Take Off) 발전기인 것을 특징으로 하는 개폐기능이 구비된 픽업트럭용 드론격납고.
The method of claim 8,
The generator 420 is a PTO (Power Take Off) generator that is connected to the power system of the pickup truck and generates electric energy with a rotational force provided.
 실내공간에 전열좌석(11)과 후열좌석(12)이 마련되고 후미에 상향 개구된 적재함(13)이 마련된 픽업트럭(10)에 설치되어 드론(20)을 운용하는데 이용되는 픽업트럭용 드론운용 시스템에 있어서,
상기 후열좌석(12)에 배치되고 드론(20)을 비행제어하기 위한 제어신호를 출력하고 드론(20)으로부터 전송되는 영상을 디스플레이(310)에 표시하는 지상통제장치; 및
드론(20)을 수용하기 위한 내부공간이 마련되고 상기 내부공간의 상부는 개구되어 수용된 드론(20)이 출입하는 통로를 형성하며 하부가 상기 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 개폐동작하는데 필요한 구동력을 제공하는 개폐구동부(130)를 포함하는 드론격납고(100);를 포함하고,
상기 드론(20)의 중앙부에 배치되고 수직으로 하향 연장된 수직바(240); 및
상기 적재함(13) 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 포함하고,
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 구획산(214)이 형성되며,
상기 수직바(240)는 자성체 재질로 이루어지며 둘레에는 둘레에는 측방으로 오목하게 함몰된 고정홈(243)이 형성되고, 상기 삽입공(212) 상에서 삽입된 수직바(240)의 고정홈과(243) 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 록킹하는 것을 특징으로 하는 픽업트럭용 드론운용 시스템.A drone operation system for pickup trucks that is installed on a pickup truck 10 with a front row seat 11 and a rear row seat 12 in the indoor space and a loading box 13 opened upward at the rear, and used to operate the drone 20 In,
A ground control device disposed in the rear seat 12 and outputting a control signal for controlling the flight 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 received drone 20 enters and exits, and the lower part is inserted into the loading box 13 to be fixedly mounted. ), and a storage cover 120 that is mounted on an upper portion of the storage body 110 and opens and closes an opened passage while sliding or rotating, and an opening/closing driver 130 that provides a driving force required for the opening and closing operation of the storage cover 120 ), including a drone hangar 100; including,
A vertical bar 240 disposed at the center of the drone 20 and extending vertically downward; And
It is disposed horizontally in the loading box 13 and is opened up and down in the central portion to form an insertion hole 212 through which the vertical bar 240 is inserted downwardly, and the diameter gradually increases toward the top around the insertion hole 212. A mounting plate 210 for guiding the lower end of the vertical bar 240 in contact with the surface of the guide groove 211 to slide toward the upper end of the insertion hole 212 by forming a guide groove 211 in an enlarged shape; Including,
On the inner surface of the guide groove 211, a plurality of concave bones 215 extending upward from the top to the bottom of the guide groove 211 while having an arc shape with a flat cross-section opening laterally toward the center of the guide groove 211 Doedoe formed continuously along the circumference, while each concave bone 215 is arranged in close contact along the circumference of the guide groove 211, a sharply raised compartment mountain 214 is formed between the adjacent two concave bones 215 And
The vertical bar 240 is made of a magnetic material, and has a circumferentially concave fixing groove 243 formed therein, and a fixing groove of the vertical bar 240 inserted in the insertion hole 212 ( 243) A pull-out hole 216 opened laterally is formed at a corresponding position, and an electromagnet 217 mounted to be pulled laterally through a pull-out hole 216 is disposed around the insertion hole 212, The electromagnet 217 is pulled outward by the elastic member 218 and disposed outside the withdrawal hole 216. When a driving power is applied and a magnetic field is formed, the electromagnet 217 is applied to the vertical bar 240 through the withdrawal hole 216. A drone operating system for a pickup truck, characterized in that it is inserted into the fixing groove 243 while being attached to selectively lock the inserted state of the vertical bar 240.
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