WO2022108223A1 - Charging system for unmanned vehicle - Google Patents

Charging system for unmanned vehicle Download PDF

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Publication number
WO2022108223A1
WO2022108223A1 PCT/KR2021/016338 KR2021016338W WO2022108223A1 WO 2022108223 A1 WO2022108223 A1 WO 2022108223A1 KR 2021016338 W KR2021016338 W KR 2021016338W WO 2022108223 A1 WO2022108223 A1 WO 2022108223A1
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WO
WIPO (PCT)
Prior art keywords
support
coupling
terminal part
lower terminal
charging station
Prior art date
Application number
PCT/KR2021/016338
Other languages
French (fr)
Korean (ko)
Inventor
박재영
Original Assignee
주식회사 하백소프트
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Publication of WO2022108223A1 publication Critical patent/WO2022108223A1/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION 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
    • B60L53/00Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/30Constructional details of charging stations
    • B60L53/31Charging columns specially adapted for electric vehicles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION 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
    • B60L3/00Electric devices on electrically-propelled vehicles for safety purposes; Monitoring operating variables, e.g. speed, deceleration or energy consumption
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION 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
    • B60L3/00Electric devices on electrically-propelled vehicles for safety purposes; Monitoring operating variables, e.g. speed, deceleration or energy consumption
    • B60L3/0007Measures or means for preventing or attenuating collisions
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION 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
    • B60L3/00Electric devices on electrically-propelled vehicles for safety purposes; Monitoring operating variables, e.g. speed, deceleration or energy consumption
    • B60L3/0023Detecting, eliminating, remedying or compensating for drive train abnormalities, e.g. failures within the drive train
    • B60L3/0069Detecting, eliminating, remedying or compensating for drive train abnormalities, e.g. failures within the drive train relating to the isolation, e.g. ground fault or leak current
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION 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
    • B60L53/00Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/10Methods 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
    • B60L53/12Inductive energy transfer
    • B60L53/124Detection or removal of foreign bodies
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION 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
    • B60L53/00Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/30Constructional details of charging stations
    • B60L53/35Means for automatic or assisted adjustment of the relative position of charging devices and vehicles
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R13/00Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
    • H01R13/02Contact members
    • H01R13/04Pins or blades for co-operation with sockets
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0042Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction
    • H02J7/0045Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction concerning the insertion or the connection of the batteries
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/70Energy storage systems for electromobility, e.g. batteries

Definitions

  • the present invention relates to a charging system, and more particularly, to a charging system for an unmanned mobile body for solving a problem of a position error and an electric leakage caused by foreign substances in the process of charging the unmanned mobile body by docking it at a charging station.
  • An unmanned vehicle is a vehicle that can perform a mission by judging the situation by itself, and typical examples include drones and autonomous vehicles.
  • UAV unmanned aerial vehicle
  • the unmanned moving object recognizes its location through GPS or IMU, etc.
  • the contact power supply method when used, there is a problem in that malfunctions due to position errors and leakage and sparks occur due to foreign substances during the contact process.
  • Korean Patent Application Laid-Open No. 10-2017-0083856 discloses the contents of “vertical take-off and landing drone and docking station”.
  • the disclosed rule take-off and landing drone and docking station are vertical take-off and landing drones that take off and land at a docking station including a first guide area for inducing landing and a second guide area for distinguishing the polarity of a charging power source.
  • a pair of built-in batteries are disposed symmetrically around the induction rod and the induction rod corresponding to the first guide area, and are connected to the power supply unit supplying power to the induction rod through the built-in battery and each built-in battery and skid on the charging pads of two polarities disposed at the boundary of the second guide region, and include a charging terminal for transferring the charging power of the charging pad to the built-in battery.
  • the disclosed charging system discloses content for overcoming the position error to some extent through the first guide region for inducing landing and the second guide region for separating the polarity of the charging power, it is still a malfunction and contact process due to the position error. There was a problem in that electric leakage and sparks were generated by foreign substances in the
  • the charging system for an unmanned moving object includes a first support part formed to be spaced apart from each other by a predetermined interval, a lower terminal part disposed on the upper part of the first support part and convexly protruding upward, a charging station for supplying power to the mobile body; A second support part provided in the movable body to receive power from the charging station, a second support part provided under the movable body, an elastic part disposed between the second support part and the movable body to provide an elastic force to the second support part; 2 It is characterized in that it includes a docking part disposed under the support part and formed to be concave to correspond to the lower terminal part and including an upper terminal part in contact with the lower terminal part.
  • the lower terminal part is a first coupling part convexly formed to protrude upward from the first support part, and a first terminal part disposed at the center of the first coupling part to supply power. , formed at the edge of the first coupling part, absorbing shock during the docking process with the docking part, and characterized in that it comprises a damper for preventing the inflow of foreign substances into the first terminal part.
  • the upper terminal part is provided under the second support part, is formed concavely to correspond to the first coupling part, and is a second coupling part coupled to the first coupling part.
  • a second terminal part disposed in the center of the second coupling part to be supplied with power in contact with the first terminal part, provided in the second coupling part, before being coupled to the lower terminal part, air (air) into the first coupling part is characterized in that it includes a spraying unit for removing foreign substances by spraying.
  • the first terminal part and the second terminal part are characterized in that they are magnetic.
  • the charging system for an unmanned moving object can minimize the occurrence of electric leakage by overcoming a position error and preventing foreign substances from accumulating by forming the lower terminal part of the charging station to be convex and the upper terminal part of the docking part to be concave. .
  • the charging system of the unmanned moving object according to the present invention can minimize the occurrence of electric leakage by spraying air to the lower terminal portion of the charging station before docking, thereby removing foreign substances from the lower terminal portion.
  • the charging system of the unmanned moving object according to the present invention can prevent the inflow of foreign substances by providing a damper in the lower terminal part, reduce the contact impact between the docking part and the charging station, and increase the bonding force.
  • FIG. 1 is a block diagram illustrating a charging system for an unmanned moving object according to an embodiment of the present invention.
  • FIG. 2 is a perspective view illustrating a charging system for an unmanned moving object according to an embodiment of the present invention.
  • FIG. 3 is a side cross-sectional view illustrating a charging system for an unmanned moving object according to an embodiment of the present invention.
  • 4 to 7 are diagrams for explaining a docking process of the charging system of an unmanned moving object according to an embodiment of the present invention.
  • FIG. 1 is a block diagram showing a charging system for an unmanned moving object according to an embodiment of the present invention
  • FIG. 2 is a perspective view showing a charging system for an unmanned moving object according to an embodiment of the present invention
  • FIG. 3 is an embodiment of the present invention It is a cross-sectional side view showing a charging system for an unmanned moving object according to the present invention
  • FIGS. 4 to 7 are views for explaining a docking process of the charging system for an unmanned moving object according to an embodiment of the present invention.
  • a charging system 300 is configured to include an unmanned moving object 100 and a charging station 200 .
  • the unmanned moving object 100 is a moving object capable of performing a task by determining the situation by itself, and may include a drone, a car, a ship, and the like. In the following description, it is assumed that the unmanned moving object 100 is a drone. Meanwhile, in the following description, using a drone as an example, the charging station 200 is provided in the lower part, but the charging station 200 and the unmanned mobile body 100 are reversed, or a part of the charging station 200 and the unmanned mobile body Some components of (100) may be formed in an inverted form.
  • the unmanned moving object 100 may include a sensing unit 110 , a battery 120 , a docking unit 130 , and a control unit 140 .
  • the sensing unit 110 may sense a position with the charging station 200 by using the force of an electromagnetic field without physical contact. That is, the sensing unit 110 may sense that the docking unit 130 approaches the charging station 200 by a predetermined distance.
  • Various types of proximity sensors such as a magnetic proximity sensor, an optical proximity sensor, an ultrasonic proximity sensor, an inductive proximity sensor, a capacitive proximity sensor, and an eddy current proximity sensor may be applied to the sensing unit 110 .
  • the battery 120 supplies power for driving the unmanned mobile body 100, and receives power from the charging station 200 through the docking unit 130 to charge the power or discharge the charged power to the unmanned mobile body ( 100) can be driven.
  • the battery 120 includes a nickel-cadmium battery, a lead storage battery, a nickel metal hydride battery (NiMH), a lithium ion battery, and a lithium iron phosphate battery (lithium- ion phosphate battery), lithium polymer battery, etc., but is not limited thereto, and various types of batteries may be used.
  • the docking unit 130 may be coupled to the charging station 200 and serve to receive power from the charging station 200 .
  • the docking part 130 may include a second support part 131 , an elastic part 132 , an upper terminal part 133 , and a connection part 134 .
  • the second support part 131 is coupled to the body portion of the unmanned moving object through the connection part 134 , and may support the upper terminal part 133 .
  • the second support 131 may preferably be provided at the bottom of the unmanned moving body in the form of a bar, and a space is provided so that the (+) terminal and the (-) terminal of the upper terminal part 133 can be sufficiently spaced apart. Thus, the leakage current can be minimized.
  • the second support part 131 may be formed of a flexible material.
  • the second support 131 may be formed of a material including silicone, urethane, rubber, or the like. Through this, the second support 131 may be prevented from being damaged in the process of making contact with the first support 210 , and may serve to increase the contact force with the first support 210 .
  • the elastic part 132 may be disposed between the second support part 131 and the unmanned moving object to provide an elastic force to the second support part 131 . That is, the elastic part 132 may provide an elastic force from the unmanned moving object toward the charging station 200 to support the upper terminal part 133 to be more firmly attached to the charging station 200 .
  • the elastic part 132 may have a passage through which air moves therein.
  • the elastic unit 132 may serve to inject air from the body of the unmanned moving object 100 to the injection unit through the passage.
  • the elastic part 132 may serve to move the power received from the charging station 200 to the battery 120 .
  • the upper terminal part 133 may include a second coupling part 133a, a second terminal part 133b, and a spraying part (not shown).
  • the second coupling part 133a is provided under the second support part 131 and is concavely formed in a shape corresponding to the first coupling part 221 of the lower terminal part 220 to be described later, and thus the first coupling part 221 .
  • the second coupling part 133a may be formed of a magnetic material having a different polarity from that of the first coupling part 221 , and may be attached to the first coupling part 221 through magnetism. Through this, the second coupling part 133a may be coupled to each other at an accurate position even if there is a gap due to a position error with the first coupling part 221 .
  • the second terminal part 133b may be disposed in the center of the second coupling part 133a and may be in contact with the first terminal part 222 of the lower terminal part 220 to be described later to receive power from the first terminal part 222 .
  • the spraying unit may be provided in the second coupling part 133a to spray air into the first coupling part 221 before being coupled to the lower terminal part 220 to remove foreign substances.
  • the docking unit 130 includes a spraying unit to remove foreign substances on the upper portion of the first coupling unit 221 through air before docking and then remove it, thereby preventing the leakage problem in advance.
  • the injection part may be configured to penetrate the second coupling part 133a or to penetrate the second terminal part 133b.
  • connection part 134 connects the body of the unmanned moving body and the second coupling part 133a to each other.
  • the connecting portion 134 may include an elevating device to lower the second coupling portion 133a in the direction of the first coupling portion 221 or lift the lowered first coupling portion 221 .
  • the connection part 134 may be provided under the unmanned moving body to connect the second coupling part 133a.
  • the controller 140 controls the overall operation of the unmanned moving object. Specific details of the control unit 140 will be described later after the structure of the charging station 200 is described.
  • the charging station 200 may serve to supply power to an unmanned moving object.
  • the charging station 200 includes a first support part 210 and a lower terminal part 220 .
  • the first support parts 210 may be provided as a pair and formed to be spaced apart from each other by a predetermined interval. That is, the first support part 210 may be provided as a pair to arrange the (+) terminal and the (-) terminal of the lower terminal part 220, so that the (+) terminal and the (-) terminal can be sufficiently spaced apart. Leakage current can be minimized by providing space.
  • the lower terminal unit 220 may be disposed on the upper portion of the first support unit 210 , and may convexly protrude upward to supply power to the docking unit 130 .
  • the lower terminal part 220 may include a first coupling part 221 , a first terminal part 222 , and a damper 223 .
  • the first coupling part 221 may be formed to protrude upward from the first support part 210 , and may be coupled to the above-described second coupling part 133a. Since the first coupling part 221 is formed to protrude upwardly, it is possible to minimize the phenomenon of water pooling. Also, the first coupling part 221 may be formed of a magnetic material having a different polarity from that of the second coupling part 133a, and may be attached to the second coupling part 133a through magnetism. Through this, the first coupling part 221 may be coupled to each other at an accurate position even if there is a gap due to a position error with the second coupling part 133a. For example, the first coupling part 221 may be formed in a hemispherical shape.
  • the first coupling part 221 may not be formed of a magnetic material, but may be formed of a metal in contact with the magnetic material. Accordingly, the first coupling part 221 may contact the second coupling part 133a formed of a magnetic material. Through this, it is possible to overcome the position error and prevent foreign substances from being attached to the second coupling part 133a by magnetism.
  • the first terminal part 222 may be disposed at the center of the first coupling part 221 to supply power to the docking part 130 through the above-described second terminal part 133b.
  • the first terminal portion 222 may be positioned at the center of the uppermost portion of the convexly formed first coupling portion 221 to prevent short circuit.
  • the damper 233 is formed on the edge of the first coupling part 221 , absorbs an impact during the docking process with the docking part 130 , and may prevent the inflow of foreign substances into the first terminal part 212 .
  • the damper 233 is formed of an elastic material such as rubber or silicone, and is elastically deformed during docking, thereby increasing the bonding force between the second coupling part 133a and the first coupling part 221 .
  • the control unit 140 establishes a vertical position with the charging station 200 through GPS or IMU, and then connects the second support unit 131 through the connection unit 134 to the charging station 200 .
  • direction can be lowered.
  • the controller 140 may stop the lowering operation.
  • the control unit 140 stops the descending operation and blows air through the injection unit to the first coupling unit 221 . ), it is possible to remove foreign substances on the first coupling part 221 and the first terminal part 222 .
  • control unit 140 may lower the second support unit 131 in the direction of the charging station 200 through the connection unit 134 .
  • the controller 140 may receive power from the charging station 200 when the docking unit 130 and the charging station 200 are in close contact with each other.
  • the lower terminal part 220 of the charging station 200 is convex, and the upper terminal part 133a of the docking part 130 is concave.
  • the charging system 300 of the unmanned moving object injects air into the lower terminal part 220 of the charging station 200 before docking, thereby removing foreign substances from the lower terminal part 220 to minimize the occurrence of electric leakage. can do.
  • the charging system 300 of the unmanned moving object includes a damper 223 on the lower terminal part 220 to prevent the inflow of foreign substances, and the docking part 130 and the charging station 200 . It can reduce the impact between the liver and increase the bonding force.
  • second support part 132 elastic part
  • receiving terminal portion 133a second coupling portion
  • control unit 200 charging station
  • first support 220 supply terminal unit
  • first coupling part 222 first terminal part
  • damper 300 charging system

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

The present invention relates to a charging system, for an unmanned vehicle, for solving the problems of positioning error and short circuit due to foreign materials when the unmanned vehicle is docked on a charging station and is being charged. The charging system for an unmanned vehicle according to the present invention comprises: a charging station comprising first support parts and lower terminal parts and supplying a power source to the vehicle, the first support parts formed a predetermined distance away from each other, and the lower terminal parts respectively disposed on the first support parts, protruding so as to be rounded upward and supplying the power source; and a docking unit provided on the vehicle, receiving the power source from the charging station, and comprising second support parts, which are provided below the vehicle, elastic parts, which are respectively disposed between the second support parts and the vehicle to provide elasticity to the second support parts, and upper terminal parts which are respectively disposed on the bottom part of the second support parts, are depressively formed so as to correspond to the lower terminal parts, and come into contact with the lower terminal parts to receive the power source.

Description

무인 이동체의 충전 시스템Unmanned vehicle charging system
본 발명은 충전 시스템에 관한 것으로, 더욱 상세하게는 무인 이동체가 충전 스테이션에 도킹하여 충전을 수행하는 과정에서 위치 오차와, 이물질에 따른 누전 문제를 해결하기 위한 무인 이동체의 충전 시스템에 관한 것이다.The present invention relates to a charging system, and more particularly, to a charging system for an unmanned mobile body for solving a problem of a position error and an electric leakage caused by foreign substances in the process of charging the unmanned mobile body by docking it at a charging station.
무인 이동체는 스스로 상황을 판단하여 임무를 수행할 수 있는 이동체로 드론 및 자율주행 자동차 등이 대표적이다.An unmanned vehicle is a vehicle that can perform a mission by judging the situation by itself, and typical examples include drones and autonomous vehicles.
최근에는 무인 이동체 수요급증에 대응하고, 다양한 종류의 무인이동체에 공통적으로 적용할 수 있는 무인 이동체 공통기술, 향후 무인기 분야 산업변화에 대응할 수 있는 차세대 무인 이동체 원천기술, 소형무인기 성능향상을 위한 소형무인기 기반기술 및 공공혁신조달 연계 소형 무인기 기술, 저고도 무인기의 교통을 감시관리하는 저고도 무인 비행장치 교통관리 감시기술 등의 개발이 활발히 진행되고 있다.Recently, in response to the rapid increase in demand for unmanned vehicles, common technology for unmanned vehicles that can be commonly applied to various types of unmanned vehicles, next-generation unmanned vehicle source technology that can respond to industrial changes in the future unmanned aerial vehicles, and small unmanned aerial vehicles to improve performance of small unmanned aerial vehicles The development of low-altitude unmanned aerial vehicle (UAV) traffic management monitoring technology that monitors and manages low-altitude unmanned aerial vehicle traffic is being actively developed.
이러한 무인 이동체를 충전하기 위해서 비접촉식 전원 공급 방법이 많이 사용되고 있으나, 장시간이 소요되기 때문에 결과적으로 접촉식 전원 공급을 효율적으로 할 수 있는 방안이 필요한 실정이다.In order to charge such an unmanned moving object, a non-contact power supply method is widely used, but it takes a long time. As a result, a method for efficiently supplying the contact power supply is required.
여기서 무인 이동체는 GPS나 IMU 등을 통해 자신의 위치를 인지하게 되는데, 접촉식 전원 공급 방법을 사용할 경우, 위치 오차에 따른 오작동과, 접촉 과정에서 이물질에 의해 누전 및 스파크가 발생하는 문제점이 있었다.Here, the unmanned moving object recognizes its location through GPS or IMU, etc. However, when the contact power supply method is used, there is a problem in that malfunctions due to position errors and leakage and sparks occur due to foreign substances during the contact process.
한편 한국공개특허 제10-2017-0083856호에는 "수직이착륙 드론 및 도킹 스테이션"에 관한 내용을 개시하고 있다.Meanwhile, Korean Patent Application Laid-Open No. 10-2017-0083856 discloses the contents of “vertical take-off and landing drone and docking station”.
개시된 수칙이착륙 드론 및 도킹 스테이션은 착지를 유도하는 제1 가이드 영역 및 충전 전원의 극성을 구분하는 제2 가이드 영역을 포함하는 도킹 스테이션에 이착륙하는 수직이착륙 드론에 있어서, 기체부, 기체부에 동력을 전달하고, 제1 가이드 영역에 대응하여 하는 유도봉, 유도봉을 중심으로 대칭되게 한 쌍의 내장형 배터리가 배치되고, 내장형 배터리를 통하여 유도봉의 전원을 공급하는 전원부 및 각각의 내장형 배터리와 대응되게 연결되고, 제2 가이드 영역의 경계로 배치되는 2개 극성의 충전 패드에 스키드(skid)하며, 충전 패드의 충전 전원을 내장형 배터리로 전달하는 충전 단자를 포함한다.The disclosed rule take-off and landing drone and docking station are vertical take-off and landing drones that take off and land at a docking station including a first guide area for inducing landing and a second guide area for distinguishing the polarity of a charging power source. A pair of built-in batteries are disposed symmetrically around the induction rod and the induction rod corresponding to the first guide area, and are connected to the power supply unit supplying power to the induction rod through the built-in battery and each built-in battery and skid on the charging pads of two polarities disposed at the boundary of the second guide region, and include a charging terminal for transferring the charging power of the charging pad to the built-in battery.
개시된 충전 시스템은 착지를 유도하는 제1 가이드 영역 및 충전 전원의 극성을 구분하는 제2 가이드 영역을 통해 위치 오차를 어느 정도 극복하기 위한 내용을 개시하고 있으나, 여전히 위치 오차에 따른 오작동과, 접촉 과정에서 이물질에 의해 누전 및 스파크가 발생하는 문제점이 있었다.Although the disclosed charging system discloses content for overcoming the position error to some extent through the first guide region for inducing landing and the second guide region for separating the polarity of the charging power, it is still a malfunction and contact process due to the position error. There was a problem in that electric leakage and sparks were generated by foreign substances in the
따라서 본 발명의 목적은 무인 이동체가 충전 스테이션에 도킹하여 충전을 수행하는 과정에서 위치 오차와, 이물질에 따른 누전 문제를 해결하기 위한 무인 이동체의 충전 시스템을 제공하는 데 있다.Accordingly, it is an object of the present invention to provide a charging system for an unmanned moving object for solving a position error and an electric leakage problem due to foreign substances in the process of charging the unmanned moving object by docking it at a charging station.
본 발명에 따른 무인 이동체의 충전 시스템은 일정 간격 이격되어 형성되는 제1 지지부, 상기 제1 지지부의 상부에 배치되며 상부로 볼록하게 돌출되는 하부 단자부를 포함하여, 이동체에 전원을 공급하는 충전 스테이션, 상기 이동체에 구비되어 상기 충전 스테이션으로부터 전원을 공급받으며, 상기 이동체의 하부에 구비되는 제2 지지부, 상기 제2 지지부와 상기 이동체 사이에 배치되어 상기 제2 지지부에 탄성력을 제공하는 탄성부, 상기 제2 지지부의 하부에 배치되어 상기 하부 단자부와 대응되도록 오목하게 형성되며 상기 하부 단자부와 접촉하는 상부 단자부를 포함하는 도킹부를 포함하는 것을 특징으로 한다.The charging system for an unmanned moving object according to the present invention includes a first support part formed to be spaced apart from each other by a predetermined interval, a lower terminal part disposed on the upper part of the first support part and convexly protruding upward, a charging station for supplying power to the mobile body; A second support part provided in the movable body to receive power from the charging station, a second support part provided under the movable body, an elastic part disposed between the second support part and the movable body to provide an elastic force to the second support part; 2 It is characterized in that it includes a docking part disposed under the support part and formed to be concave to correspond to the lower terminal part and including an upper terminal part in contact with the lower terminal part.
본 발명에 따른 무인 이동체의 충전 시스템에 있어서, 상기 하부 단자부는 상기 제1 지지부로부터 상부로 볼록하게 돌출되어 형성되는 제1 결합부, 상기 제1 결합부의 중심부에 배치되어 전원을 공급하는 제1 단자부, 상기 제1 결합부의 가장자리에 형성되며, 상기 도킹부와 도킹 과정에서 충격을 흡수하고, 상기 제1 단자부로의 이물질 유입을 방지하는 댐퍼를 포함하는 것을 특징으로 한다.In the charging system of the unmanned moving object according to the present invention, the lower terminal part is a first coupling part convexly formed to protrude upward from the first support part, and a first terminal part disposed at the center of the first coupling part to supply power. , formed at the edge of the first coupling part, absorbing shock during the docking process with the docking part, and characterized in that it comprises a damper for preventing the inflow of foreign substances into the first terminal part.
본 발명에 따른 무인 이동체의 충전 시스템에 있어서, 상기 상부 단자부는 상기 제2 지지부의 하부에 구비되며, 상기 제1 결합부와 대응되도록 오목하게 형성되어 상기 제1 결합부와 결합되는 제2 결합부, 상기 제2 결합부의 중심부에 배치되어 상기 제1 단자부와 접촉하여 전원을 공급받는 제2 단자부, 상기 제2 결합부에 구비되어, 상기 하부 단자부와 결합되기 이전에 상기 제1 결합부로 공기(air)를 분사하여 이물질을 제거하는 분사부를 포함하는 것을 특징으로 한다.In the charging system of the unmanned moving body according to the present invention, the upper terminal part is provided under the second support part, is formed concavely to correspond to the first coupling part, and is a second coupling part coupled to the first coupling part. , a second terminal part disposed in the center of the second coupling part to be supplied with power in contact with the first terminal part, provided in the second coupling part, before being coupled to the lower terminal part, air (air) into the first coupling part ) is characterized in that it includes a spraying unit for removing foreign substances by spraying.
본 발명에 따른 무인 이동체의 충전 시스템에 있어서, 상기 제1 단자부 및 상기 제2 단자부는 자성체인 것을 특징으로 한다.In the charging system for an unmanned moving object according to the present invention, the first terminal part and the second terminal part are characterized in that they are magnetic.
본 발명에 따른 무인 이동체의 충전 시스템은 충전 스테이션의 하부 단자부를 볼록하게 형성하고, 도킹부의 상부 단자부를 오목하게 형성함으로써, 위치 오차를 극복하고, 이물질이 쌓이는 것을 방지하여 누전 발생을 최소화할 수 있다.The charging system for an unmanned moving object according to the present invention can minimize the occurrence of electric leakage by overcoming a position error and preventing foreign substances from accumulating by forming the lower terminal part of the charging station to be convex and the upper terminal part of the docking part to be concave. .
또한 본 발명에 따른 무인 이동체의 충전 시스템은 도킹전 충전 스테이션의 하부 단자부로 공기를 분사함으로써, 하부 단자부의 이물질을 제거하여 누전 발생을 최소화할 수 있다.In addition, the charging system of the unmanned moving object according to the present invention can minimize the occurrence of electric leakage by spraying air to the lower terminal portion of the charging station before docking, thereby removing foreign substances from the lower terminal portion.
또한 본 발명에 따른 무인 이동체의 충전 시스템은 하부 단자부에 댐퍼를 구비하여 외부 이물질 유입을 방지할 수 있으며, 도킹부와 충전 스테이션간의 접촉 충격을 줄이고, 결속력을 높일 수 있다.In addition, the charging system of the unmanned moving object according to the present invention can prevent the inflow of foreign substances by providing a damper in the lower terminal part, reduce the contact impact between the docking part and the charging station, and increase the bonding force.
도 1은 본 발명의 실시예에 따른 무인 이동체의 충전 시스템을 나타낸 블록도이다.1 is a block diagram illustrating a charging system for an unmanned moving object according to an embodiment of the present invention.
도 2는 본 발명의 실시예에 따른 무인 이동체의 충전 시스템을 나타낸 사시도이다.2 is a perspective view illustrating a charging system for an unmanned moving object according to an embodiment of the present invention.
도 3은 본 발명의 실시예에 따른 무인 이동체의 충전 시스템을 나타낸 측단면도이다.3 is a side cross-sectional view illustrating a charging system for an unmanned moving object according to an embodiment of the present invention.
도 4 내지 도 7은 본 발명의 실시예에 따른 무인 이동체의 충전 시스템의 도킹 과정을 설명하기 위한 도면이다.4 to 7 are diagrams for explaining a docking process of the charging system of an unmanned moving object according to an embodiment of the present invention.
본 발명의 상세한 설명에 앞서, 이하에서 설명되는 본 명세서 및 청구범위에 사용된 용어나 단어는 통상적이거나 사전적인 의미로 한정해서 해석되어서는 아니 되며, 발명자는 그 자신의 발명을 가장 최선의 방법으로 설명하기 위해 용어의 개념으로 적절하게 정의할 수 있다는 원칙에 입각하여 본 발명의 기술적 사상에 부합하는 의미와 개념으로 해석되어야만 한다. 따라서 본 명세서에 기재된 실시예와 도면에 도시된 구성은 본 발명의 가장 바람직한 실시예에 불과할 뿐, 본 발명의 기술적 사상을 모두 대변하는 것은 아니므로, 본 출원시점에 있어서 이들을 대체할 수 있는 다양한 균등물과 변형 예들이 있을 수 있음을 이해하여야 한다. Prior to the detailed description of the present invention, the terms or words used in the present specification and claims described below should not be construed as being limited to their ordinary or dictionary meanings, and the inventors should develop their own inventions in the best way. It should be interpreted as meaning and concept consistent with the technical idea of the present invention based on the principle that it can be appropriately defined as a concept of a term for explanation. Therefore, the embodiments described in the present specification and the configurations shown in the drawings are only the most preferred embodiments of the present invention, and do not represent all the technical spirit of the present invention, so various equivalents that can be substituted for them at the time of the present application It should be understood that there may be water and variations.
이하, 첨부된 도면을 참조하여 본 발명의 바람직한 실시예들을 상세히 설명한다. 이때, 첨부된 도면에서 동일한 구성 요소는 가능한 동일한 부호로 나타내고 있음을 유의해야 한다. 또한, 본 발명의 요지를 흐리게 할 수 있는 공지 기능 및 구성에 대한 상세한 설명은 생략할 것이다. 마찬가지의 이유로 첨부 도면에 있어서 일부 구성요소는 과장되거나 생략되거나 또는 개략적으로 도시되었으며, 각 구성요소의 크기는 실제 크기를 전적으로 반영하는 것이 아니다.Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings. In this case, it should be noted that in the accompanying drawings, the same components are denoted by the same reference numerals as much as possible. In addition, detailed descriptions of well-known functions and configurations that may obscure the gist of the present invention will be omitted. For the same reason, some components are exaggerated, omitted, or schematically illustrated in the accompanying drawings, and the size of each component does not fully reflect the actual size.
도 1은 본 발명의 실시예에 따른 무인 이동체의 충전 시스템을 나타낸 블록도이고, 도 2는 본 발명의 실시예에 따른 무인 이동체의 충전 시스템을 나타낸 사시도이고, 도 3은 본 발명의 실시예에 따른 무인 이동체의 충전 시스템을 나타낸 측단면도이고, 도 4 내지 도 7은 본 발명의 실시예에 따른 무인 이동체의 충전 시스템의 도킹 과정을 설명하기 위한 도면이다.1 is a block diagram showing a charging system for an unmanned moving object according to an embodiment of the present invention, FIG. 2 is a perspective view showing a charging system for an unmanned moving object according to an embodiment of the present invention, and FIG. 3 is an embodiment of the present invention It is a cross-sectional side view showing a charging system for an unmanned moving object according to the present invention, and FIGS. 4 to 7 are views for explaining a docking process of the charging system for an unmanned moving object according to an embodiment of the present invention.
도 1 내지 도 7을 참조하면, 본 발명의 실시예에 따른 충전 시스템(300)은 무인 이동체(100) 및 충전 스테이션(200)을 포함하여 구성된다.1 to 7 , a charging system 300 according to an embodiment of the present invention is configured to include an unmanned moving object 100 and a charging station 200 .
무인 이동체(100)는 스스로 상황을 판단하여 임무를 수행할 수 있는 이동체로 드론, 자동차, 선박 등이 포함될 수 있다. 이하 설명에서는 무인 이동체(100)가 드론(Drone)인 것으로 가정하고 설명하도록 한다. 한편 하기의 설명에서는 드론을 예로 하여 하부에 충전 스테이션(200)이 구비되는 것으로 설명하지만, 충전 스테이션(200)과 무인 이동체(100)가 반전되거나, 충전 스테이션(200)의 일부 구성과, 무인 이동체(100)의 일부 구성이 반전되는 형태로 형성될 수 있다.The unmanned moving object 100 is a moving object capable of performing a task by determining the situation by itself, and may include a drone, a car, a ship, and the like. In the following description, it is assumed that the unmanned moving object 100 is a drone. Meanwhile, in the following description, using a drone as an example, the charging station 200 is provided in the lower part, but the charging station 200 and the unmanned mobile body 100 are reversed, or a part of the charging station 200 and the unmanned mobile body Some components of (100) may be formed in an inverted form.
이러한 무인 이동체(100)는 센싱부(110), 배터리(120), 도킹부(130) 및 제어부(140)를 포함하여 구성될 수 있다.The unmanned moving object 100 may include a sensing unit 110 , a battery 120 , a docking unit 130 , and a control unit 140 .
센싱부(110)는 물리적인 접촉없이 전자계의 힘을 이용하여 충전 스테이션(200)과의 위치를 센싱할 수 있다. 즉 센싱부(110)는 도킹부(130)가 충전 스테이션(200)에 일정 거리로 근접한 것을 센싱할 수 있다. 이러한 센싱부(110)는 자기 근접 센서, 광학 근접 센서, 초음파 근접 센서, 유도성 근접 센서, 용량성 근접 센서, 와전류 근접 센서 등 다양한 종류의 근접 센서가 적용될 수 있다.The sensing unit 110 may sense a position with the charging station 200 by using the force of an electromagnetic field without physical contact. That is, the sensing unit 110 may sense that the docking unit 130 approaches the charging station 200 by a predetermined distance. Various types of proximity sensors such as a magnetic proximity sensor, an optical proximity sensor, an ultrasonic proximity sensor, an inductive proximity sensor, a capacitive proximity sensor, and an eddy current proximity sensor may be applied to the sensing unit 110 .
배터리(120)는 무인 이동체(100)를 구동하기 위한 전원을 공급하며, 도킹부(130)를 통해 충전 스테이션(200)으로부터 전원을 공급받아 전원이 충전되거나, 충전된 전원을 방전하여 무인 이동체(100)를 구동시킬 수 있다. 이러한 배터리(120)는 니켈-카드뮴 전지(nickel-cadmium battery), 납 축전지, 니켈-수소 전지(NiMH: nickel metal hydride battey), 리튬 이온 전지(lithium ion battery), 리튬인산철 이온 전지(lithium-ion Phosphate Battery), 리튬 폴리머 전지(lithium polymer battery) 등을 포함할 수 있으나 이에 한정된 것은 아니고, 다양한 종류의 전지가 사용될 수 있다.The battery 120 supplies power for driving the unmanned mobile body 100, and receives power from the charging station 200 through the docking unit 130 to charge the power or discharge the charged power to the unmanned mobile body ( 100) can be driven. The battery 120 includes a nickel-cadmium battery, a lead storage battery, a nickel metal hydride battery (NiMH), a lithium ion battery, and a lithium iron phosphate battery (lithium- ion phosphate battery), lithium polymer battery, etc., but is not limited thereto, and various types of batteries may be used.
도킹부(130)는 충전 스테이션(200)에 결합되어, 충전 스테이션(200)으로부터 전원을 공급받는 역할을 수행할 수 있다.The docking unit 130 may be coupled to the charging station 200 and serve to receive power from the charging station 200 .
이러한 도킹부(130)는 제2 지지부(131), 탄성부(132), 상부 단자부(133) 및 연결부(134)를 포함하여 구성될 수 있다.The docking part 130 may include a second support part 131 , an elastic part 132 , an upper terminal part 133 , and a connection part 134 .
제2 지지부(131)는 연결부(134)를 통해 무인 이동체의 몸체 부분에 결합되며, 상부 단자부(133)를 지지할 수 있다. 이러한 제2 지지부(131)는 바람직하게 바(bar) 형태로 무인 이동체의 하부에 구비될 수 있으며, 상부 단자부(133)의 (+) 단자와 (-) 단자가 충분히 이격될 수 있도록 공간을 마련하여 누설 전류를 최소화 할 수 있다. 한편 제2 지지부(131)는 플렉시블한 재질로 형성될 수 있다. 예를 들어 제2 지지부(131)는 실리콘, 우레탄, 고무 등을 포함하는 재질로 형성될 수 있다. 이를 통해 제2 지지부(131)는 제1 지지부(210)와 접촉하는 과정에서 파손을 방지할 수 있으며, 제1 지지부(210)와의 접촉력을 높이는 역할을 할 수 있다.The second support part 131 is coupled to the body portion of the unmanned moving object through the connection part 134 , and may support the upper terminal part 133 . The second support 131 may preferably be provided at the bottom of the unmanned moving body in the form of a bar, and a space is provided so that the (+) terminal and the (-) terminal of the upper terminal part 133 can be sufficiently spaced apart. Thus, the leakage current can be minimized. Meanwhile, the second support part 131 may be formed of a flexible material. For example, the second support 131 may be formed of a material including silicone, urethane, rubber, or the like. Through this, the second support 131 may be prevented from being damaged in the process of making contact with the first support 210 , and may serve to increase the contact force with the first support 210 .
탄성부(132)는 제2 지지부(131)와 무인 이동체 사이에 배치되어 제2 지지부(131)에 탄성력을 제공할 수 있다. 즉 탄성부(132)는 무인 이동체로부터 충전 스테이션(200) 방향으로 탄성력을 제공하여 상부 단자부(133)가 충전 스테이션(200)에 더욱 견고히 밀착될 수 있도록 지원할 수 있다.The elastic part 132 may be disposed between the second support part 131 and the unmanned moving object to provide an elastic force to the second support part 131 . That is, the elastic part 132 may provide an elastic force from the unmanned moving object toward the charging station 200 to support the upper terminal part 133 to be more firmly attached to the charging station 200 .
또한 탄성부(132)는 내부에 공기가 이동하는 통로가 형성될 수 있다. 이를 통해 탄성부(132)는 무인 이동체(100)의 몸체로부터 공기가 주입되어, 통로를 통해 분사부로 공기를 주입하는 역할을 수행할 수 있다.In addition, the elastic part 132 may have a passage through which air moves therein. Through this, the elastic unit 132 may serve to inject air from the body of the unmanned moving object 100 to the injection unit through the passage.
또한 탄성부(132)는 충전 스테이션(200)으로부터 전달받은 전원을 배터리(120)로 이동시키는 역할을 수행할 수도 있다.In addition, the elastic part 132 may serve to move the power received from the charging station 200 to the battery 120 .
상부 단자부(133)는 제2 결합부(133a), 제2 단자부(133b) 및 분사부(미도시)를 포함하여 구성될 수 있다.The upper terminal part 133 may include a second coupling part 133a, a second terminal part 133b, and a spraying part (not shown).
제2 결합부(133a)는 제2 지지부(131)의 하부에 구비되며, 후술할 하부 단자부(220)의 제1 결합부(221)와 대응되는 형상으로 오목하게 형성되어 제1 결합부(221)와 결합될 수 있다. 이러한 제2 결합부(133a)는 제1 결합부(221)와 서로 다른 극성의 자성체(magnetic)로 형성되어, 제1 결합부(221)와 자성을 통해 부착될 수 있다. 이를 통해 제2 결합부(133a)은 제1 결합부(221)와의 위치 오차에 따른 유격이 있더라도 정확한 위치에 서로 결합될 수 있다.The second coupling part 133a is provided under the second support part 131 and is concavely formed in a shape corresponding to the first coupling part 221 of the lower terminal part 220 to be described later, and thus the first coupling part 221 . ) can be combined with The second coupling part 133a may be formed of a magnetic material having a different polarity from that of the first coupling part 221 , and may be attached to the first coupling part 221 through magnetism. Through this, the second coupling part 133a may be coupled to each other at an accurate position even if there is a gap due to a position error with the first coupling part 221 .
제2 단자부(133b)는 제2 결합부(133a)의 중심부에 배치되어 후술할 하부 단자부(220)의 제1 단자부(222)와 접촉하여 제1 단자부(222)로부터 전원을 공급받을 수 있다.The second terminal part 133b may be disposed in the center of the second coupling part 133a and may be in contact with the first terminal part 222 of the lower terminal part 220 to be described later to receive power from the first terminal part 222 .
분사부는 제2 결합부(133a)에 구비되어, 하부 단자부(220)와 결합되기 이전에 제1 결합부(221)로 공기(air)를 분사하여 이물질을 제거할 수 있다. 예를 들어, 비가 내린 이후에는 제1 결합부(221)의 상부에 빗물이 유입될 수 있고, 이는 누전 문제로 이어질 수 있다. 이에 따라 본 발명의 실시예에 따른 도킹부(130)는 분사부를 구비하여 도킹 전에 공기를 통해 제1 결합부(221)의 상부에 이물질을 제거한 후 제거를 실시함으로써, 누전 문제를 사전에 예방할 수 있다. 이러한 분사부는 도시되지는 않지만 제2 결합부(133a)를 관통하여 구성되거나, 제2 단자부(133b)를 관통하여 구성될 수 있다.The spraying unit may be provided in the second coupling part 133a to spray air into the first coupling part 221 before being coupled to the lower terminal part 220 to remove foreign substances. For example, after rain, rainwater may flow into the upper portion of the first coupling part 221 , which may lead to an electric leakage problem. Accordingly, the docking unit 130 according to the embodiment of the present invention includes a spraying unit to remove foreign substances on the upper portion of the first coupling unit 221 through air before docking and then remove it, thereby preventing the leakage problem in advance. have. Although not shown, the injection part may be configured to penetrate the second coupling part 133a or to penetrate the second terminal part 133b.
연결부(134)는 무인 이동체의 몸체와 제2 결합부(133a)를 서로 연결한다. 이러한 연결부(134)는 승하강 장치를 구비하여, 제2 결합부(133a)를 제1 결합부(221)방향으로 하강시키거나, 하강된 제1 결합부(221)를 상승시킬 수 있다. 바람직하게 연결부(134)는 무인 이동체의 하부에 구비되어 제2 결합부(133a)를 연결할 수 있다.The connection part 134 connects the body of the unmanned moving body and the second coupling part 133a to each other. The connecting portion 134 may include an elevating device to lower the second coupling portion 133a in the direction of the first coupling portion 221 or lift the lowered first coupling portion 221 . Preferably, the connection part 134 may be provided under the unmanned moving body to connect the second coupling part 133a.
제어부(140)는 무인 이동체의 전반적인 동작을 제어한다. 제어부(140)의 구체적인 내용은 충전 스테이션(200)의 구조를 설명한 후 후술하도록 한다.The controller 140 controls the overall operation of the unmanned moving object. Specific details of the control unit 140 will be described later after the structure of the charging station 200 is described.
충전 스테이션(200)은 무인 이동체에 전원을 공급하는 역할을 수행할 수 있다.The charging station 200 may serve to supply power to an unmanned moving object.
이러한 충전 스테이션(200)은 제1 지지부(210) 및 하부 단자부(220)를 포함한다.The charging station 200 includes a first support part 210 and a lower terminal part 220 .
제1 지지부(210)는 한 쌍으로 구비되어 일정 간격 이격되어 형성될 수 있다. 즉 제1 지지부(210)는 하부 단자부(220)의 (+) 단자와 (-) 단자를 배치하기 위하여 한 쌍으로 구비될 수 있으며, (+) 단자와 (-) 단자가 충분히 이격될 수 있도록 공간을 마련하여 누설 전류를 최소화 할 수 있다.The first support parts 210 may be provided as a pair and formed to be spaced apart from each other by a predetermined interval. That is, the first support part 210 may be provided as a pair to arrange the (+) terminal and the (-) terminal of the lower terminal part 220, so that the (+) terminal and the (-) terminal can be sufficiently spaced apart. Leakage current can be minimized by providing space.
하부 단자부(220)는 제1 지지부(210)의 상부에 배치되며, 상부로 볼록하게 돌출되어 전원을 도킹부(130)에 전원을 공급할 수 있다.The lower terminal unit 220 may be disposed on the upper portion of the first support unit 210 , and may convexly protrude upward to supply power to the docking unit 130 .
이러한 하부 단자부(220)는 제1 결합부(221), 제1 단자부(222) 및 댐퍼(223)을 포함할 수 있다.The lower terminal part 220 may include a first coupling part 221 , a first terminal part 222 , and a damper 223 .
제1 결합부(221)는 제1 지지부(210)로부터 상부로 볼록하게 돌출되어 형성되어, 상술한 제2 결합부(133a)에 결합될 수 있다. 이러한 제1 결합부(221)는 상부로 볼록하게 돌출되어 형성됨으로써, 물이 고이는 현상을 최소화할 수 있다. 또한 제1 결합부(221)는 제2 결합부(133a)와 서로 다른 극성의 자성체로 형성되어, 제2 결합부(133a)와 자성을 통해 부착될 수 있다. 이를 통해 제1 결합부(221)는 제2 결합부(133a)와의 위치 오차에 따른 유격이 있더라도 정확한 위치에 서로 결합될 수 있다. 예를 들어 제1 결합부(221)는 반구형상으로 형성될 수 있다.The first coupling part 221 may be formed to protrude upward from the first support part 210 , and may be coupled to the above-described second coupling part 133a. Since the first coupling part 221 is formed to protrude upwardly, it is possible to minimize the phenomenon of water pooling. Also, the first coupling part 221 may be formed of a magnetic material having a different polarity from that of the second coupling part 133a, and may be attached to the second coupling part 133a through magnetism. Through this, the first coupling part 221 may be coupled to each other at an accurate position even if there is a gap due to a position error with the second coupling part 133a. For example, the first coupling part 221 may be formed in a hemispherical shape.
한편 제1 결합부(221)는 자성체로 구성되지 않고, 자성체에 접촉하는 금속으로 형성될 수 있다. 이에 따라 제1 결합부(221)는 자성체로 형성되는 제2 결합부(133a)에 접촉할 수 있다. 이를 통해 위치 오차를 극복함과 동시에 제2 결합부(133a)에 자성에 의해 이물질이 부착되는 것을 방지할 수 있다.Meanwhile, the first coupling part 221 may not be formed of a magnetic material, but may be formed of a metal in contact with the magnetic material. Accordingly, the first coupling part 221 may contact the second coupling part 133a formed of a magnetic material. Through this, it is possible to overcome the position error and prevent foreign substances from being attached to the second coupling part 133a by magnetism.
제1 단자부(222)는 제1 결합부(221)의 중심부에 배치되어 상술한 제2 단자부(133b)를 통해 도킹부(130)에 전원을 공급할 수 있다. 여기서 제1 단자부(222)는 볼록하게 형성되는 제1 결합부(221)의 최상부 가운데에 위치하여 누전을 예방할 수 있다.The first terminal part 222 may be disposed at the center of the first coupling part 221 to supply power to the docking part 130 through the above-described second terminal part 133b. Here, the first terminal portion 222 may be positioned at the center of the uppermost portion of the convexly formed first coupling portion 221 to prevent short circuit.
댐퍼(233)는 제1 결합부(221)의 가장자리에 형성되며, 도킹부(130)와 도킹 과정에서 충격을 흡수하고, 제1 단자부(212)로의 이물질 유입을 방지할 수 있다. 여기서 댐퍼(233)는 고무, 실리콘 등의 탄성이 있는 재질로 형성되어, 도킹 시 탄성 변형되어, 제2 결합부(133a)와 제1 결합부(221) 사이의 결속력을 높여줄 수 있다.The damper 233 is formed on the edge of the first coupling part 221 , absorbs an impact during the docking process with the docking part 130 , and may prevent the inflow of foreign substances into the first terminal part 212 . Here, the damper 233 is formed of an elastic material such as rubber or silicone, and is elastically deformed during docking, thereby increasing the bonding force between the second coupling part 133a and the first coupling part 221 .
이하 도킹부(130)와 충전 스테이션(200)의 도킹 과정을 설명하도록 한다.Hereinafter, a process of docking the docking unit 130 and the charging station 200 will be described.
먼저 도 4에 도시된 바와 같이, 제어부(140)는 GPS 또는 IMU를 통해 충전 스테이션(200)과의 수직 위치를 잡은 후에, 연결부(134)를 통해 제2 지지부(131)를 충전 스테이션(200) 방향으로 하강시킬 수 있다. 이때 제어부(140)는 센싱부(110)를 통해 충전 스테이션(200)과 일정 거리에 근접한 것이 인식된 경우, 하강 동작을 멈출 수 있다.First, as shown in FIG. 4 , the control unit 140 establishes a vertical position with the charging station 200 through GPS or IMU, and then connects the second support unit 131 through the connection unit 134 to the charging station 200 . direction can be lowered. In this case, when it is recognized through the sensing unit 110 that it approaches the charging station 200 by a predetermined distance, the controller 140 may stop the lowering operation.
다음으로 제어부(140)는 도 5에 도시된 바와 같이, 제2 지지부(131)가 충전 스테이션(200)에 일정 거리 만큼 근접한 경우 하강 동작을 멈춘 상태에서 분사부를 통해 공기를 제1 결합부(221)상에 분사하여, 제1 결합부(221) 및 제1 단자부(222) 상에 있는 이물질을 제거할 수 있다.Next, as shown in FIG. 5 , when the second support part 131 is close to the charging station 200 by a certain distance, the control unit 140 stops the descending operation and blows air through the injection unit to the first coupling unit 221 . ), it is possible to remove foreign substances on the first coupling part 221 and the first terminal part 222 .
다음으로 제어부(140)는 도 6에 도시된 바와 같이, 연결부(134)를 통해 제2 지지부(131)를 충전 스테이션(200) 방향으로 하강시킬 수 있다.Next, as shown in FIG. 6 , the control unit 140 may lower the second support unit 131 in the direction of the charging station 200 through the connection unit 134 .
그리고 제어부(140)는 도 7에 도시된 바와 같이, 도킹부(130)와 충전 스테이션(200)이 완전히 밀착 되면, 충전 스테이션(200)으로부터 전원을 공급받을 수 있다.And, as shown in FIG. 7 , the controller 140 may receive power from the charging station 200 when the docking unit 130 and the charging station 200 are in close contact with each other.
이와 같이 본 발명의 실시예에 따른 무인 이동체의 충전 시스템(300)은 충전 스테이션(200)의 하부 단자부(220)를 볼록하게 형성하고, 도킹부(130)의 상부 단자부(133a)를 오목하게 형성함으로써, 위치 오차를 극복하고, 이물질이 쌓이는 것을 방지하여 누전 발생을 최소화할 수 있다.As described above, in the charging system 300 of the unmanned moving object according to the embodiment of the present invention, the lower terminal part 220 of the charging station 200 is convex, and the upper terminal part 133a of the docking part 130 is concave. By doing so, it is possible to overcome the position error and prevent the accumulation of foreign substances to minimize the occurrence of electric leakage.
또한 본 발명의 실시예에 따른 무인 이동체의 충전 시스템(300)은 도킹전 충전 스테이션(200)의 하부 단자부(220)로 공기를 분사함으로써, 하부 단자부(220)의 이물질을 제거하여 누전 발생을 최소화할 수 있다.In addition, the charging system 300 of the unmanned moving object according to the embodiment of the present invention injects air into the lower terminal part 220 of the charging station 200 before docking, thereby removing foreign substances from the lower terminal part 220 to minimize the occurrence of electric leakage. can do.
또한 본 발명의 실시예에 따른 무인 이동체의 충전 시스템(300)은 하부 단자부(220)에 댐퍼(223)를 구비하여 외부 이물질 유입을 방지할 수 있으며, 도킹부(130)와 충전 스테이션(200)간의 충격을 줄이고, 결속력을 높일 수 있다.In addition, the charging system 300 of the unmanned moving object according to the embodiment of the present invention includes a damper 223 on the lower terminal part 220 to prevent the inflow of foreign substances, and the docking part 130 and the charging station 200 . It can reduce the impact between the liver and increase the bonding force.
이상 본 발명을 몇 가지 바람직한 실시예를 사용하여 설명하였으나, 이들 실시예는 예시적인 것이며 한정적인 것이 아니다. 이와 같이, 본 발명이 속하는 기술분야에서 통상의 지식을 지닌 자라면 본 발명의 사상과 첨부된 특허청구범위에 제시된 권리범위에서 벗어나지 않으면서 균등론에 따라 다양한 변화와 수정을 가할 수 있음을 이해할 것이다. Although the present invention has been described above using several preferred embodiments, these examples are illustrative and not restrictive. As such, those of ordinary skill in the art to which the present invention pertains will understand that various changes and modifications can be made in accordance with the doctrine of equivalents without departing from the spirit of the present invention and the scope of rights set forth in the appended claims.
[부호의 설명][Explanation of code]
100 : 무인 이동체 110 : 센싱부100: unmanned moving object 110: sensing unit
120 : 배터리 130 : 도킹부120: battery 130: docking unit
131 : 제2 지지부 132 : 탄성부131: second support part 132: elastic part
133 : 수신 단자부 133a : 제2 결합부133: receiving terminal portion 133a: second coupling portion
133b : 제2 단자부 134 : 연결부133b: second terminal part 134: connection part
140 : 제어부 200 : 충전 스테이션140: control unit 200: charging station
210 : 제1 지지부 220 : 공급 단자부210: first support 220: supply terminal unit
221 : 제1 결합부 222 : 제1 단자부221: first coupling part 222: first terminal part
223 : 댐퍼 300 : 충전 시스템223: damper 300: charging system

Claims (4)

  1. 일정 간격 이격되어 형성되는 제1 지지부, 상기 제1 지지부의 상부에 배치되며 상부로 볼록하게 돌출되는 하부 단자부를 포함하여, 이동체에 전원을 공급하는 충전 스테이션;a charging station for supplying power to a moving object, including a first support part spaced apart from each other and a lower terminal part disposed on the first support part and convexly protruding upward;
    상기 이동체에 구비되어 상기 충전 스테이션으로부터 전원을 공급받으며, 상기 이동체의 하부에 구비되는 제2 지지부, 상기 제2 지지부와 상기 이동체 사이에 배치되어 상기 제2 지지부에 탄성력을 제공하는 탄성부, 상기 제2 지지부의 하부에 배치되어 상기 하부 단자부와 대응되도록 오목하게 형성되며 상기 하부 단자부와 접촉하는 상부 단자부를 포함하는 도킹부;A second support part provided in the movable body to receive power from the charging station, a second support part provided under the movable body, an elastic part disposed between the second support part and the movable body to provide an elastic force to the second support part; 2 a docking part disposed under the support part and formed concavely to correspond to the lower terminal part and including an upper terminal part in contact with the lower terminal part;
    를 포함하는 것을 특징으로 하는 무인 이동체의 충전 시스템.Charging system of an unmanned mobile body, characterized in that it comprises a.
  2. 제1항에 있어서,According to claim 1,
    상기 하부 단자부는,The lower terminal part,
    상기 제1 지지부로부터 상부로 볼록하게 돌출되어 형성되는 제1 결합부;a first coupling part convexly protruding upward from the first support part;
    상기 제1 결합부의 중심부에 배치되어 전원을 공급하는 제1 단자부;a first terminal unit disposed in the center of the first coupling unit to supply power;
    상기 제1 결합부의 가장자리에 형성되며, 상기 도킹부와 도킹 과정에서 충격을 흡수하고, 상기 제1 단자부로의 이물질 유입을 방지하는 댐퍼;a damper formed on an edge of the first coupling part, absorbing an impact during a docking process with the docking part, and preventing foreign substances from flowing into the first terminal part;
    를 포함하는 것을 특징으로 하는 무인 이동체의 충전 시스템.Charging system of an unmanned mobile body, characterized in that it comprises a.
  3. 제2항에 있어서,3. The method of claim 2,
    상기 상부 단자부는,The upper terminal part,
    상기 제2 지지부의 하부에 구비되며, 상기 제1 결합부와 대응되도록 오목하게 형성되어 상기 제1 결합부와 결합되는 제2 결합부;a second coupling part provided under the second support part and concavely formed to correspond to the first coupling part and coupled to the first coupling part;
    상기 제2 결합부의 중심부에 배치되어 상기 제1 단자부와 접촉하여 전원을 공급받는 제2 단자부;a second terminal part disposed in the center of the second coupling part and receiving power in contact with the first terminal part;
    상기 제2 결합부에 구비되어, 상기 하부 단자부와 결합되기 이전에 상기 제1 결합부로 공기(air)를 분사하여 이물질을 제거하는 분사부;a spraying part provided in the second coupling part to spray air into the first coupling part before being coupled to the lower terminal part to remove foreign substances;
    를 포함하는 것을 특징으로 하는 무인 이동체의 충전 시스템.Charging system of an unmanned mobile body, characterized in that it comprises a.
  4. 제3항에 있어서,4. The method of claim 3,
    상기 제1 단자부 및 상기 제2 단자부 중 적어도 하나는 자성체인 것을 특징으로 하는 무인 이동체의 충전 시스템.At least one of the first terminal part and the second terminal part is a magnetic material.
PCT/KR2021/016338 2020-11-19 2021-11-10 Charging system for unmanned vehicle WO2022108223A1 (en)

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