WO2018086132A1 - 检测装置及无人机 - Google Patents

检测装置及无人机 Download PDF

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Publication number
WO2018086132A1
WO2018086132A1 PCT/CN2016/105780 CN2016105780W WO2018086132A1 WO 2018086132 A1 WO2018086132 A1 WO 2018086132A1 CN 2016105780 W CN2016105780 W CN 2016105780W WO 2018086132 A1 WO2018086132 A1 WO 2018086132A1
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WO
WIPO (PCT)
Prior art keywords
slider
battery
detecting device
circuit
switch
Prior art date
Application number
PCT/CN2016/105780
Other languages
English (en)
French (fr)
Inventor
孙亮
郭晓凯
彭涛
李洪山
欧迪
Original Assignee
深圳市大疆创新科技有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 深圳市大疆创新科技有限公司 filed Critical 深圳市大疆创新科技有限公司
Priority to PCT/CN2016/105780 priority Critical patent/WO2018086132A1/zh
Priority to CN202010201911.6A priority patent/CN111319777B/zh
Priority to CN201680002431.9A priority patent/CN106687374B/zh
Publication of WO2018086132A1 publication Critical patent/WO2018086132A1/zh

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Classifications

    • 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
    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
    • B64U20/83—Electronic components structurally integrated with aircraft elements, e.g. circuit boards carrying loads
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/0085—Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M2220/00—Batteries for particular applications
    • H01M2220/20—Batteries in motive systems, e.g. vehicle, ship, plane
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10—Energy storage using batteries

Definitions

  • the invention relates to a drone technology, in particular to a detecting device and a drone.
  • the drone is a rapidly developing flying device that has the advantages of flexibility, quick response, unmanned flight, and low operational requirements.
  • the scope of use of drones has been expanded to three major areas of military, scientific research and civil use, specifically in power, communications, meteorology, agriculture, oceanography, exploration, photography, disaster prevention and mitigation, crop yield estimation, anti-drug, private border patrols.
  • Various tasks are carried out in the fields of public security and anti-terrorism.
  • batteries have become more and more popular as key components of power supply in drones. After installing the battery, the user does not know whether the battery installation is in place. Once the battery is not installed, the drone cannot perform the flight task, which will cause the user to misjudge that the drone has failed, and the user experience is not good.
  • Embodiments of the present invention aim to solve at least one of the technical problems existing in the prior art. To this end, embodiments of the present invention need to provide a detecting device and a drone.
  • a detecting device of an embodiment of the present invention includes a battery, a battery mount, a circuit, and a slider.
  • the battery is provided with at least one rail.
  • the battery mount has at least one guiding slot corresponding to the at least one guide rail and a sliding slot communicating with the at least one guiding slot.
  • the circuit is disposed on the battery mount and the circuit includes a switch.
  • the slider is mounted on the battery mount and is slidable into the guide slot along the chute.
  • the slider moves along the chute to disconnect the switch.
  • the slider moves along the chute to close the switch, and the battery powers the circuit to cause the circuit to send an indication signal.
  • the switch includes: the switch includes a fixed terminal and a moving terminal, one end of the moving terminal is elastically connected to the fixed terminal, and the other end is separated from the fixed terminal, the moving terminal It is used to contact the fixed terminal when the external force is pressed to close the switch.
  • the slider interferes with an end of the at least one rail when the battery is snapped into place.
  • the at least one channel is perpendicular to the chute.
  • the battery mount defines a mounting slot
  • the mounting slot includes a bottom wall and a first side wall extending from the bottom wall and abutting the end of the battery, the at least one guiding groove and the sliding groove being formed on a bottom wall of the mounting groove.
  • the first sidewall is provided with a connection electrode electrically connected to the circuit, and the end of the battery is provided with a contact electrode, the contact being contacted when the battery is in place
  • An electrode is electrically coupled to the connection electrode and the switch is closed to cause the circuit to form a closed loop.
  • the mounting slot further includes a second sidewall and a third sidewall extending from the bottom wall, the first sidewall being coupled to the second sidewall and the third sidewall Between the walls, a guide rail is disposed on the second side wall and/or the third side wall.
  • the battery further includes a bottom surface provided with the at least one rail, a first side of the battery corresponding to the end of the battery, and a second side and a third side extending from the bottom surface, the first The side surface is connected between the second side surface and the third side surface, and the second side surface and/or the third side surface are formed with a guiding groove corresponding to the guiding rail.
  • the bottom wall includes opposite first sides and second sides, the at least one guiding groove is disposed on the first side, and the sliding member includes a first slider and a second sliding a block, and a connecting member connecting the first slider and the second slider, the first slider is located on the first side, and the second slider and the circuit are disposed at the second On the side, the connecting member penetrates the bottom wall.
  • the first slider is coupled to the bottom of the chute by an elastic member; or/and the second slider is coupled to the second side of the bottom wall by an elastic member.
  • the width of the first slider in a direction perpendicular to the extending direction of the guide groove is smaller than the depth of the sliding groove.
  • the first slider, the second slider, and the connector are integrally formed as the slider.
  • the elastic member includes any one of a metal spring, a rubber spring, and the like.
  • the first slider has a wedge-shaped structure, including a bottom surface of the slider, a side surface of the slider, and a slope connecting the bottom surface of the slider and the side surface of the slider, and one end of the elastic member is fixed at The bottom of the sliding slot is connected to the bottom surface of the slider, and the side of the slider is closer to the first sidewall than the inclined surface.
  • the moving terminal is disposed outside a moving path of the second slider, and the second slider includes a body portion and a protrusion for pressing the moving terminal to The switch is closed.
  • the moving terminal is disposed on a movement path of the second slider, and the second slider is for pressing the moving terminal to close the switch.
  • the detecting device further includes a guide plate fixedly coupled to the second side of the bottom wall, the guide plate and the bottom wall forming a guiding cavity, the second slider It is housed in the guiding cavity.
  • the detecting device further includes a button coupled to the second slider, the button being exposed from the battery mount, the button being capable of moving the second slider.
  • the circuit includes a display unit that is configured to display the indication signal.
  • the circuit includes a communication unit for transmitting the indication signal to the terminal.
  • An unmanned aerial vehicle includes the detecting device according to any one of the above embodiments.
  • the number of detecting devices is two
  • the drone includes a fuselage
  • two detecting devices are respectively disposed on opposite sides of the fuselage.
  • each detecting device includes a button exposed outside the body, a first button and a second button disposed in the first button, the first button and the first The two buttons are used for time-sharing/simultaneous compression control of the slides of the two detecting devices to move/move simultaneously.
  • the detecting device of the unmanned aerial vehicle is provided with a circuit capable of transmitting a battery in-position indication signal on a battery mount, and the battery and the switch are disposed in the circuit to supply power to the circuit through the battery and control the switch and the circuit through the slider. Turning on and then transmitting the battery in-place indication signal allows the user to determine if the battery is in place. When the battery is not in place and the drone is unable to perform the mission, the user will re-install the battery first, and will not assume that the drone has failed first, which improves the user experience.
  • FIG. 1 is a schematic perspective view of a drone of a certain embodiment of the present invention.
  • Figure 2 is an enlarged schematic view of the portion I in Figure 1.
  • FIG. 3 is a schematic perspective view of the battery of FIG. 1.
  • FIG. 4 is a perspective view showing another perspective of the battery of FIG. 1.
  • Figure 5 is a structural schematic view showing a state of the second side of the bottom wall of the mounting groove of the unmanned aerial vehicle of Figure 1.
  • Fig. 6 is a structural schematic view showing another state of the second side of the bottom wall of the mounting groove of the unmanned aerial vehicle of Fig. 1.
  • Figure 7 is a perspective view showing the structure of the slider of the drone of Figure 1.
  • Figure 8 is a perspective view showing another perspective of the slider of the drone of Figure 1.
  • FIG. 9 is a schematic structural view of a circuit of the unmanned aerial vehicle of FIG. 1.
  • Figure 10 is a schematic illustration of the combination button and detection device of the drone of Figure 1.
  • a battery 10 a bottom surface 12, a guide rail 120, a first side surface 14, a second side surface 16, a first guiding groove 160, a third side surface 18, and a second guiding groove 180;
  • Elastic member 40 guide plate 50, guiding cavity 52, button 60;
  • the circuit 70, the switch 72, the fixed terminal 720, the moving terminal 722, the display unit 74, and the communication unit 76 are connected to the circuit 70, the switch 72, the fixed terminal 720, the moving terminal 722, the display unit 74, and the communication unit 76.
  • the first feature "on” or “under” the second feature may be a direct contact of the first and second features, or the first and second features may be indirectly through an intermediate medium, unless otherwise explicitly stated and defined. contact.
  • the first feature "above”, “above” and “above” the second feature may be that the first feature is directly above or above the second feature, or merely that the first feature level is higher than the second feature.
  • the first feature “below”, “below” and “below” the second feature may be that the first feature is directly below or obliquely below the second feature, or merely that the first feature level is less than the second feature.
  • the drone 200 provided by the embodiment of the present invention includes a body 102 and two detecting devices 100 .
  • the two detecting devices 100 are respectively disposed on opposite sides of the body 102 .
  • each detecting device 100 includes a battery 10 , a battery mount 20 , a slider 30 , a guide plate 50 , a button 60 , and a circuit 70 .
  • the battery 10 has a rectangular parallelepiped structure including a bottom surface 12 , a first side surface 14 , a second side surface 16 , and a third side surface 18 .
  • the first side 14 is located at the end of the battery 10 that snaps into the body 102 along the battery 10, with the first side 14 away from the initial end of the snap.
  • the second side 16 and the third side 18 are located at opposite ends of the battery 10 and are connected to the first side 14 .
  • the second side 16 corresponds to the top of the body 102
  • the third side 18 corresponds to the bottom of the body 102 .
  • the bottom surface 12 is connected to both the first side surface 14, the second side surface 16, and the third side surface 18.
  • the bottom surface 12 is provided with two guide rails 120, and the guide rails 120 have a rectangular strip shape.
  • the first side 14 is provided with a contact electrode (not shown).
  • the second side surface 16 is formed with a first guiding groove 160, and the third side surface 18 is formed with a second guiding groove 180.
  • the battery 10 may be of other shapes, such as a cylindrical structure having a circular, elliptical, triangular, pentagonal, hexagonal, etc. cross section.
  • the number of the guide rails 120 is not limited to two in the embodiment, and may be any number of one, three, four, or the like.
  • the shape of the guide rail 120 is not limited to the rectangular strip shape in the present embodiment, and may be a structure of another shape, for example, a cylindrical structure having a circular cross section, an elliptical shape, a triangular shape, a pentagon shape, a hexagonal shape, or the like.
  • the battery mount 20 defines a mounting slot 20a for mounting the battery 10.
  • the mounting groove 20a includes a bottom wall 22, a first side wall 24 extending from the bottom wall 22 and engaging the first side surface 14 of the end of the battery 10, and a second side connected to the bottom wall 22 and the first side wall 24 Wall 26 and third side wall 28.
  • the second side wall 26 is adjacent the top of the fuselage 102 and the third side wall 28 is adjacent the bottom of the fuselage 102.
  • the bottom wall 22, the first side wall 24, the second side wall 26 and the third side wall 28 are respectively opposite to the bottom surface 12, the first side surface 14, the second side surface 16, and the first side Three sides 18 fit together.
  • the bottom wall 22 includes a first side 220 and a second side 222 .
  • Two guide slots 224 corresponding to the two guide rails 120 and a sliding slot 226 communicating with one of the guide slots 224 are defined in the bottom wall 22 of the first side 220.
  • the guide slots 224 and the sliding slots 226 are perpendicular to each other.
  • the first side wall 24 is provided with a connection electrode 240 electrically connected to the circuit 70 and corresponding to a contact electrode (not shown) of the battery 10.
  • the second side wall 26 is provided with a first guiding rail (not shown) corresponding to the first guiding groove 160 of the second side surface 16, and the third side wall 28 is formed with a second corresponding to the guiding groove of the third surface 126.
  • Guide rail 280 The shape and size of the first guiding rail are matched with the shape and size of the first guiding groove 160; the shape and size of the second guiding rail 280 are matched with the shape and size of the second guiding groove 180.
  • the sliding member 30 includes a first slider 32, a second slider 34 and a connecting member 36.
  • the slider 30 is elastically coupled to the bottom 226a of the chute 226 by the elastic member 40 to be fixed to the bottom wall 22.
  • the first slider 32 has a wedge-shaped structure, and includes a slider bottom surface 320, a slider side surface 322, and a slider slope 324 connecting the slider bottom surface 320 and the slider side surface 322.
  • the slider side 322 is opposite to the first side wall 24, and the slider side 322 is larger than the slider
  • the ramp 324 is closer to the first side wall 24. Referring to FIGS. 2, 5 and 6, when the battery 10 is snapped into the mounting groove 20a and snapped into place, the slider side 322 of the first slider 32 is in contact with the end of the guide rail 120. That is, the length of the guide rail 120 is less than or equal to the distance between the end of the guide groove 224 near the first side wall 24 and the side surface 322 of the slider.
  • One end of the elastic member 40 is fixed to the bottom portion 226a of the sliding slot 226, and the other end is connected to the bottom surface 320 of the slider.
  • the first sliding block 32 is received in the sliding slot 226, and the first sliding block 32 can slide into the guiding slot along the sliding slot 226. 224.
  • the elastic member 40 applies a force to the first slider 32 to press the first slider 32 into the guide groove 224.
  • the elastic member 40 is a compression spring, and may be, but not limited to, a metal spring or a rubber spring. In other embodiments, the elastic member 40 can also be other elastically preferred components.
  • the second slider 34 includes a body 340 and a protrusion 342 disposed on the body 340 and extending outwardly of the body 340.
  • the connecting member 36 is disposed through the bottom wall 22 and connects the first slider 32 and the second slider 34.
  • the first slider 32, the second slider 34 and the connecting member 36 are integrally formed as the sliding member 30.
  • the first slider 32, the second slider 34, and the connecting member 36 may be a split forming structure, and the three are combined by one or more of threading, snapping, welding, gluing, and the like. Assembled into a slider 30
  • the guide plate 50 is fixedly coupled to the second side 222 of the bottom wall 22 by screws.
  • the guide plate 50 and the bottom wall 22 form a guiding cavity 52, and the body 340 of the second slider 34 is received in the guiding cavity 52.
  • the button 60 is disposed on the top of the battery mount 20, and one end of the button 60 passes through the second side wall 26 of the battery mount 20 and is coupled to the second slider 34.
  • the other end of the button 60 is The battery mount 20 is exposed outside the body 102 of the drone 200.
  • the button 60 is pressed, the second slider 34 and the first slider 32 can be moved, and the first slider 32 is completely slid into the slot 226 away from the guiding slot 224, so that the slider side 322 does not interfere with the rail 120.
  • the end facilitates removal of the battery 10 from the mounting slot 20a.
  • the elastic member 40 pushes the button 60 through the slider 30 to return the button 60 to its original position.
  • buttons 60 in the two detecting devices 100 are respectively defined as a first button 104 and a second button 106, and the second button 106 is disposed in the first button 104 and operates independently of each other, first
  • the button 104 and the second button 105 can be pressed in time to control the movement of the sliders 30 of the two detecting devices 100 in a time-sharing manner.
  • the first button 104 and the second button 106 can also be simultaneously pressed to simultaneously control the movement of the sliders 30 of the two detecting devices 100, respectively.
  • the circuit 70 includes a switch 72 and a display unit 74.
  • the switch 72 includes a fixed terminal 720 and a moving terminal 722.
  • One end of the moving terminal 722 is elastically coupled to the fixed terminal 720, and the other end of the moving terminal 722 is separated from the fixed terminal 720 as a free end.
  • the moving terminal 722 is pressed by an external force, the free end of the moving terminal 722 is in contact with the fixed terminal 720, and the switch 72 is closed. At this time, the switch 72 is in an on state.
  • the elastic connecting end of the moving terminal 722 has an elastic restoring force for separating the other end of the moving terminal 722.
  • the moving terminal 722 is disposed outside the moving path of the second slider 34 , that is, the moving terminal 722 is disposed outside the extending direction of the guiding cavity 52 .
  • the first slider 32 moves toward the guiding groove 224, the first slider 32 drives the protruding portion 342 of the second slider 34 to slide, and the protruding portion 342 presses the moving terminal 722 of the switch 72 to move and makes the moving terminal
  • the free end of 722 is in contact with fixed terminal 720 to cause switch 72 to close.
  • the display unit 74 includes any one of an indicator light, a display screen, and the like.
  • the battery 10 supplies power to the circuit 70, the circuit 70 transmits an indication signal, and the display unit 74 is configured to display an indication signal.
  • the display unit 74 is an indicator light
  • the indication signal sent by the circuit 70 is an on indicator light
  • the display unit 74 is a display screen
  • the indication signal sent by the circuit 70 is to turn on the display screen, or the display indicates that the battery 10 is stuck in place.
  • the related information may be any one or more combinations of text, graphics or sound.
  • the side wall of the guide rail 120 abuts the first slider 32 to move the first slider 32 along the sliding slot 226 toward the bottom 226a of the sliding slot 226, the first slide
  • the block 32 drives the protruding portion 342 of the second slider 34 to move away from the switch 72, so that the moving terminal 722 is separated from the fixed terminal 720 under the elastic restoring force to open the switch 72.
  • the contact electrode disposed on the first side 14 of the battery 10 is in contact with and electrically connected to the connection electrode 240 disposed on the first side wall 24.
  • the first slider 32 moves along the sliding slot 226 in the direction away from the bottom 226a of the sliding slot 226 under the action of the elastic member 40, and the first slider 32 drives the protruding portion 342 of the second slider 34 to move toward the switch 72.
  • the protrusion 342 will interfere with and press the moving terminal 722 to bring the moving terminal 722 into contact with the fixed terminal 720 to close the switch 72.
  • circuit 70 forms a closed loop, and battery 10 is electrically coupled in circuit 70 to power circuit 70 to cause circuit 70 to issue an indication signal, and display unit 74 displays the indication signal to indicate to the user that battery 10 is stuck in place.
  • the detecting device 100 of the drone 200 of the embodiment of the present invention is provided with a circuit 70 capable of transmitting a battery 10 in-position indication signal on the battery mount 20, and the battery 10 and the switch 72 are disposed in the circuit 70 to pass the battery 10 to the circuit 70. Powering and controlling the conduction of the switch 72 and the circuit 70 through the slider 30 to transmit the indication signal of the battery 10 in place allows the user to determine whether the battery 10 is in place. When the battery 10 is not in place and the drone 200 is unable to perform the flight task, the user will give priority to the problem that the battery is not in place, and the misjudgment that is not preemptive is that the drone 200 has failed, improving the user experience.
  • the drone 200 of the embodiment of the present invention also has the following advantageous effects.
  • the cooperation of the first guiding groove 160 and the first guiding rail 260 facilitates the battery 10 being stuck on the battery mount 20 and preventing the battery 10 from falling off the battery mount 20, so that the structure of the detecting device 100 is more stable.
  • the guiding groove 224 and the sliding groove 226 are designed to be perpendicular to each other, so that the guide rail 120 can facilitate the pushing of the first sliding block 32 into the sliding groove 226.
  • the first slider 32 has a wedge structure. In the will When the battery 10 is mounted to the battery mount 20, the guide rail 120 is urged to push the first slider 32 to move.
  • the slider side 322 can abut against the end of the rail 120 to prevent the rail 120 from slipping out of the channel 224.
  • the guiding cavity 52 cooperates with the second slider 34 so that the second slider 34 is restrained in the guiding cavity 52 and can move in the extending direction of the guiding cavity 52.
  • the guide rail 120 on the bottom surface 12 of the battery 10 can be T-shaped.
  • the guide groove 224 on the bottom wall 22 is also T-shaped to match the T-shaped guide rail 120. In this way, the battery 10 can be effectively prevented from coming off the battery mount 20.
  • the battery 10 may be formed with the first guiding groove 160 only on the second side 16 or may form the second guiding groove 180 only on the third side 18 .
  • the manner in which the slider 30 is fixed to the bottom wall 22 by the elastic member 40 is not limited to the above manner, and one end of the elastic member 40 may be fixed to the second side 222 of the bottom wall 22, and One end is fixed to the second slider 34.
  • the elastic member 40 applies a force to the second slider 34 to pull the first slider 32 connected to the second slider 34 into the guide groove 224.
  • the moving terminal 722 of the switch 72 can also be disposed on the moving path of the second slider 34, and the second slider 34 is used to press the moving terminal 722 to bring the moving terminal 722 into contact with the fixed terminal 720.
  • the switch is closed.
  • the protrusion 342 may not be provided in the second slider 34.
  • the circuit 70 includes a communication unit 188 that generates and transmits an indication signal to a terminal in communication with the drone 200 when the circuit 70 forms a closed loop and the battery 10 supplies power to the circuit 70.
  • the terminal can be an electronic device such as a remote controller, a mobile phone, a computer, a PAD, a bottom station, a smart bracelet, a smart watch, a smart helmet, and the like. In this way, the user can determine whether the battery 10 is installed in place by the indication signal remotely received by the terminal, thereby further improving the user experience.
  • first and second are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated.
  • features defining “first” or “second” may include at least one of the features, either explicitly or implicitly.
  • a plurality means at least two, for example two, three, unless specifically defined otherwise.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

一种检测装置（100）及无人机（200），检测装置（100）包括电池（10）、电池安装座（20）、电路（70）及滑动件（30）。电池（10）设置有至少一个导轨（120）。电池安装座（20）开设与至少一个导轨（120）对应的至少一个导槽（224）及与至少一个导槽（224）连通的滑槽（226）。电路（70）设置在电池安装座（20）上，电路（70）包括开关（72）。滑动件（30）安装在电池安装座（20）上并能够沿着滑槽（226）滑入导槽（224）。当电池（10）的导轨（120）开始卡入对应的导槽（224）时，滑动件（30）沿着滑槽（226）移动以使开关（72）断开。当电池（10）卡入到位时，滑动件（30）沿着滑槽（226）移动使开关（72）闭合，且电池（10）给电路（70）供电以使电路（70）发送指示信号。

Description

检测装置及无人机 技术领域
本发明涉及无人机技术，具体涉及一种检测装置及无人机。
背景技术
无人机是一种处在迅速发展中的飞行装置，其具有机动灵活、反应快速、无人飞行、操作要求低的优点。目前，无人机的使用范围已经扩宽到军事、科研、民用三大领域，具体可在电力、通信、气象、农业、海洋、勘探、摄影、防灾减灾、农作物估产、缉毒缉私、边境巡逻、治安反恐等领域执行各项任务。随着无人机的应用越来越广泛，电池作为无人机中提供动力的关键元件也越来越受到人们的关注。现有的无人机在安装电池后用户并不清楚电池安装是否到位，一旦电池没有装到位，无人机就无法执行飞行任务，会让用户误判为无人机发生了故障，用户体验不佳。
发明内容
本发明的实施方式旨在至少解决现有技术中存在的技术问题之一。为此，本发明的实施方式需要提供一种检测装置及无人机。
本发明实施方式的一种检测装置，所述检测装置包括电池、电池安装座、电路及滑动件。所述电池设置有至少一个导轨。所述电池安装座开设与所述至少一个导轨对应的至少一个导槽及与所述至少一个导槽连通的滑槽。所述电路设置在所述电池安装座上，所述电路包括开关。所述滑动件安装在所述电池安装座上并能够沿着所述滑槽滑入所述导槽。
当所述电池的所述至少一个导轨开始卡入对应的所述导槽时，所述滑动件沿着所述滑槽移动以使所述开关断开。
当所述电池卡入到位时，所述滑动件沿着所述滑槽移动使开关闭合，且所述电池给所述电路供电以使所述电路发送指示信号。
在某些实施方式中，所述开关包括，所述开关包括固定端子及与移动端子，所述移动端子的一端与所述固定端子弹性连接，另一端与所述固定端子分离，所述移动端子用于在外力压迫时与所述固定端子接触以使开关闭合。
在某些实施方式中，当所述电池卡入到位时，所述滑动件与所述至少一个导轨的末端抵触。
在某些实施方式中，所述至少一个导槽与所述滑槽垂直。
在某些实施方式中，所述电池安装座开设一个安装槽，所述安装槽包括底壁及自所述 底壁延伸且与所述电池的端部贴合的第一侧壁，所述至少一个导槽及所述滑槽形成在所述安装槽的底壁上。
在某些实施方式中，所述第一侧壁上设置与所述电路电连接的连接电极，所述电池的所述端部设置有接触电极，当所述电池卡入到位时，所述接触电极与所述连接电极电连接且所述开关闭合使所述电路形成闭合回路。
在某些实施方式中，所述安装槽还包括自所述底壁延伸的第二侧壁及第三侧壁，所述第一侧壁连接在所述第二侧壁与所述第三侧壁之间，所述第二侧壁和/或所述第三侧壁上设置有导向轨。所述电池还包括设置有所述至少一个导轨的底面、与所述电池的所述端部对应的电池第一侧面、及自所述底面延伸的第二侧面及第三侧面，所述第一侧面连接在所述第二侧面与所述第三侧面之间，所述第二侧面和/或所述第三侧面形成有与所述导向轨对应的导向槽。
在某些实施方式中，所述底壁包括相背的第一侧及第二侧，所述至少一个导槽设置在所述第一侧，所述滑动件包括第一滑块、第二滑块、及连接所述第一滑块与所述第二滑块的连接件，所述第一滑块位于所述第一侧，所述第二滑块及所述电路设置在所述第二侧，所述连接件穿设所述底壁。所述第一滑块通过弹性件连接在所述滑槽的底部；或/和所述第二滑块通过弹性件连接在所述底壁的所述第二侧。
在某些实施方式中，所述第一滑块沿垂直于所述导槽延伸方向的宽度小于所述滑槽的深度。
在某些实施方式中，所述第一滑块、所述第二滑块、及所述连接件一体成型为所述滑动件。
在某些实施方式中，所述弹性件包括金属弹簧、橡胶弹簧等中的任意一种。
在某些实施方式中，所述第一滑块呈楔形结构，包括滑块底面、滑块侧面、及连接所述滑块底面与所述滑块侧面的斜面，所述弹性件的一端固定在所述滑槽的底部，另一端与所述滑块底面连接，所述滑块侧面较所述斜面更接近所述第一侧壁。
在某些实施方式中，所述移动端子设置在所述第二滑块的移动路线外，所述第二滑块包括本体部及突出部，所述突出部用于压迫所述移动端子以使所述开关闭合。
在某些实施方式中，所述移动端子设置在所述第二滑块的移动路线上，所述第二滑块用于压迫所述移动端子以使所述开关闭合。
在某些实施方式中，所述检测装置还包括固定连接在所述底壁的所述第二侧的导向板，所述导向板与所述底壁形成一导向腔，所述第二滑块收容在所述导向腔内。
在某些实施方式中，所述检测装置还包括与所述第二滑块连接的按钮，所述按钮从所述电池安装座暴露，所述按钮能够带动所述第二滑块移动。
在某些实施方式中，所述电路包括显示单元，所述单元显示用于显示所述指示信号。
在某些实施方式中，所述电路包括通信单元，所述通信单元用于发送所述指示信号给终端。
本发明实施方式提供的一种无人机，所述无人机包括上述任意一项实施方式所述的检测装置。
在某些实施方式中，所述检测装置的数量为两个，所述无人机包括机身，两个检测装置分别设置在所述机身的相背两侧。
在某些实施方式中，每个检测装置包括暴露在所述机身外的按钮，分别为第一按钮及设置在所述第一按钮内的第二按钮，所述第一按钮及所述第二按钮用于分时受压/同时受压控制所述两个检测装置的滑动件分别移动/同时移动。
本发明实施方式的无人机的检测装置在电池安装座上设置能够发送电池到位指示信号的电路，并将电池及开关设置在电路中以通过电池给电路供电及通过滑动件控制开关及电路的导通进而将电池到位的指示信号发送出去使用户能够判断电池是否安装到位。在电池没有装到位，无人机无法执行飞行任务时，用户就会先会重新安装电池，而不会先入为主的认为无人机发生了故障，提升了用户体验。
本发明的实施方式的附加方面和优点将在下面的描述中部分给出，部分将从下面的描述中变得明显，或通过本发明的实施方式的实践了解到。
附图说明
本发明的上述和/或附加的方面和优点从结合下面附图对实施方式的描述中将变得明显和容易理解，其中：
图1是本发明某些实施方式的无人机的立体结构示意图。
图2是图1中I处放大示意图。
图3是图1中电池的立体结构示意图。
图4是图1中电池的另一视角的立体结构示意图。
图5是图1中无人机的安装槽底壁的第二侧的一种状态的结构示意图。
图6是图1中无人机的安装槽底壁的第二侧的另一种状态的结构示意图。
图7是图1中无人机的滑动件的立体结构示意图。
图8是图1中无人机的滑动件的另一视角的立体结构示意图。
图9是图1中无人机的电路的结构示意图。
图10是图1中无人机的组合按钮与检测装置的示意图。
主要元件符号附图说明：
无人机200、检测装置100、机身102、第一按钮104、第二按钮106；
电池10、底面12、导轨120、第一侧面14、第二侧面16、第一导向槽160、第三侧面18、第二导向槽180；
电池安装座20、安装槽20a、底壁22、第一侧220、第二侧222、导槽224、滑槽226、底部226a、第一侧壁24、连接电极240、第二侧壁26、第三侧壁28、第二导向轨280；
滑动件30、第一滑块32、滑块底面320、滑块侧面322、滑块斜面324、第二滑块34、本体340、突出部342、连接件36；
弹性件40、导向板50、导向腔52、按钮60；
电路70、开关72、固定端子720、移动端子722、显示单元74、通信单元76。
具体实施方式
以下结合附图对本发明的实施方式作进一步说明。附图中相同或类似的标号自始至终表示相同或类似的元件或具有相同或类似功能的元件。
另外，下面结合附图描述的本发明的实施方式是示例性的，仅用于解释本发明的实施方式，而不能理解为对本发明的限制。
在本发明中，除非另有明确的规定和限定，第一特征在第二特征“上”或“下”可以是第一和第二特征直接接触，或第一和第二特征通过中间媒介间接接触。而且，第一特征在第二特征“之上”、“上方”和“上面”可是第一特征在第二特征正上方或斜上方，或仅仅表示第一特征水平高度高于第二特征。第一特征在第二特征“之下”、“下方”和“下面”可以是第一特征在第二特征正下方或斜下方，或仅仅表示第一特征水平高度小于第二特征。
在本说明书的描述中，参考术语“某些实施方式”、“一个实施方式”、“一些实施方式”、“示例”、“具体示例”、或“一些示例”等的描述意指结合该实施例或示例描述的具体特征、结构、材料或者特点包含于本发明的至少一个实施例或示例中。在本说明书中，对上述术语的示意性表述不必须针对的是相同的实施例或示例。而且，描述的具体特征、结构、材料或者特点可以在任一个或多个实施例或示例中以合适的方式结合。此外，在不相互矛盾的情况下，本领域的技术人员可以将本说明书中描述的不同实施例或示例以及不同实施例或示例的特征进行结合和组合。
尽管上面已经示出和描述了本发明的实施例，可以理解的是，上述实施例是示例性的，不能理解为对本发明的限制，本领域的普通技术人员在本发明的范围内可以对上述实施例进行变化、修改、替换和变型。
请参阅图1，本发明实施方式提供的无人机200包括机身102及两个检测装置100，两个检测装置100分别设置在机身102的相背两侧。
请参阅图1、图2、图5及图9，每个检测装置100包括电池10、电池安装座20、滑动件30、导向板50、按钮60、电路70。
请参阅图3及图4，电池10呈长方体结构，包括底面12、第一侧面14、第二侧面16及第三侧面18。第一侧面14位于电池10的沿着电池10卡入机身102的端部，第一侧面14远离卡入的起始端。第二侧面16及第三侧面18位于电池10相背的两端，且均与第一侧面14连接，第二侧面16与机身102的顶部对应，第三侧面18与机身102的底部对应。底面12与第一侧面14、第二侧面16、及第三侧面18均连接。
底面12设置有两个导轨120，导轨120呈矩形条状。第一侧面14设置有接触电极(图未示)。第二侧面16形成有第一导向槽160、第三侧面18形成有第二导向槽180。在其他实施方式中，电池10可以是其他形状的结构，例如：截面为圆形、椭圆形、三角形、五边形、六边形等的柱体结构。导轨120的数量并不局限于本实施方式中的两个，还可是一个、三个、四个等任意数量。导轨120的形状也不局限于本实施方式中的矩形条状，还可以是其他形状的结构，例如：截面为圆形、椭圆形、三角形、五边形、六边形等的柱体结构。
请参阅图1及图2，电池安装座20开设一个用于安装电池10的安装槽20a。安装槽20a包括底壁22、自底壁22延伸且与电池10端部的第一侧面14贴合的第一侧壁24、及与底壁22及第一侧壁24均连接的第二侧壁26及第三侧壁28。第二侧壁26靠近机身102的顶部，第三侧壁28靠近机身102的底部。其中，当电池10卡人安装槽20a内时，底壁22、第一侧壁24、第二侧壁26及第三侧壁28分别与底面12、第一侧面14、第二侧面16及第三侧面18贴合。
请参阅图2及图5，底壁22包括第一侧220及第二侧222。在第一侧220的底壁22上开设有与两个导轨120对应的两个导槽224及与其中一个导槽224连通的滑槽226，导槽224与滑槽226相互垂直。
第一侧壁24上设置有与电路70电连接且与电池10的接触电极(图未示)对应的连接电极240。
第二侧壁26上设置有与第二侧面16的第一导向槽160对应的第一导向轨(图未示)，第三侧壁28形成有与第三面126的导向槽对应的第二导向轨280。第一导向轨的形状及尺寸与第一导向槽160的形状与尺寸匹配；第二导向轨280的形状及尺寸与第二导向槽180的形状及尺寸相匹配。
请一并参阅图2、图6及图7，滑动件30包括第一滑块32、第二滑块34及连接件36。滑动件30通过弹性件40弹性连接在滑槽226的底部226a从而固定在底壁22上。
第一滑块32呈楔形结构，包括滑块底面320、滑块侧面322、及连接滑块底面320与滑块侧面322的滑块斜面324。滑块侧面322与第一侧壁24相对，且滑块侧面322较滑块 斜面324更接近第一侧壁24。请结合图2、图5及图6，当电池10卡入安装槽20a并卡到位时，第一滑块32的滑块侧面322与导轨120的末端抵触。也就是说，导轨120的长度小于或等于导槽224靠近第一侧壁24的一端到滑块侧面322之间的距离。弹性件40的一端固定在滑槽226的底部226a，另一端与滑块底面320连接，第一滑块32收容在滑槽226内，第一滑块32能够沿着滑槽226滑入导槽224。
在初始状态下，弹性件40会给第一滑块32施加一个力以使第一滑块32被压进导槽224内。本实施方式中，弹性件40为压缩弹簧，可以是但不限于为金属弹簧、橡胶弹簧。在其他实施方式中，弹性件40还可以是其他弹性较佳的元件。
第二滑块34包括本体340及设置在本体340上并朝本体340外延伸的突出部342。
连接件36穿设底壁22并连接第一滑块32与第二滑块34，第一滑块32、第二滑块34及连接件36一体成型为滑动件30。在其他实施方式中，第一滑块32、第二滑块34及连接件36可以为分体成型结构，三者通过螺纹、卡合、焊接、胶合等的一种或多种相组合的方式组装成滑动件30
导向板50通过螺钉固定连接在底壁22的第二侧222。导向板50与底壁22形成一导向腔52，第二滑块34的本体340收容在导向腔52内。
请参阅图5及图6，按钮60设置在电池安装座20的顶部，按钮60的一端穿过电池安装座20的第二侧壁26后与第二滑块34连接，按钮60的另一端从电池安装座20暴露在无人机200的机身102外。按钮60被按压时能够带动第二滑块34及第一滑块32移动，并使第一滑块32离开导槽224完全滑入滑槽226内，进而使滑块侧面322不抵触导轨120的末端以便于将电池10可以从安装槽20a上取出。当释放按钮60时，弹性件40通过滑动件30推动按钮60使按钮60回复到原来的位置。
请参阅图2及图10，两个检测装置100中的两个按钮60分别定义为第一按钮104与第二按钮106，第二按钮106设置在第一按钮104内且互相独立工作，第一按钮104及第二按钮105能够分时按压，以便分时控制两个检测装置100的滑动件30分别移动。第一按钮104及第二按钮106也能够同时按压，以便同时控制两个检测装置100的滑动件30分别移动。
请一并参阅图5-6及图9，电路70包括开关72及显示单元74。开关72包括固定端子720及移动端子722。移动端子722的一端与固定端子720弹性连接，移动端子722的另一端与固定端子720分离成为自由端。当移动端子722受到外力压迫时，移动端子722的自由端与固定端子720接触，开关72闭合，此时，开关72处于导通状态。移动端子722的弹性连接端具有使移动端子722的另一端分离的弹性回复力，当移动端子722没有受到外力压迫时，移动端子722的自由端与固定端子720分离回复到自由状态，开关72断开，也 就是说，在自然状态下，移动端子722的自由端与固定端子720分离，开关72处于断开的不导通状态。
请参阅图5及图6，移动端子722设置在第二滑块34的移动路线外，也就是说，移动端子722设置在导向腔52的延伸方向外。当第一滑块32朝靠近导槽224的方向移动时，第一滑块32带动第二滑块34的突出部342滑动，突出部342会压迫开关72的移动端子722移动，并使移动端子722的自由端与固定端子720接触进而使开关72闭合。
显示单元74包括指示灯、显示屏等中的任意一种，当电池10卡入到位时，电池10给电路70供电，电路70发送指示信号，显示单元74用于显示指示信号。例如：当显示单元74为指示灯，电路70发送的指示信号为开启指示灯；当显示单元74为显示屏，电路70发送的指示信号为开启显示屏、或是显示表明电池10卡入到位的相关信息，此相关信息可以是文字、图形或者声音中的任意一种或多种组合。
当电池10的导轨120开始卡入对应的导槽224时，导轨120的侧壁抵触第一滑块32使第一滑块32沿着滑槽226朝滑槽226的底部226a移动，第一滑块32带动第二滑块34的突出部342朝远离开关72方向移动，使移动端子722在弹性回复力下与固定端子720分离进而使开关72断开。
当电池10卡入到位时，设置在电池10的第一侧面14的接触电极与设置在第一侧壁24的连接电极240接触并导通。第一滑块32在弹性件40的作用下沿着滑槽226朝远离滑槽226的底部226a方向移动，且第一滑块32带动第二滑块34的突出部342朝靠近开关72方向移动，突出部342会抵触并压迫移动端子722使移动端子722与固定端子720接触而使开关72闭合。此时，电路70形成闭合回路，且电池10电连接在电路70中为电路70供电以使电路70发出指示信号，显示单元74显示所述指示信号以向用户表示电池10卡入到位。
本发明实施方式的无人机200的检测装置100在电池安装座20上设置能够发送电池10到位指示信号的电路70，并将电池10及开关72设置在电路70中以通过电池10给电路70供电及通过滑动件30控制开关72及电路70的导通进而将电池10到位的指示信号发送出去使用户能够判断电池10是否安装到位。在电池10没有装到位，无人机200无法执行飞行任务时，用户就会优先考虑电池没有装到位的问题，而不会先入为主的误判为无人机200发生了故障，提升了用户体验。
本发明实施方式的无人机200还具有以下有益效果。第一、第一导向槽160与第一导向轨260的配合便于电池10卡设在电池安装座20上并防止电池10从电池安装座20上脱落，使检测装置100的结构更加稳定。第二、导槽224与滑槽226设计成相互垂直的结构，可以方便导轨120将第一滑块32推入滑槽226内。第三、第一滑块32呈楔形结构。在将 电池10安装到电池安装座20上时，以便于导轨120推动第一滑块32移动。再者，在电池10安装完成时，滑块侧面322能够抵住导轨120的末端以防止导轨120滑出导槽224。第四、导向腔52与第二滑块34配合，以便于第二滑块34被限制在导向腔52内并能沿导向腔52的延伸方向移动。
在某些实施方式中，电池10底面12上的导轨120可呈T形，对应地，底壁22上导槽224也为与T形导轨120相匹配的T形。如此，可以有效地防止电池10从电池安装座20上脱落。
请参阅图3及图4，在某些实施方式中，电池10可只在第二侧面16形成有第一导向槽160，或可只在第三侧面18形成第二导向槽180。
在某些实施方式中，滑动件30通过弹性件40固定在底壁22上的方式并不局限于上述方式，还可以是：弹性件40的一端固定在底壁22的第二侧222，另一端固定在第二滑块34上。在初始状态下，弹性件40会给第二滑块34施加一个力以使与第二滑块34连接的第一滑块32被拉进导槽224内。
在某些实施方式中，开关72的移动端子722还可设置在第二滑块34的移动路线上，第二滑块34用于压迫移动端子722以使移动端子722与固定端子720接触进而使开关闭合。此时，第二滑块34的就可不设置突出部342。
在某些实施方式中，电路70包括通信单元188，当电路70形成闭合回路且电池10给电路70供电时，通信单元188会产生并发送指示信号给与无人机200通信的终端。终端可以是遥控器、手机、电脑、PAD、底面站、智能手环、智能手表、智能头盔等电子装置。如此，用户可以通过终端远程接收到的指示信号来判断电池10是否安装到位，进一步提升了用户体验。
在本说明书的描述中，参考术语“某些实施方式”、“一个实施方式”、“一些实施方式”、“示意性实施方式”、“示例”、“具体示例”、或“一些示例”的描述意指结合所述实施方式或示例描述的具体特征、结构、材料或者特点包含于本实用新型的至少一个实施方式或示例中。在本说明书中，对上述术语的示意性表述不一定指的是相同的实施方式或示例。而且，描述的具体特征、结构、材料或者特点可以在任何的一个或多个实施方式或示例中以合适的方式结合。
此外，术语“第一”、“第二”仅用于描述目的，而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量。由此，限定有“第一”、“第二”的特征可以明示或者隐含地包括至少一个所述特征。在本实用新型的描述中，“多个”的含义是至少两个，例如两个，三个，除非另有明确具体的限定。
尽管上面已经示出和描述了本实用新型的实施例，可以理解的是，上述实施例是示例 性的，不能理解为对本实用新型的限制，本领域的普通技术人员在本实用新型的范围内可以对上述实施例进行变化、修改、替换和变型，本实用新型的范围由权利要求及其等同物限定。

Claims (21)

  1. 一种检测装置，其特征在于，所述检测装置包括：
    电池，设置有至少一个导轨；
    电池安装座，开设与所述至少一个导轨对应的至少一个导槽及与所述至少一个导槽连通的滑槽；
    设置在所述电池安装座上的电路，所述电路包括开关；及
    滑动件，安装在所述电池安装座上并能够沿着所述滑槽滑入所述导槽；
    当所述电池的所述至少一个导轨开始卡入对应的所述导槽时，所述滑动件沿着所述滑槽移动以使所述开关断开；
    当所述电池卡入到位时，所述滑动件沿着所述滑槽移动使开关闭合，且所述电池给所述电路供电以使所述电路发送指示信号。
  2. 如权利要求1所述的检测装置，其特征在于，所述开关包括，所述开关包括固定端子及与移动端子，所述移动端子的一端与所述固定端子弹性连接，另一端与所述固定端子分离，所述移动端子用于在外力压迫时与所述固定端子接触以使开关闭合。
  3. 如权利要求1所述的检测装置，其特征在于，当所述电池卡入到位时，所述滑动件与所述至少一个导轨的末端抵触。
  4. 如权利要求1所述的检测装置，其特征在于，所述至少一个导槽与所述滑槽垂直。
  5. 如权利要求2所述的检测装置，其特征在于，所述电池安装座开设一个安装槽，所述安装槽包括底壁及自所述底壁延伸且与所述电池的端部贴合的第一侧壁，所述至少一个导槽及所述滑槽形成在所述安装槽的底壁上。
  6. 如权利要求5所述的检测装置，其特征在于，所述第一侧壁上设置与所述电路电连接的连接电极，所述电池的所述端部设置有接触电极，当所述电池卡入到位时，所述接触电极与所述连接电极电连接且所述开关闭合使所述电路形成闭合回路。
  7. 如权利要求5所述的检测装置，其特征在于，所述安装槽还包括自所述底壁延伸的第二侧壁及第三侧壁，所述第一侧壁连接在所述第二侧壁与所述第三侧壁之间，所述第二侧壁和/或所述第三侧壁上设置有导向轨；
    所述电池还包括设置有所述至少一个导轨的底面、与所述电池的所述端部对应的电池第一侧面、及自所述底面延伸的第二侧面及第三侧面，所述第一侧面连接在所述第二侧面与所述第三侧面之间，所述第二侧面和/或所述第三侧面形成有与所述导向轨对应的导向槽。
  8. 如权利要求5所述的检测装置，其特征在于，所述底壁包括相背的第一侧及第二侧，所述至少一个导槽设置在所述第一侧，所述滑动件包括第一滑块、第二滑块、及连接所述第一滑块与所述第二滑块的连接件，所述第一滑块位于所述第一侧，所述第二滑块及所述电路设置在所述第二侧，所述连接件穿设所述底壁；
    所述第一滑块通过弹性件连接在所述滑槽的底部；或/和
    所述第二滑块通过弹性件连接在所述底壁的所述第二侧。
  9. 如权利要求8所述的检测装置，其特征在于，所述第一滑块沿垂直于所述导槽延伸方向的宽度小于所述滑槽的深度。
  10. 如权利要求8所述的检测装置，其特征在于，所述第一滑块、所述第二滑块、及所述连接件一体成型为所述滑动件。
  11. 如权利要求8所述的检测装置，其特征在于，所述弹性件包括金属弹簧、橡胶弹簧等中的任意一种。
  12. 如权利要求8所述的检测装置，其特征在于，所述第一滑块呈楔形结构，包括滑块底面、滑块侧面、及连接所述滑块底面与所述滑块侧面的斜面，所述弹性件的一端固定在所述滑槽的底部，另一端与所述滑块底面连接，所述滑块侧面较所述斜面更接近所述第一侧壁。
  13. 如权利要求8所述的检测装置，其特征在于，所述移动端子设置在所述第二滑块的移动路线外，所述第二滑块包括本体部及突出部，所述突出部用于压迫所述移动端子以使所述开关闭合。
  14. 如权利要求8所述的检测装置，其特征在于，所述移动端子设置在所述第二滑块的移动路线上，所述第二滑块用于压迫所述移动端子以使所述开关闭合。
  15. 如权利要求8所述的检测装置，其特征在于，所述检测装置还包括固定连接在所述底壁的所述第二侧的导向板，所述导向板与所述底壁形成一导向腔，所述第二滑块收容在所述导向腔内。
  16. 如权利要求8所述的检测装置，其特征在于，所述检测装置还包括与所述第二滑块连接的按钮，所述按钮从所述电池安装座暴露，所述按钮能够带动所述第二滑块移动。
  17. 如权利要求8所述的检测装置，其特征在于，所述电路包括显示单元，所述单元显示用于显示所述指示信号。
  18. 如权利要求8所述的检测装置，其特征在于，所述电路包括通信单元，所述通信单元用于发送所述指示信号给终端。
  19. 一种无人机，其特征在于，所述无人机包括如权利要求1-18任意一项所述的检测装置。
  20. 如权利要求19所述的无人机，其特征在于，所述检测装置的数量为两个，所述无人机包括机身，两个检测装置分别设置在所述机身的相背两侧。
  21. 如权利要求20所述的无人机，其特征在于，每个检测装置包括暴露在所述机身外的按钮，分别为第一按钮及设置在所述第一按钮内的第二按钮，所述第一按钮及所述第二按钮用于分时受压/同时受压控制所述两个检测装置的滑动件分别移动/同时移动。
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112644732A (zh) * 2021-01-05 2021-04-13 徐艳 一种车载多旋翼无人机起降平台
FR3116663A1 (fr) * 2020-11-26 2022-05-27 Intent Interface électromécanique pour gérer automatiquement une batterie d'un drone

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106995061B (zh) * 2017-05-20 2023-07-21 国网湖北省电力有限公司襄阳供电公司 一种无人机的电池保护装置
CN207303190U (zh) * 2017-09-30 2018-05-01 深圳市大疆创新科技有限公司 电池模块以及无人机
CN116674386A (zh) * 2018-01-19 2023-09-01 深圳市大疆创新科技有限公司 一种电池安全提示系统
WO2020000180A1 (zh) * 2018-06-26 2020-01-02 深圳市大疆创新科技有限公司 一种电池组件、自主移动平台和自主移动平台系统
CN112740470B (zh) * 2019-12-18 2024-05-14 深圳市大疆创新科技有限公司 开关结构、电池组件和电子设备
CN113064084A (zh) * 2021-03-19 2021-07-02 深圳市道通智能航空技术股份有限公司 一种监测电池的方法、电池及无人机
CN114171855B (zh) * 2022-01-05 2024-01-12 惠州市忠邦电子有限公司 组合式电池包及智能沙发

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH077278A (ja) * 1993-06-14 1995-01-10 Casio Comput Co Ltd 電池蓋のロック構造
CN2664299Y (zh) * 2003-09-12 2004-12-15 明基电通股份有限公司 移动电话及其电池卡合结构
CN1829106A (zh) * 2005-03-04 2006-09-06 三星电子株式会社 用于便携式终端的电池包安装设备
CN2816887Y (zh) * 2005-08-23 2006-09-13 英业达股份有限公司 电子装置的电池定位及释放共享模块结构
CN203690968U (zh) * 2013-12-06 2014-07-02 深圳市大疆创新科技有限公司 电池、具有该电池的飞行器

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60254556A (ja) * 1984-05-30 1985-12-16 Canon Inc 電池蓋装着検知機構
JP2001176475A (ja) * 1999-12-17 2001-06-29 Hitachi Kokusai Electric Inc 携帯電話機のバッテリ保持構造
CN101893917A (zh) * 2009-05-19 2010-11-24 仁宝电脑工业股份有限公司 电子装置的电池匣的固定结构及其固定方法
CN201532979U (zh) * 2009-11-03 2010-07-21 四川长虹电器股份有限公司 蓄电池组的安装架
KR101271567B1 (ko) * 2010-08-16 2013-06-11 주식회사 엘지화학 고정부재가 플레이트들의 관통구에 삽입되어 있는 구조의 전지모듈 및 이를 포함하는 전지팩
CN102832060B (zh) * 2011-06-15 2014-12-31 上海电科电器科技有限公司 转换开关的联锁装置
KR101373038B1 (ko) * 2012-12-27 2014-03-11 김영진 수상인명구조를 위한 에어백과 에어백 낙하장치를 갖춘 공중부양 비행로봇
EP2871694B1 (en) * 2013-10-01 2018-02-07 LG Chem, Ltd. Battery cell and battery module using same
FR3015774A1 (fr) * 2013-12-24 2015-06-26 Commissariat Energie Atomique Systeme de fixation amovible d'une batterie a un support
CN205564859U (zh) * 2016-05-10 2016-09-07 傲飞创新科技（深圳）有限公司 无人机电池盒装载结构

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH077278A (ja) * 1993-06-14 1995-01-10 Casio Comput Co Ltd 電池蓋のロック構造
CN2664299Y (zh) * 2003-09-12 2004-12-15 明基电通股份有限公司 移动电话及其电池卡合结构
CN1829106A (zh) * 2005-03-04 2006-09-06 三星电子株式会社 用于便携式终端的电池包安装设备
CN2816887Y (zh) * 2005-08-23 2006-09-13 英业达股份有限公司 电子装置的电池定位及释放共享模块结构
CN203690968U (zh) * 2013-12-06 2014-07-02 深圳市大疆创新科技有限公司 电池、具有该电池的飞行器

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3116663A1 (fr) * 2020-11-26 2022-05-27 Intent Interface électromécanique pour gérer automatiquement une batterie d'un drone
WO2022111996A1 (fr) * 2020-11-26 2022-06-02 Intent Interface electromecanique pour systeme automatique de gestion de batteries d'un drone
CN112644732A (zh) * 2021-01-05 2021-04-13 徐艳 一种车载多旋翼无人机起降平台

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CN106687374B (zh) 2020-04-24

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