WO2024016807A1 - 无人机机架、机库和车辆 - Google Patents

无人机机架、机库和车辆 Download PDF

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Publication number
WO2024016807A1
WO2024016807A1 PCT/CN2023/094505 CN2023094505W WO2024016807A1 WO 2024016807 A1 WO2024016807 A1 WO 2024016807A1 CN 2023094505 W CN2023094505 W CN 2023094505W WO 2024016807 A1 WO2024016807 A1 WO 2024016807A1
Authority
WO
WIPO (PCT)
Prior art keywords
drone
uav
power supply
contact
mounting
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
PCT/CN2023/094505
Other languages
English (en)
French (fr)
Inventor
李东平
陈继承
郄星
赵晨宇
王轶纲
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BYD Co Ltd
Original Assignee
BYD Co Ltd
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 BYD Co Ltd filed Critical BYD Co Ltd
Priority to CA3261802A priority Critical patent/CA3261802A1/en
Priority to EP23841876.8A priority patent/EP4559816A4/en
Publication of WO2024016807A1 publication Critical patent/WO2024016807A1/zh
Priority to US19/018,193 priority patent/US20250145313A1/en
Priority to MX2025000633A priority patent/MX2025000633A/es
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/007—Helicopter portable landing pads
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/30—Constructional details of charging stations
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
    • B60L53/14—Conductive energy transfer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/80—Exchanging energy storage elements, e.g. removable batteries
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
    • B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
    • B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
    • B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/40—Modular UAVs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/70—Constructional aspects of the UAV body
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/30—Supply or distribution of electrical power
    • B64U50/37—Charging when not in flight
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U60/00—Undercarriages
    • B64U60/30—Undercarriages detachable from the body
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/80—Vertical take-off or landing, e.g. using rockets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/90—Launching from or landing on platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/90—Launching from or landing on platforms
    • B64U70/92—Portable platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U80/00—Transport or storage specially adapted for UAVs
    • B64U80/20—Transport or storage specially adapted for UAVs with arrangements for servicing the UAV
    • B64U80/25—Transport or storage specially adapted for UAVs with arrangements for servicing the UAV for recharging batteries; for refuelling
    • E—FIXED CONSTRUCTIONS
    • E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
    • E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
    • E01F3/00—Landing stages for helicopters, e.g. located above buildings
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
    • E04H6/00—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages
    • E04H6/42—Devices or arrangements peculiar to garages, not covered elsewhere, e.g. securing devices, safety devices, monitoring and operating schemes; centering devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00—Type of vehicles
    • B60L2200/10—Air crafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2260/00—Operating Modes
    • B60L2260/40—Control modes
    • B60L2260/50—Control modes by future state prediction
    • B60L2260/52—Control modes by future state prediction drive range estimation, e.g. of estimation of available travel distance
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2260/00—Operating Modes
    • B60L2260/40—Control modes
    • B60L2260/50—Control modes by future state prediction
    • B60L2260/54—Energy consumption estimation
    • 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
    • B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/90—Launching from or landing on platforms
    • B64U70/92—Portable platforms
    • B64U70/93—Portable platforms for use on a land or nautical vehicle
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/90—Launching from or landing on platforms
    • B64U70/97—Means for guiding the UAV to a specific location on the platform, e.g. platform structures preventing landing off-centre
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U80/00—Transport or storage specially adapted for UAVs
    • B64U80/80—Transport or storage specially adapted for UAVs by vehicles
    • B64U80/86—Land vehicles
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
    • E04H6/00—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages
    • E04H6/44—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages for storing aircraft

Definitions

  • This application relates to the field of drone technology, and in particular to a drone rack, hangar and vehicle.
  • the hangar serves as a take-off and landing platform for the drone and can be placed on vehicles, ships and building walls.
  • This application aims to solve at least one of the technical problems existing in the prior art. To this end, this application proposes a drone rack that can realize automatic charging of the drone on a parking platform.
  • This application also proposes a hangar with the above-mentioned drone rack.
  • This application also proposes a vehicle with the above-mentioned hangar.
  • the UAV is provided with a charging terminal
  • the UAV frame includes: a mounting body, the mounting body is used to install the UAV, the mounting body Suitable for parking on a parking platform; an electrical connection line, the first end of the electrical connection line is provided with a first fitting portion, the first fitting portion is suitable for electrical connection with the charging terminal, and the third end of the electrical connection line
  • the two ends are connected to the second fitting part at the bottom of the mounting body, and the second fitting part is suitable for electrical connection with the power supply end of the parking platform.
  • the UAV frame according to the embodiment of the present application can be installed on the UAV.
  • the UAV frame includes an installation body and an electrical connection cable.
  • the electrical connection cable can The power supply end of the parking platform is connected to the charging end of the drone, so that the drone can be automatically charged on the parking platform, thus helping to reduce the need for charging the drone. Manual operation of electricity improves user experience.
  • the mounting body is provided with a wiring channel, the wiring channel extends to the bottom of the mounting body, and the electrical connection wire is installed to the wiring channel.
  • the second fitting portion includes a contact bump
  • the power supply end is provided with a contact groove
  • the contact bump is adapted to extend into the contact groove so that the second fitting portion electrically connected to the power supply terminal.
  • an installation channel is provided in the second fitting part, and an elastic member is provided in the installation channel.
  • the elastic member cooperates with the contact protrusion to apply force toward the contact protrusion. The force causes the contact bump to have a tendency to protrude out of the mounting channel.
  • the plurality of contact protrusions are arranged in one-to-one correspondence with the plurality of avoidance through holes.
  • Each of the contact protrusions is provided with a plurality of avoidance through holes.
  • the bump can extend out of the corresponding escape through hole to contact the power supply terminal.
  • the mounting body includes: a support part adapted to be supported on the parking platform; a mounting part disposed on the top of the support part, the mounting part and the The support portion cooperates to define a placement space, and both the front and rear portions of the placement space are open to be suitable for installing the drone.
  • the top of the support part is formed as a support surface to cooperate with the drone, and the support surface is provided with a first hollow part.
  • the mounting part is provided with a second hollow part.
  • the top of the mounting part is provided with a mounting assembly for mounting external equipment.
  • the installation component includes: a screw hole, the screw hole is provided on the top of the installation part; an adapter joint, the adapter joint is threadedly matched with the screw hole, and the adapter joint extends out of the
  • the end of the mounting part is provided with a fixing hole; a fastener, the fastener is adapted to cooperate with external equipment and the fixing hole.
  • the hangar according to the second embodiment of the present application includes: a parking platform and the drone rack of the above embodiment, the parking platform is provided with a power supply end; when the installation body is parked on the parking platform, the The second matching part is adapted to be electrically connected to the power supply terminal.
  • the parking platform is suitable for parking drones, and the drone rack can be installed on the drone.
  • the drone rack includes a mounting body and an electrical connection line. When the drone passes through the mounting body When parked on the parking platform, the electrical connection cable can connect the power supply end of the parking platform to the charging end of the drone, so that the drone can be automatically charged on the parking platform, thus helping to reduce the manual labor required to charge the drone. operation to improve user experience.
  • the hangar further includes a charge controller electrically connected to the power supply end, and the charge controller is used to control the electrical output of the power supply end.
  • the hangar further includes a current detection loop, the current detection loop having a There are two contacts arranged at intervals on the electrical end. When the second mating part contacts the two contacts, the current detection circuit is turned on to determine that the UAV frame is parked on the parking platform.
  • the hangar further includes a centering mechanism for adjusting the position of the installation body on the parking platform so that the installation body is between the second mating part and the parking platform.
  • the power supply terminal is electrically connected to a neutral state.
  • a vehicle according to a third embodiment of the present application includes: a body and a hangar of the above embodiment, and the hangar is disposed on the top of the body.
  • a hangar is provided on the top of the vehicle body.
  • the parking platform of the hangar is suitable for parking a drone.
  • the drone rack can be installed on the drone.
  • the drone rack includes an installation body and an electric motor.
  • the electrical connection cable can connect the power supply end of the parking platform to the charging end of the drone, so that the drone can be automatically charged on the parking platform. It is helpful to reduce the manual operation of charging the drone and improve the user experience.
  • Figure 1 is a schematic diagram of a UAV frame, UAV and external equipment according to an embodiment of the present application
  • Figure 2 is a schematic diagram of a drone frame and external equipment according to an embodiment of the present application
  • Figure 3 is an exploded view of Figure 2;
  • Figure 4 is a cross-sectional view of Figure 2;
  • Figure 5 is a schematic diagram of the power supply end and the second mating part according to an embodiment of the present application.
  • Figure 6 is a schematic diagram of a drone frame, a drone and a centering mechanism according to an embodiment of the present application
  • Figure 7 is a schematic diagram of a hangar according to an embodiment of the present application.
  • the UAV 200 is provided with a charging terminal.
  • An external power supply can be connected to the charging terminal to charge the UAV 200.
  • the charging terminal can be located at the tail, bottom or top of the UAV 200. .
  • the UAV frame 9 includes: an installation body 91 and an electrical connection line 92.
  • the installation body 91 is used to install the UAV 200, and the installation body 91 is suitable for parking on the parking platform 80. That is to say, the installation body 91 can be connected to the parking platform 80.
  • the UAV 200 is fixed, and at least part of the installation body 91 is located below the UAV 200.
  • the installation body 91 can increase the height of the UAV 200 and avoid the body and surrounding components of the UAV 200 from appearing when the UAV 200 lands. Interference, the installation body 91 can also increase the contact area between the drone 200 and the parking platform 80, so as to reduce the operational difficulty of the drone 200 landing on the parking platform 80.
  • the first end of the electrical connection wire 92 is provided with a first fitting portion 921.
  • the first fitting portion 921 is suitable for electrical connection with the charging terminal.
  • the first fitting portion 921 can maintain a plug-in fixed electrical connection state with the charging terminal.
  • the electrical connection wire The second end of 92 is connected to the second fitting part 922 at the bottom of the installation body 91.
  • the second fitting part 922 is suitable for electrical connection with the power supply end 801 of the parking platform 80.
  • the second fitting part 922 is The mating part 922 can contact the power supply end 801 of the parking platform 80 to achieve electrical connection. Therefore, the charging current can be output through the power supply end 801 and conducted to the charging end through the electrical connection wire 92, thereby realizing the UAV 200 being placed on the parking platform. 80 automatically charges.
  • the power supply end 801, the charging end and the electrical connection line 92 can transmit current for charging the drone 200, and the power supply end 801, the charging end and the electrical connection line 92 can also transmit data to facilitate the unmanned aerial vehicle.
  • the drone 200 exports the internal data of the drone 200 while charging.
  • the charging terminal is a Type-c female connector
  • the first mating part 921 is a Type-c male connector.
  • the UAV frame 9 can be designed to be matched with different types of UAVs 200, so that the UAV frame 9 closely matches the corresponding UAV 200, and the wiring channels will be
  • the first mating portion of the electrical connection wire 92 921 leads to the charging end of the corresponding UAV 200, and ensures that the first mating portion 921 of the electrical connection line 92 is matched with the charging end interface of the UAV 200, so that the UAV frame 9 can match any model on the market. Charging interface of HMI 200.
  • the UAV frame 9 can be installed on the UAV 200.
  • the UAV frame 9 includes an installation body 91 and an electrical connection cable 92.
  • the UAV 200 is parked on the parking platform through the installation body 91.
  • the electrical connection line 92 can connect the power supply end 801 of the parking platform 80 and the charging end of the drone 200, so that the drone 200 can be automatically charged on the parking platform 80, thereby helping to reduce the impact on the drone. 200 charging manual operation improves user experience.
  • the installation body 91 is provided with a wiring channel, the wiring channel extends to the bottom of the installation body 91 , and the electrical connecting wires 92 are installed in the wiring channel.
  • the channel can be used to fix the electrical connection wire 92 and control the direction of the electrical connection wire 92 to prevent the electrical connection wire 92 from loosening and shaking.
  • the wiring channel can be provided on the inner side of the installation body 91 to reduce the risk of the electrical connection wire 92 leakage, to hide the electrical connection wire 92, thereby reducing the impact of the electrical connection wire 92 on the performance and aesthetics of the drone 200, and improving the service life of the electrical connection wire 92.
  • the second mating part 922 includes contact bumps 9211
  • the power supply end 801 is provided with a contact groove 8011
  • the contact bumps 9211 are adapted to extend into the contact grooves. groove 8011, so that the second mating part 922 and the power supply terminal 801 are electrically connected.
  • the cooperation of the contact bump 9211 and the contact groove 8011 can realize multi-directional and multi-angle charging, and also facilitates the electrical connection between the second mating part 922 and the power supply terminal 801.
  • the establishment and separation of the electrical connection between the second mating part 922 and the power supply terminal 801 are prevented from affecting the take-off and landing operations of the UAV 200 .
  • the second matching part 922 includes a wireless charging receiver, and the power supply end 801 is provided with a wireless charging transmitter.
  • the wireless charging receiver can communicate with the wireless charging receiver.
  • the charging transmitter is facing directly, so that the second matching part 922 and the power supply terminal 801 are electrically connected, thereby realizing charging of the drone 200 .
  • the second fitting portion 922 is provided with an installation channel, and an elastic member is provided in the installation channel.
  • the elastic member cooperates with the contact protrusion 9211 to exert force toward the contact protrusion 9211, and the force makes the contact
  • the bump 9211 has a tendency to extend out of the installation channel.
  • the installation channel can be set along the direction of gravity.
  • the contact bump 9211 can extend out of the installation channel from the lower end of the installation channel under the force of the elastic member.
  • the contact protrusion 9211 can extend out of the installation channel under the force of the elastic member, and extend into the contact groove.
  • the bottom of the groove 8011 stops, which helps to improve the reliability of the electrical connection between the contact bump 9211 and the contact groove 8011 and avoid the problem of virtual connection.
  • the elastic member and the contact bump 9211 are configured as spring pins, so that the contact bump 9211 can extend and retract the installation channel.
  • the power supply terminal 801 is provided with multiple contact bumps 9211.
  • the one-to-one corresponding contact grooves 8011 form a charging circuit after each contact protrusion 9211 extends into the corresponding contact groove 8011, and enhance the carrying capacity of the charging circuit, thereby conducive to increasing the charging speed of the drone 200.
  • the mounting body 91 is provided with a plurality of avoidance through holes, and the plurality of contact protrusions 9211 are arranged in one-to-one correspondence with the plurality of avoidance through holes. Each contact protrusion 9211 can extend out the corresponding avoidance through hole to contact the power supply terminal 801.
  • the contact protrusion 9211 can be pressed into the avoidance through hole. At this time, the avoidance through hole can protect the contact.
  • the bump 9211 reduces the pressure on the contact bump 9211.
  • the contact bump 9211 can stretch out the corresponding avoidance through hole under the force of the elastic member, and It goes deep enough to stop against the bottom of the contact groove 8011, thereby improving the reliability of the electrical connection between the contact bump 9211 and the contact groove 8011 and avoiding the problem of virtual connection.
  • the maximum length of each contact bump 9211 extending out of the avoidance through hole is 2 mm to 3 mm.
  • the mounting body 91 includes: a support portion 911 and a mounting portion 912 .
  • the support portion 911 is adapted to be supported on the parking platform 80 , and at least a portion of the support portion 911 can be Located below the drone 200, the support portion 911 can increase the distance between the body of the drone 200 and the parking platform 80 to avoid interference between the body of the drone 200 and surrounding components when the drone 200 lands.
  • the support portion 911 can also increase the contact area between the drone 200 and the parking platform 80 to reduce the operational difficulty of the drone 200 landing on the parking platform 80.
  • the support portion 911 can also achieve buffering and reduction. The impact of the shock can reduce the impact force that the UAV 200 receives when landing, thereby improving the safety of the UAV 200 and preventing the UAV 200 from falling when the UAV 200 falls to the ground abnormally due to high-frequency electromagnetic interference or other reasons. bad.
  • the installation part 912 is provided on the top of the support part 911.
  • the installation part 912 and the support part 911 cooperate to define a placement space.
  • the front and rear parts of the placement space are open to accommodate the installation of the UAV 200.
  • the middle part of the body of the UAV 200 It can be installed in the placement space, and the mounting part 912 and the supporting part 911 can wrap around the body of the drone 200 to ensure the stability of the drone 200 and the mounting body 91 .
  • the top of the support portion 911 is formed as a support surface to cooperate with the drone 200 , and the support surface is provided with a first hollow portion 9111 , wherein the support surface can face the unmanned aerial vehicle.
  • the bottom of the machine 200 is supported.
  • the first hollow portion 9111 can penetrate the support surface in the direction of gravity so that the support surface forms a hollow structure.
  • the first hollow portion 9111 can reduce the weight of the support portion 911 to achieve a lightweight design of the support portion 911. This is beneficial to reducing the flight load weight of the UAV 200 and improving the battery life of the UAV 200.
  • the first hollow part 9111 can correspond to the cooling air vents at the bottom of the drone 200 to ensure smooth heat dissipation at the bottom cooling air vents of the drone 200.
  • the first hollow part 9111 can also correspond to the device interface at the bottom of the drone 200 to ensure smooth heat dissipation. Avoid the device interface at the bottom of the drone 200.
  • the mounting portion 912 is provided with a second hollow portion 9122 , and the second hollow portion 9122 can penetrate the mounting portion 912 in the thickness direction of the mounting portion 912 , so that the mounting portion 912 forms a Hollow Structures, Vol.
  • the two hollow parts 9122 can reduce the weight of the installation part 912 to achieve a lightweight design of the installation part 912, which is beneficial to reducing the flight load weight of the UAV 200 and improving the endurance of the UAV 200.
  • the second hollow portion 9122 may correspond to the cooling air vents of the drone 200 to ensure smooth heat dissipation through the cooling air vents of the drone 200 .
  • the mounting portion 912 is provided with a plurality of second hollow portions 9122 to further reduce the weight of the mounting portion 912 .
  • the mounting part 912 and the supporting part 911 may be integrally formed to facilitate the production of the mounting part 912 and the supporting part 911 .
  • the mounting part 912 and the supporting part 911 pass through Multiple fasteners 93 or buckles are detachably connected to facilitate fixing the drone 200 between the mounting part 912 and the support part 911, thereby simplifying the connection between the drone frame 9 and the drone. 200% assembly process reduces assembly deviations and ensures production consistency.
  • the installation part 912 can be installed in place from above the drone 200 , and the support surface of the support part 911 is buckled at the front end limit point of the drone 200 so as to Make the support part 911 fit the lower surface of the drone 200, and pre-tighten the fastening installation part 93 so that the installation part 912 and the support part 911 are connected, and a certain pre-tightening gap is reserved at the connection.
  • the outer shell profile of the UAV 200 may be provided with a plurality of bosses suitable for limited cooperation with the mounting part 912 and/or the supporting part 911. Limiting block to ensure that the UAV 200 closely matches the UAV frame 9 in any direction without the risk of slipping out.
  • the fastening mounting parts 93 may be bolts. Nuts suitable for mating with the bolts are pre-embedded in the bottom of the mounting part 912 . The bolts may pass through the support part 911 and then engage with the nuts. Fix so that the mounting part 912 and the supporting part 911 are both fit with the shell profile of the drone 200, ensuring that the drone frame 9 and the drone 200 are closely matched to prevent the drone 200 from sliding out of the placement space.
  • the bolts are countersunk head bolts, and the nuts are GB809-A standard M3*10 embedded round nuts.
  • the mounting part 912 and the support part 911 can be connected by four countersunk head bolts.
  • the mounting part 912 is designed with a contoured structure of the drone 200 casing.
  • the mounting part 912 can be closely attached to the outer surface of the drone 200 , and the mounting part 912 can be in contact with the drone 200 The protruding portion of the housing is engaged so that the mounting portion 912 is stably fixed to the drone 200 .
  • the top of the mounting portion 912 is provided with a mounting assembly 94 for mounting an external device 400 , so that the external device 400 can pass through the connection with the drone frame 9
  • the installation component 94 is fixed to expand the functions of the drone 200 so that the drone 200 can meet the execution conditions of complex tasks such as rescue search and film and television shooting through the external device 400, and meet the personalized needs of users.
  • the external device 400 may be an action camera, a fill light, etc.
  • the mounting assembly 94 includes: screw holes 941 , adapter joints 942 and fasteners 943 .
  • the screw holes 941 are provided on the top of the mounting part 912 .
  • 941 can be formed on embedded nuts,
  • the pre-embedded nut is pre-embedded on the top of the mounting part 912.
  • the adapter joint 942 is threaded with the screw hole 941.
  • the end of the adapter joint 942 extending out of the installation part 912 is provided with a fixing hole.
  • the fastener 943 is suitable for connecting with the external device 400.
  • the user can flexibly replace the external device 400 as needed by disassembling and assembling the external device 400 and the fastener 943, thereby improving the practicality of the drone 200.
  • the external device 400 needs other adapter devices to be fixed on the mounting part 912, the corresponding adapter joint 942 and fastener 943 can be replaced.
  • the screw hole 941 can be connected to a variety of adapter devices on the market.
  • a hangar 1000 according to the second embodiment of the present application includes: a parking platform 80 and the UAV frame 9 in the above embodiment.
  • the parking platform 80 is provided with a power supply end 801, When the installation body 91 is parked on the parking platform 80 , the second matching portion 922 is suitable for electrical connection with the power supply end 801 .
  • the parking platform 80 is suitable for parking the drone 200, and the drone rack 9 can be installed on the drone 200.
  • the drone rack 9 includes an installation body 91 and an electrical connection line 92. , when the drone 200 is parked on the parking platform 80 through the installation body 91, the electrical connection line 92 can connect the power supply terminal 801 of the parking platform 80 and the charging terminal of the drone 200, so that the drone 200 can be placed on the parking platform.
  • the drone 80 is automatically charged, which helps reduce the manual operation of charging the drone 200 and improves the user experience.
  • the hangar 1000 also includes a charge controller electrically connected to the power supply terminal 801.
  • the charge controller is used to control the electrical output of the power supply terminal 801.
  • the charge controller can detect the current amount of the power supply terminal 801 to determine whether Whether to stop the power output, the current size of the power supply terminal 801 can determine whether the drone 200 is fully charged, and the charging controller can cut off the power in time after the drone 200 is fully charged to avoid overcharging of the drone 200.
  • the charging controller can monitor the charging current of the drone 200 and the battery voltage of the drone 200.
  • the drone 200 During the charging process, the current of the power supply terminal 801 is about 4A. After the drone 200 is fully charged, the current drops to less than 0.1A. At this time, the drone 200 is fully charged, and the controller stops the power output for charging the drone 200 to prevent excessive charging. Charging causes damage to the drone 200 battery.
  • the hangar 1000 further includes a current detection circuit.
  • the current detection circuit has two spaced contacts located at the power supply end 801. When the second mating part 922 is in contact with the two contacts, the current detection circuit The loop is turned on to determine that the UAV frame 9 is parked on the parking platform 80 , that is to say, when the two contact bumps 9211 on the second matching part 922 are in contact with the corresponding two contact points, the parking platform 80
  • the power supply end 801 of the UAV 200 is connected to the charging end of the UAV 200, and the current detection loop is in a conductive state with current flowing through it, then it is determined that the UAV frame 9 is parked on the parking platform 80, and the UAV 200 can be charged.
  • the power supply end 801 of the parking platform 80 and the charging end of the drone 200 are not connected, and the current of the current detection circuit is 0, and it is in a non-conducting state, then It can be determined that the second mating portion 922 of the drone frame 9 is not electrically connected to the power supply terminal 801, and the drone 200 is not in a charging state.
  • the two contacts of the current detection circuit can be contacts provided separately on the power supply terminal 801, or the two contact grooves 8011 on the power supply terminal 801 can be used as contacts.
  • the hangar 1000 also includes a centering mechanism 100 .
  • the centering mechanism 100 is used to adjust the position of the installation body 91 on the parking platform 80 so that the installation body 91 is at
  • the second matching part 922 is electrically connected to the power supply end 801 in a centered state, thereby realizing automatic centering and charging of the UAV 200 .
  • the centering mechanism 100 includes: a driving motor 10, a rotating frame, a moving part 30 and a push rod 40.
  • the driving motor 10 is dynamically connected to the rotating frame, and the rotating frame is used to drive the moving part 30 to move.
  • the component 30 drives the push rod 40 to move, and the push rod 40 is used to push the installation body 91 located on the parking platform 80 to move, so that the installation body 91 drives the drone 200 to achieve automatic centering.
  • the second fitting part 922 is directly opposite to the power supply terminal 801, and the contact protrusion 9211 extends into the contact groove 8011.
  • the second fitting part 922 is electrically connected to the power supply terminal 801, and the drone 200 can be charged.
  • the motor shaft of the driving motor 10 is provided with a power gear 11, and the rotating frame includes a plurality of rotating rods 21 arranged in a square frame shape along the circumferential direction. At least one end of each rotating rod 21 is provided with a matching gear 211, wherein The matching gear 211 at the end of one rotating rod 21 meshes with the power gear 11, and the matching gear 211 of each rotating rod 21 in the remaining rotating rods 21 meshes with its adjacent matching gear 211 so that each rotating rod 21 can be transmitted through power.
  • each rotating rod 21 is provided with a moving part 30 that cooperates with it and moves relative to it.
  • the moving parts 30 on the two parallel rotating rods 21 are connected through a push rod 40 .
  • the horizontal and vertical directions are defined in the horizontal plane where the centering mechanism 100 is located, and the push rod 40 may include a first rod in the transverse direction and a second rod in the longitudinal direction.
  • the first rod is used to adjust the drone. 200 in the horizontal direction
  • the second rod is used to adjust the position of the drone 200 in the longitudinal direction to achieve automatic centering of the drone 200.
  • the number of corresponding rotating rods 21 is four, among which the two longitudinally opposite rotating rods 21 correspond to the first rod to drive the first rod to move in the transverse direction, and the other two transversely opposite rotating rods 21 correspond to the second rod.
  • the two longitudinally opposite rotating rods 21 correspond to the first rod to drive the first rod to move in the transverse direction
  • the other two transversely opposite rotating rods 21 correspond to the second rod.
  • To drive the second rod to move in the longitudinal direction and at least two adjacent rotating rods 21 are provided with matching gears 211 at both ends, and other rotating rods 21 are provided with matching gears 211 at only one end or both ends, so that multiple
  • the synchronous rotation of the rotating rod 21 realizes synchronous position adjustment in the horizontal and vertical directions, and realizes the automatic centering of the UAV 200.
  • the push rod 40 may include two first rods that are opposite in the transverse direction and two first rods that are opposite in the longitudinal direction. a second rod, the two first rods can move toward or away from each other transversely, and the two second rods can move toward or away from each other longitudinally, so that when both first rods and both second rods are facing
  • the support part 911 can be pushed, and the support part 911 can drive the drone 200 to correct the lateral position and longitudinal position of the drone 200, so that the drone 200 can move to the middle position, thereby realizing the drone 200. of automatic centering.
  • the rotating rods 21 are also configured with at least four, including two transverse rotating rods that are opposite in the transverse direction and two longitudinal rotating rods that are opposite in the longitudinal direction.
  • the power gear 11 of the driving motor 10 meshes with the matching gear 211 of one of the transverse rotating rods or one of the longitudinal rotating rods to transmit power to the rotating rod 21, and the other end of the rotating rod 21 is also provided with a matching gear.
  • the gear 211, and other rotating rods 21 realize the sequential transmission of power by matching the gear 211, and the rotating rod 21 is provided with a moving part 30 connected with its power.
  • the rotating rod 21 rotates under the drive of the driving motor 10, and synchronously drives the moving part 30 to move.
  • the moving member 30 is used to drive the two first rods to move toward or away from each other, or to drive the two second rods to move toward or away from each other.
  • the number of rotating rods 21 and push rods 40 can also be 6, 8, etc., and the push rods 40 can move toward or away from each other in pairs, so that the automatic centering of the UAV 200 can be realized.
  • the moving parts 30 on the two transverse rotating rods are connected with the second rod and are used to push the second rod to move in the longitudinal direction
  • the moving parts 30 on the two longitudinal rotating rods are connected with the first rod and are used to push the second rod to move longitudinally.
  • the centering mechanism 100 of the embodiment of the present application by arranging the driving motor 10, the rotating frame, the moving part 30 and the push rod 40, the drone 200 can be pushed to move to the middle position, and the automatic centering of the drone 200 can be realized. It reduces the difficulty of centering and improves the fixed stability of the UAV 200. At the same time, multiple push rods 40 can be driven by only one drive motor 10, which can effectively reduce the cost of the centering mechanism 100 and reduce the difficulty of control.
  • the hangar 1000 also includes a power swap mechanism 300 .
  • the power swap mechanism 300 includes a power swap drive assembly 301 and a power swap mechanical claw 302 .
  • the power swap mechanical claw 302 is suitable for clamping
  • the battery replacement drive assembly 301 is suitable for driving the battery replacement mechanical claw 302 to move.
  • the battery replacement drive assembly 301 can drive The battery replacement mechanical claw 302 replaces the battery 201 in a power-deficient state on the drone 200 with a fully charged battery 201 to quickly replenish the power of the drone 200 and increase the cruising range of the drone 200.
  • the battery replacement drive assembly 301 is configured as a gantry screw slide structure.
  • the vehicle according to the third embodiment of the present application includes: a body and the hangar 1000 in the above embodiment.
  • the hangar 1000 is arranged on the top of the body.
  • the hangar 1000 can be used as vehicle-mounted equipment. There are no unmanned vehicles in the hangar 1000.
  • the aircraft 200 can collect road condition information around the vehicle from a higher perspective, which can make up for the vehicle's limitations in the "visual" area, effectively improve the vehicle's field of vision, and better obtain environmental information that is difficult to obtain around the vehicle. , reduce blind spots, improve driving safety, and can also be used to assist the automatic driving of vehicles.
  • the UAV 200 can be electrically connected to the power supply terminal 801 of the parking platform 80 through the electrical connection line 92 on the UAV frame 9, and the vehicle power supply can supply power to the power supply terminal 801 to achieve
  • the automatic charging function eliminates the manual operation process and indirectly increases the drone 200 battery life.
  • UAV 200 is becoming more and more popular in people's daily life for shooting, performing, etc., and it is closely related to vehicles. The combination can also meet the convenience of carrying and transporting the UAV 200.
  • a hangar 1000 is provided on the top of the vehicle body.
  • the parking platform 80 of the hangar 1000 is suitable for parking the drone 200.
  • the drone rack 9 can be installed on the drone 200.
  • the frame 9 includes an installation body 91 and an electrical connection cable 92.
  • the electrical connection cable 92 can connect the power supply terminal 801 of the parking platform 80 to the charging terminal of the drone 200.
  • the UAV 200 can be automatically charged on the parking platform 80, thereby conducive to reducing the manual operation of charging the UAV 200 and improving the user experience.
  • the vehicle owner or the vehicle control system controls the UAV 200 to return to the parking platform 80, or when the UAV 200 is low on power and automatically returns to the parking platform 80, the centering mechanism 100 of the hangar 1000 is used.
  • the drone 200 Cooperating with the drone frame 9, the drone 200 is fixed in the center of the parking platform 80.
  • the second matching part 922 is directly facing the power supply end 801, and the contact protrusion 9211 extends into the contact groove 8011.
  • the matching part 922 is electrically connected to the power supply terminal 801, and the drone 200 can be charged automatically.
  • the charging controller monitors the charging current and the voltage of the battery 201 of the drone 200. After the drone 200 is fully charged, the current drops to 0.1 Within A, the drone 200 is fully charged at this time, and the charge controller stops the power output for charging the drone 200. Prevent damage to the battery 201 caused by overcharging.
  • first and second are used for descriptive purposes only and cannot be understood as indicating or implying relative importance or implicitly indicating the quantity of indicated technical features. Therefore, features defined as “first” and “second” may explicitly or implicitly include one or more of these features.
  • plurality means two or more than two, unless otherwise explicitly and specifically limited.
  • connection In this application, unless otherwise clearly stated and limited, the terms “installation”, “connection”, “connection”, “fixing” and other terms should be understood in a broad sense. For example, it can be a fixed connection or a detachable connection. , or integrated; it can be a mechanical connection, an electrical connection, or a communication; it can be a direct connection, or an indirect connection through an intermediate medium, or an internal connection between two elements or an interaction between two elements .
  • fixing and other terms should be understood in a broad sense. For example, it can be a fixed connection or a detachable connection. , or integrated; it can be a mechanical connection, an electrical connection, or a communication; it can be a direct connection, or an indirect connection through an intermediate medium, or an internal connection between two elements or an interaction between two elements .
  • the specific meanings of the above terms in this application can be understood according to specific circumstances.
  • a first feature being “on” or “below” a second feature may mean that the first and second features are in direct contact, or the first and second features are in indirect contact through an intermediary. touch.
  • the terms “above”, “above” and “above” the first feature is above the second feature may mean that the first feature is directly above or diagonally above the second feature, or simply means that the first feature is higher in level than the second feature.
  • the first feature “below”, “below” and “beneath” the second feature may mean that the first feature is directly below or diagonally below the second feature, or simply means that the first feature has a smaller horizontal height than the second feature. feature.
  • references to the terms “one embodiment,” “some embodiments,” “an example,” “specific examples,” or “some examples” or the like means that specific features are described in connection with the embodiment or example. , structures, materials or features are included in at least one embodiment or example of the present application. In this specification, the schematic expressions of the above terms are not necessarily directed to the same embodiment or example. Furthermore, the specific features, structures, materials or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, those skilled in the art may combine and combine different embodiments or examples and features of different embodiments or examples described in this specification unless they are inconsistent with each other.

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Abstract

一种无人机机架、机库和车辆。无人机机架包括：安装本体和电连接线，安装本体用于安装无人机，安装本体适于停放在停放平台，电连接线的第一端设有第一配合部，第一配合部适于与充电端电连接，电连接线的第二端连接至安装本体底部的第二配合部，第二配合部适于与停放平台的供电端电连接。

Description

无人机机架、机库和车辆
相关申请的交叉引用
本申请基于申请号为：2022108521073，申请日为2022年07月19日的中国专利申请提出，并要求该中国专利申请的优先权，该中国专利申请的全部内容在此引入本申请作为参考。
技术领域
本申请涉及无人机技术领域，尤其是涉及一种无人机机架、机库和车辆。
背景技术
相关技术中指出，无人机在停放状态下，需要停放在机库内，而机库作为无人机的起降平台，可以放置在车辆、船舶以及建筑物墙体上。
然而，由于无人机的续航有限，无人机在执行完飞行任务返回至机库后，需要人工将外接电源接入无人机进行充电，人工充电操作较为繁琐，影响用户体验。
申请内容
本申请旨在至少解决现有技术中存在的技术问题之一。为此，本申请在于提出一种无人机机架，所述无人机机架可以实现无人机在停放平台上自动进行充电。
本申请还提出一种具有上述无人机机架的机库。
本申请还提出一种具有上述机库的车辆。
根据本申请第一方面的无人机机架，无人机设有充电端，所述无人机机架包括：安装本体，所述安装本体用于安装所述无人机，所述安装本体适于停放在停放平台；电连接线，所述电连接线的第一端设有第一配合部，所述第一配合部适于与所述充电端电连接，所述电连接线的第二端连接至所述安装本体底部的第二配合部，所述第二配合部适于与所述停放平台的供电端电连接。
根据本申请实施例的无人机机架，可安装于无人机，无人机机架包括安装本体和电连接线，在无人机通过安装本体停放在停放平台时，电连接线可将停放平台的供电端与无人机的充电端导通，以实现无人机在停放平台上自动进行充电，从而有利于减少对无人机充 电的人工操作，提升用户体验。
在一些实施例中，所述安装本体设有走线通道，所述走线通道延伸至所述安装本体的底部，所述电连接线安装至所述走线通道。
在一些实施例中，所述第二配合部包括接触凸点，所述供电端设有接触凹槽，所述接触凸点适于伸入到所述接触凹槽以使得所述第二配合部和所述供电端电连接。
进一步地，所述第二配合部内设有安装通道，所述安装通道内设有弹性件，所述弹性件与所述接触凸点配合以朝向所述接触凸点施加作用力，所述作用力使得所述接触凸点具有伸出所述安装通道的趋势。
进一步地，所述接触凸点为多个，所述安装本体上设有多个避让通孔，多个所述接触凸点与所述多个避让通孔一一对应设置，每个所述接触凸点可伸出相应的所述避让通孔以与所述供电端接触。
在一些实施例中，所述安装本体包括：支撑部，所述支撑部适于支撑于所述停放平台；安装部，所述安装部设在所述支撑部的顶部，所述安装部和所述支撑部配合限定出放置空间，所述放置空间的前部和后部均敞开以适于安装所述无人机。
进一步地，所述支撑部的顶部形成为与所述无人机配合的支撑面，所述支撑面设有第一镂空部。
进一步地，所述安装部设有第二镂空部。
进一步地，所述安装部的顶部设有用于安装外部设备的安装组件。
进一步地，所述安装组件包括：螺孔，所述螺孔设置于所述安装部的顶部；转接接头，所述转接接头与所述螺孔螺纹配合，所述转接接头伸出所述安装部的端部设有固定孔；紧固件，所述紧固件适于与外部设备和所述固定孔配合。
根据本申请第二方面实施例的机库，包括：停放平台和上述实施例的无人机机架，所述停放平台设有供电端；所述安装本体停放于所述停放平台时，所述第二配合部适于与所述供电端电连接。
根据本申请实施例的机库，停放平台适于停放无人机，无人机机架可安装于无人机，无人机机架包括安装本体和电连接线，在无人机通过安装本体停放在停放平台时，电连接线可将停放平台的供电端与无人机的充电端导通，以实现无人机在停放平台上自动进行充电，从而有利于减少对无人机充电的人工操作，提升用户体验。
在一些实施例中，所述机库还包括与所述供电端电连接的充电控制器，所述充电控制器用于控制所述供电端的电输出。
在一些实施例中，所述机库还包括电流检测回路，所述电流检测回路具有位于所述供 电端的两个间隔设置的触点，所述第二配合部与两个所述触点接触时，所述电流检测回路导通以判定所述无人机机架停放于所述停放平台。
在一些实施例中，所述机库还包括归中机构,所述归中机构用于调整所述安装本体在所述停放平台的位置，以使所述安装本体处于所述第二配合部与所述供电端电连接的归中状态。
根据本申请第三方面实施例的车辆，包括：车身和上述实施例的机库，所述机库设置于所述车身的顶部。
根据本申请实施例的车辆，其车身的顶部设有机库，机库的停放平台适于停放无人机，无人机机架可安装于无人机，无人机机架包括安装本体和电连接线，在无人机通过安装本体停放在停放平台时，电连接线可将停放平台的供电端与无人机的充电端导通，以实现无人机在停放平台上自动进行充电，从而有利于减少对无人机充电的人工操作，提升用户体验。
本申请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，或通过本申请的实践了解到。
附图说明
图1是根据本申请实施例的无人机机架、无人机和外部设备的示意图；
图2是根据本申请实施例的无人机机架和外部设备的示意图；
图3是图2的一个爆炸图；
图4是图2的一个剖面图；
图5是根据本申请实施例的供电端和第二配合部的示意图；
图6是根据本申请一个实施例的无人机机架、无人机和归中机构的示意图；
图7是根据本申请一个实施例的机库的示意图。
附图标记：
机库1000、归中机构100、驱动电机10、动力齿轮11、转动杆21、配合齿轮211、移
动件30、推杆40、停放平台80、供电端801、接触凹槽8011、无人机机架9、安装本体91、支撑部911、第一镂空部9111、安装部912、第二镂空部9122、电连接线92、第一配合部921、接触凸点9211、第二配合部922、紧固安装件93、安装组件94、预埋螺母941、转接接头942、紧固件943、无人机200、电池201、换电机构300、换电驱动组件301、换电机械爪302、外部设备400。
具体实施方式
下面详细描述本申请的实施例，所述实施例的示例在附图中示出，其中自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。下面通过参考附图描述的实施例是示例性的，旨在用于解释本申请，而不能理解为对本申请的限制。
下文的公开提供了许多不同的实施例或例子用来实现本申请的不同结构。为了简化本申请的公开，下文中对特定例子的部件和设置进行描述。当然，它们仅仅为示例，并且目的不在于限制本申请。此外，本申请可以在不同例子中重复参考数字和/或字母。这种重复是为了简化和清楚的目的，其本身不指示所讨论各种实施例和/或设置之间的关系。此外，本申请提供了的各种特定的工艺和材料的例子，但是本领域普通技术人员可以意识到其他工艺的可应用于性和/或其他材料的使用。
下面，参照图1-图7具体描述本申请实施例的无人机机架9、机库1000和车辆。
参照图1-图4所示，无人机200设有充电端，外部供电电源可接入充电端向无人机200充电，充电端可设于无人机200的尾部、底部或顶部等位置。
无人机机架9包括：安装本体91和电连接线92，其中，安装本体91用于安装无人机200，安装本体91适于停放在停放平台80，也就是说，安装本体91可与无人机200进行固定，安装本体91的至少一部分位于无人机200的下方，安装本体91可实现无人机200的增高，避免无人机200降落时无人机200的机体与周围部件出现干涉，安装本体91还可以提升无人机200与停放平台80的接触面积，以降低无人机200降落在停放平台80上的操作难度。
电连接线92的第一端设有第一配合部921，第一配合部921适于与充电端电连接，第一配合部921可以与充电端保持插接固定的电连接状态，电连接线92的第二端连接至安装本体91底部的第二配合部922，第二配合部922适于与停放平台80的供电端801电连接，在无人机200停放在停放平台80时，第二配合部922可与停放平台80的供电端801接触以实现电连接，由此，充电电流可通过供电端801输出，并通过电连接线92传导至充电端，从而实现无人机200在停放平台80上自动进行充电。
需要说明的是，供电端801、充电端和电连接线92既可以传输电流以用于无人机200的充电，供电端801、充电端和电连接线92还可以传输数据，以便于无人机200在充电时将无人机200内部数据导出。可选地，充电端为Type-c母头，第一配合部921为Type-c公头。
在本申请的一些实施例中，无人机机架9可与不同型号的无人机200进行配套设计，以使无人机机架9与对应的无人机200配合紧密，走线通道将电连接线92的第一配合部 921引向对应无人机200的充电端，并保证电连接线92的第一配合部921与无人机200的充电端接口配套，以使无人机机架9可以匹配市场上任意型号无人机200的充电接口。
根据本申请实施例的无人机机架9，可安装于无人机200，无人机机架9包括安装本体91和电连接线92，在无人机200通过安装本体91停放在停放平台80时，电连接线92可将停放平台80的供电端801与无人机200的充电端导通，以实现无人机200在停放平台80上自动进行充电，从而有利于减少对无人机200充电的人工操作，提升用户体验。
在本申请的一些实施例中，参照图1-图4所示，安装本体91设有走线通道，走线通道延伸至安装本体91的底部，电连接线92安装至走线通道，走线通道可用于固定电连接线92，并控制电连接线92的走向，以避免电连接线92松脱和晃动，走线通道可设于安装本体91的内部一侧，以减少电连接线92的外漏，实现对电连接线92的隐藏，从而有利于减少电连接线92的对无人机200性能和美观性的影响，并提升电连接线92的使用寿命，走线通道内可设有适于与电连接线92过盈配合的卡槽。
在本申请的一些实施例中，参照图4和图5所示，第二配合部922包括接触凸点9211，供电端801设有接触凹槽8011，接触凸点9211适于伸入到接触凹槽8011，以使得第二配合部922和供电端801电连接，接触凸点9211和接触凹槽8011的配合，可实现多方向多角度充电，还便于第二配合部922与供电端801电连接的建立和分离，以避免第二配合部922与供电端801电连接的建立和分离影响无人机200的起降操作。
在本申请的另一些实施例中，第二配合部922包括无线充电接收器，供电端801设有无线充电发射器，在无人机200停放在停放平台80时，无线充电接收器可与无线充电发射器正对，以使得第二配合部922和供电端801电连接，进而实现无人机200的充电。
在本申请的一些实施例中，第二配合部922内设有安装通道，安装通道内设有弹性件，弹性件与接触凸点9211配合以朝向接触凸点9211施加作用力，作用力使得接触凸点9211具有伸出安装通道的趋势，安装通道可沿重力方向设置，接触凸点9211可在弹性件的作用力下由安装通道的下端伸出安装通道，无人机200降落后，第二配合部922在未与接触凹槽8011对齐配合时，接触凸点9211可在无人机200和无人机机架9的重力影响下，使弹性件压缩，接触凸点9211缩回安装通道内，从而使无人机200停稳，第二配合部922在与接触凹槽8011对齐配合时，接触凸点9211可在弹性件的作用力下伸出安装通道，并伸入至与接触凹槽8011的槽底止抵，从而有利于提升接触凸点9211与接触凹槽8011电连接的可靠性，避免虚接问题。可选地，弹性件与接触凸点9211构造成弹簧针，以使接触凸点9211可伸出和缩回安装通道。
在本申请的一些实施例中，接触凸点9211为多个，供电端801设有与多个接触凸点9211 一一对应的接触凹槽8011，以在每个接触凸点9211伸入到对应接触凹槽8011后形成充电回路，并增强充电回路的承载能力，从而有利于提升无人机200的充电速度。安装本体91上设有多个避让通孔，多个接触凸点9211与多个避让通孔一一对应设置，每个接触凸点9211可伸出相应的避让通孔以与供电端801接触，也就是说，无人机200降落后，在第二配合部922在未与接触凹槽8011对齐配合时，接触凸点9211可被压回避让通孔内，此时，避让通孔可保护接触凸点9211，减少接触凸点9211受到的压力，在第二配合部922在与接触凹槽8011对齐配合时，接触凸点9211可在弹性件的作用力下伸出相应的避让通孔，并深入至与接触凹槽8011的槽底止抵，从而有利于提升接触凸点9211与接触凹槽8011电连接的可靠性，避免虚接问题。可选地，每个接触凸点9211伸出避让通孔的最大长度为2mm～3mm。
在本申请的一些实施例中，参照图1-图4所示，安装本体91包括：支撑部911和安装部912，支撑部911适于支撑于停放平台80，支撑部911的至少一部分位可位于无人机200的下方，支撑部911可增大无人机200的机体与停放平台80的间距，避免无人机200降落时无人机200的机体与周围部件出现干涉，同时，支撑部911还可以提升无人机200与停放平台80的接触面积，以降低无人机200降落在停放平台80上的操作难度，此外，在无人机200降落时，支撑部911还可以实现缓冲减震的作用，降低无人机200在降落时受到的冲击力，从而有利于提升无人机200的安全性，在无人机200由于高频电磁干扰等原因异常坠地时避免无人机200摔坏。
安装部912设在支撑部911的顶部，安装部912和支撑部911配合限定出放置空间，放置空间的前部和后部均敞开以适于安装无人机200，无人机200的机体中部可穿设于放置空间，安装部912和支撑部911可环绕包覆无人机200的机体，以保证无人机200与安装本体91固定的稳定性。
在本申请的一些实施例中，参照图3所示，支撑部911的顶部形成为与无人机200配合的支撑面，支撑面设有第一镂空部9111，其中，支撑面可对无人机200底部进行支撑，第一镂空部9111可在重力方向贯穿支撑面，以使支撑面形成镂空结构，第一镂空部9111可减轻支撑部911的重量，以实现支撑部911的轻量化设计，从而有利于减轻无人机200飞行负载重量，提升无人机200的续航。同时，第一镂空部9111可以与无人机200底部的散热风口对应，以保证无人机200的底部散热风口散热畅通，第一镂空部9111还可以无人机200底部的设备接口对应，以避让无人机200底部的设备接口。
在本申请的一些实施例中，参照图3所示，安装部912设有第二镂空部9122，第二镂空部9122可在安装部912的厚度方向贯穿安装部912，以使安装部912形成镂空结构，第 二镂空部9122可减少安装部912的重量，以实现安装部912的轻量化设计，从而有利于减轻无人机200飞行负载重量，提升无人机200的续航。
在本申请的一些实施例中，第二镂空部9122可与无人机200的散热风口对应，以保证无人机200的散热风口散热畅通。优选地，在保证安装部912结构强度的情况下，安装部912设有多个第二镂空部9122，以进一步地减轻安装部912的重量。
在本申请的一些实施例中，参照图3所示，安装部912与支撑部911均可以是一体成型，以便于安装部912与支撑部911的生产，同时，安装部912与支撑部911通过多个紧固安装件93或卡扣等方式可拆卸地连接，以便于将无人机200固定在安装部912与支撑部911之间，从而有利于简化无人机机架9与无人机200的装配工序，减少装配偏差保证生产一致性。
在本申请的一些实施例中，参照图1和图3所示，安装部912可从无人机200的上方安装到位，支撑部911的支撑面扣在无人机200前端限位点，以使支撑部911与无人机200下底面贴合，将紧固安装件93预紧，以使安装部912与支撑部911进行连接，并在连接处保留一定预紧间隙，紧固后安装部912和支撑部911的支撑面与无人机200外壳型面贴合，无人机200外壳型面上可设有多个适于与安装部912和/或支撑部911限位配合的凸台限位块，以保证无人机200在任意方向均与无人机机架9配合紧密，无滑动脱出风险。
在本申请的一些实施例中，参照图3所示，紧固安装件93可以是螺栓，安装部912地底部预埋有适于与螺栓配合的螺母，螺栓可穿过支撑部911后与螺母固定，以使安装部912和支撑部911均与无人机200的外壳型面贴合，保证无人机机架9与无人机200配合紧密，防止无人机200滑动脱出放置空间。可选地，螺栓为沉头螺栓，螺母为GB809-A标准的M3*10嵌装圆螺母，安装部912和支撑部911可通过4个沉头螺栓连接。
在本申请的一些实施例中，安装部912为无人机200壳体的仿形结构设计，安装部912可与无人机200外表面紧密贴合，且安装部912可与无人机200壳体自带的凸起部分卡接，以使安装部912稳定地固定于无人机200。
在本申请的一些实施例中，参照图2和图3所示，安装部912的顶部设有用于安装外部设备400的安装组件94，以使外部设备400可通过与无人机机架9的安装组件94固定，实现对无人机200的功能的拓展，以使无人机200可通过外部设备400来满足救援搜寻、影视拍摄等复杂任务的执行条件，满足用户的个性化需求。可选地，外部设备400可以是运动相机、补光灯等。
在本申请的一些实施例中，参照图2和图3所示，安装组件94包括：螺孔941、转接接头942和紧固件943，螺孔941设置于安装部912的顶部，螺孔941可形成于预埋螺母， 预埋螺母预埋于安装部912的顶部，转接接头942与螺孔941螺纹配合，转接接头942伸出安装部912的端部设有固定孔，紧固件943适于与外部设备400和固定孔配合，由此，通过将外部设备400与紧固件943的拆装，用户可以根据需要灵活地更换外部设备400，从而有利于提升无人机200的实用性。另外，在外部设备400需要其他转接装置固定在安装部912时，可更换对应配套的转接接头942和紧固件943即可，螺孔941可与市面在售多款转接装置连接。
参照图1-图7所示，根据本申请第二方面实施例的机库1000，包括：停放平台80和上述实施例的中的无人机机架9，停放平台80设有供电端801，安装本体91停放于停放平台80时，第二配合部922适于与供电端801电连接。
根据本申请实施例的机库1000，停放平台80适于停放无人机200，无人机机架9可安装于无人机200，无人机机架9包括安装本体91和电连接线92，在无人机200通过安装本体91停放在停放平台80时，电连接线92可将停放平台80的供电端801与无人机200的充电端导通，以实现无人机200在停放平台80上自动进行充电，从而有利于减少对无人机200充电的人工操作，提升用户体验。
在本申请的一些实施例中，机库1000还包括与供电端801电连接的充电控制器，充电控制器用于控制供电端801的电输出，充电控制器可检测供电端801的电流量以判断是否停止电源输出，供电端801的电流大小可判断无人机200是否充满电，充电控制器可在无人机200充满电后及时断电以避免无人机200过充。具体地，在停放平台80的供电端801与无人机200的充电端导通后，充电控制器可对无人机200的充电电流与无人机200的电池电压进行监控，无人机200充电过程中供电端801的电流在4A左右，无人机200电量充满后电流降为0.1A以内，此时无人机200充满电，控制器停止对无人机200充电的电源输出，防止过充导致无人机200电池的损坏。
在本申请的一些实施例中，机库1000还包括电流检测回路，电流检测回路具有位于供电端801的两个间隔设置的触点，第二配合部922与两个触点接触时，电流检测回路导通以判定无人机机架9停放于停放平台80，也就是说，在第二配合部922的上的两个接触凸点9211分别与对应的两个触点接触时，停放平台80的供电端801与无人机200的充电端导通，电流检测回路处于有电流通过的导通状态，则判定无人机机架9停放于停放平台80，且无人机200可进行充电。在两个接触凸点9211未与两个触点接触时，停放平台80的供电端801与无人机200的充电端未导通，电流检测回路的电流为0，处于未导通状态，则可判定无人机机架9的第二配合部922未与供电端801电连接，无人机200未处于充电状态。
需要说明的是，电流检测回路的两个触点可以是单独设置于供电端801的触点，也可以将供电端801上两个接触凹槽8011作为触点。
在本申请的一些实施例中，参照6和图7所示，机库1000还包括归中机构100，归中机构100用于调整安装本体91在停放平台80的位置，以使安装本体91处于第二配合部922与供电端801电连接的归中状态，从而实现无人机200的自动归中和充电。
参照6和图7所示，归中机构100包括：驱动电机10、转动框架、移动件30以及推杆40，驱动电机10与转动框架动力连接，转动框架用于带动移动件30运动，而移动件30带动推杆40运动，推杆40用于推动位于停放平台80上的安装本体91运动，以使安装本体91带动无人机200实现自动归中，在安装本体91处于归中状态下，第二配合部922与供电端801正对，接触凸点9211伸入到接触凹槽8011，第二配合部922和供电端801电连接，无人机200可进行充电。
其中，驱动电机10的电机轴设有动力齿轮11，转动框架包括沿周向排布成方框形的多个转动杆21，每个转动杆21的至少一个端部设有配合齿轮211，其中一个转动杆21的端部的配合齿轮211与动力齿轮11啮合，其余转动杆21中的每个转动杆21的配合齿轮211与其相邻的配合齿轮211啮合使得每个转动杆21通过动力传输可转动，每个转动杆21均设有与其配合且相对其移动的移动件30，相互平行的两个转动杆21上的移动件30通过推杆40相连。
具体而言，在归中机构100所在的水平面内定义出横向和纵向，而推杆40可以包括一个横向上的第一杆以及一个纵向上的第二杆，第一杆用于调整无人机200在横向上的位置，而第二杆用于调整无人机200在纵向上的位置，以实现无人机200的自动归中。
对应转动杆21的数量为四个，其中纵向上相对的两个转动杆21与第一杆对应以带动第一杆在横向上运动，横向上相对的另两个转动杆21与第二杆对应以带动第二杆在纵向上运动，而至少相邻的两个转动杆21的两端均设置配合齿轮211，其他的转动杆21仅一端或两端均设置配合齿轮211，即可实现多个转动杆21的同步转动，进而实现横向以及纵向上同步的位置调整，实现无人机200的自动归中。
当然，本申请转动框架、移动件30以及推杆40的配合形式不限于此，在另一些实施例中，推杆40可以包括在横向上相对的两个第一杆以及在纵向上相对的两个第二杆，两个第一杆可以在横向上朝向或远离彼此运动，两个第二杆可以在纵向上朝向或远离彼此运动，以在两个第一杆以及两个第二杆均朝向彼此运动时，可推动支撑部911，并使支撑部911带动无人机200，对无人机200的横向位置和纵向位置进行矫正，使无人机200运动至中间位置，实现无人机200的自动归中。
进而，转动杆21也至少构造为四个，包括在横向上相对的两个横向转杆和纵向上相对的两个纵向转杆。驱动电机10为一个，驱动电机10的动力齿轮11与其中一个横向转杆或一个纵向转杆的配合齿轮211啮合，将动力传递至该转动杆21，而该转动杆21的另一端也设置配合齿轮211，且其他转动杆21通过配合齿轮211实现动力的依次传递，而转动杆21上设置与其动力连接的移动件30，转动杆21在驱动电机10带动下转动，并同步驱动移动件30移动，而移动件30用于带动两个第一杆朝向彼此或远离彼此运动，或带动两个第二杆朝向彼此或远离彼此运动。
示例性地，转动杆21以及推杆40还可以为6个、8个等，且使推杆40可以两两相向或相背运动，即可实现无人机200的自动归中。
需要说明的是，两个横向转杆上的移动件30与第二杆连接，并用于推动第二杆在纵向上运动，而两个纵向转杆上的移动件30与第一杆连接，并用于推动第一杆在横向上运动，且无人机200放置在归中机构100的中间位置上，可以避免无人机200出现偏置现象，以提高固定稳定性。
根据本申请实施例的归中机构100，通过设置驱动电机10、转动框架、移动件30以及推杆40，可以推动无人机200运动至中间位置，可以实现无人机200的自动归中，降低归中难度，并提高无人机200的固定稳定性，同时仅通过一个驱动电机10即可实现多个推杆40的动力驱动，可以有效降低归中机构100的成本，并降低控制难度。
在本申请的一些实施例中，参照图7所示，机库1000还包括换电机构300，换电机构300包括换电驱动组件301和换电机械爪302，换电机械爪302适于夹持和拆装无人机200的电池201，换电驱动组件301适于驱动换电机械爪302移动，在无人机200被归中机构100归中限位后，换电驱动组件301可驱动换电机械爪302将无人机200上缺电状态的电池201更换为满电状态的电池201，以实现快速补充无人机200的电量，增加无人机200的续航里程。可选地，换电驱动组件301构造为龙门丝杆滑台结构。
根据本申请第三方面实施例的车辆，包括：车身和上述实施例的中的机库1000，机库1000设置于车身的顶部，机库1000可作为车载设备使用，机库1000内的无人机200在起飞后，可将以更高的视角采集车辆周边的路况信息，可弥补车辆在“视觉”区域上的限制，有效提高车辆的视界，可以较好的获取车辆周围难以获取的环境信息，减少盲区，提升驾驶安全性，还可用于辅助车辆的自动驾驶。此外，在无人机200返航后，无人机200可通过无人机机架9上的电连接线92与停放平台80的供电端801电连接，车载电源可为供电端801供电，以实现自动充电的功能，省去人工操作的过程，并间接提高无人机200续航时间。另外，无人机200在人们的日常生活中也越来越普及作为拍摄、表演等，其与车辆 的结合也能满足无人机200的搭载转运便利性。
根据本申请实施例的车辆，其车身的顶部设有机库1000，机库1000的停放平台80适于停放无人机200，无人机机架9可安装于无人机200，无人机机架9包括安装本体91和电连接线92，在无人机200通过安装本体91停放在停放平台80时，电连接线92可将停放平台80的供电端801与无人机200的充电端导通，以实现无人机200在停放平台80上自动进行充电，从而有利于减少对无人机200充电的人工操作，提升用户体验。
在本申请的一些具体实施例中，车主或车载控制系统控制无人机200返航到停放平台80，或无人机200电量不足自动返航到停放平台80时，通过机库1000的归中机构100与无人机机架9的配合，将无人机200固定在停放平台80中央，此时第二配合部922与供电端801正对，接触凸点9211伸入到接触凹槽8011，第二配合部922和供电端801电连接，无人机200可进行自动充电，充电过程由充电控制器对充电电流与无人机200电池201电压进行监控，无人机200电量充满后电流降为0.1A以内，此时无人机200充满电，充电控制器停止对无人机200充电的电源输出。防止过充导致电池201的损坏。
在本申请的描述中，需要理解的是，术语“厚度”、“上”、“下”、“前”、“后”、“顶”、“底”、“内”、“外”、等指示的方位或位置关系为基于附图所示的方位或位置关系，仅是为了便于描述本申请和简化描述，而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作，因此不能理解为对本申请的限制。
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一个或者更多个该特征。在本申请的描述中，“多个”的含义是两个或两个以上，除非另有明确具体的限定。
在本申请中，除非另有明确的规定和限定，术语“安装”、“相连”、“连接”、“固定”等术语应做广义理解，例如，可以是固定连接，也可以是可拆卸连接，或成一体；可以是机械连接，也可以是电连接，还可以是通信；可以是直接相连，也可以通过中间媒介间接相连，可以是两个元件内部的连通或两个元件的相互作用关系。对于本领域的普通技术人员而言，可以根据具体情况理解上述术语在本申请中的具体含义。
在本申请中，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“一个实施例”、“一些实施例”、“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申请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。
尽管已经示出和描述了本申请的实施例，本领域的普通技术人员可以理解：在不脱离本申请的原理和宗旨的情况下可以对这些实施例进行多种变化、修改、替换和变型，本申请的范围由权利要求及其等同物限定。

Claims (15)

  1. 一种无人机机架，其中，无人机(200)设有充电端，所述无人机机架包括：
    安装本体(91)，所述安装本体(91)用于安装所述无人机(200)，所述安装本体(91)适于停放在停放平台(80)；
    电连接线(92)，所述电连接线(92)的第一端设有第一配合部(921)，所述第一配合部(921)适于与所述充电端电连接，所述电连接线(92)的第二端连接至所述安装本体(91)底部的第二配合部(922)，所述第二配合部(922)适于与所述停放平台(80)的供电端(801)电连接。
  2. 根据权利要求1所述的无人机机架，其中，所述安装本体(91)设有走线通道，所述走线通道延伸至所述安装本体(91)的底部，所述电连接线(92)安装至所述走线通道。
  3. 根据权利要求1或2所述的无人机机架，其中，所述第二配合部(922)包括接触凸点(9211)，所述供电端(801)设有接触凹槽(8011)，所述接触凸点(9211)适于伸入到所述接触凹槽(8011)以使得所述第二配合部(922)和所述供电端(801)电连接。
  4. 根据权利要求3所述的无人机机架，其中，所述第二配合部(922)内设有安装通道，所述安装通道内设有弹性件，所述弹性件与所述接触凸点(9211)配合以朝向所述接触凸点(9211)施加作用力，所述作用力使得所述接触凸点(9211)具有伸出所述安装通道的趋势。
  5. 根据权利要求3所述的无人机机架，其中，所述接触凸点(9211)为多个，所述安装本体(91)上设有多个避让通孔，多个所述接触凸点(9211)与所述多个避让通孔一一对应设置，每个所述接触凸点(9211)可伸出相应的所述避让通孔以与所述供电端(801)接触。
  6. 根据权利要求1-5中任一项所述的无人机机架，其中，所述安装本体(91)包括：
    支撑部(911)，所述支撑部(911)适于支撑于所述停放平台(80)；
    安装部(912)，所述安装部(912)设在所述支撑部(911)的顶部，所述安装部(912)和所述支撑部(911)配合限定出放置空间，所述放置空间的前部和后部均敞开以适于安装所述无人机(200)。
  7. 根据权利要求6所述的无人机机架，其中，所述支撑部(911)的顶部形成为与所述无人机配合的支撑面，所述支撑面设有第一镂空部(9111)。
  8. 根据权利要求6或7所述的无人机机架，其中，所述安装部(912)设有第二镂空部(9122)。
  9. 根据权利要求6-8中任一项所述的无人机机架，其中，所述安装部(912)的顶部设有用于安装外部设备(400)的安装组件(94)。
  10. 根据权利要求9所述的无人机机架，其中，所述安装组件(94)包括：
    螺孔(941)，所述螺孔(941)设置于所述安装部(912)的顶部；
    转接接头(942)，所述转接接头(942)与所述螺孔(941)螺纹配合，所述转接接头(942)伸出所述安装部(912)的端部设有固定孔；
    紧固件(943)，所述紧固件(943)适于与外部设备(400)和所述固定孔配合。
  11. 一种机库，其中，包括：
    停放平台(80)，所述停放平台(80)设有供电端(801)；
    无人机机架，所述无人机机架为根据权利要求1-10中任一项所述的无人机机架，所述安装本体(91)停放于所述停放平台(80)时，所述第二配合部(922)适于与所述供电端(801)电连接。
  12. 根据权利要求11所述的机库，其中，还包括与所述供电端(801)电连接的充电控制器，所述充电控制器用于控制所述供电端(801)的电输出。
  13. 根据权利要求11或12所述的机库，其中，还包括电流检测回路，所述电流检测回路具有位于所述供电端(801)的两个间隔设置的触点，所述第二配合部(922)与两个所述触点接触时，所述电流检测回路导通以判定所述无人机机架停放于所述停放平台(80)。
  14. 根据权利要求11-13中任一项所述的机库，其中，还包括归中机构(100),所述归中机构(100)用于调整所述安装本体(91)在所述停放平台(80)的位置，以使所述安装本体(91)处于所述第二配合部(922)与所述供电端(801)电连接的归中状态。
  15. 一种车辆，其中，包括：
    车身；
    机库，所述机库为根据权利要求11-14中任一项所述的机库，所述机库设置于所述车身的顶部。
PCT/CN2023/094505 2022-07-19 2023-05-16 无人机机架、机库和车辆 Ceased WO2024016807A1 (zh)

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