CN107697314A - A kind of unmanned plane lifting gear - Google Patents

A kind of unmanned plane lifting gear Download PDF

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Publication number
CN107697314A
CN107697314A CN201710851248.2A CN201710851248A CN107697314A CN 107697314 A CN107697314 A CN 107697314A CN 201710851248 A CN201710851248 A CN 201710851248A CN 107697314 A CN107697314 A CN 107697314A
Authority
CN
China
Prior art keywords
platform
unmanned plane
horizontal
push rod
slide rail
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.)
Granted
Application number
CN201710851248.2A
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Chinese (zh)
Other versions
CN107697314B (en
Inventor
杨凌
文朋
冯小淋
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.)
Fu Jinjun
Original Assignee
Chengdu Tianqi Technology 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 Chengdu Tianqi Technology Co Ltd filed Critical Chengdu Tianqi Technology Co Ltd
Publication of CN107697314A publication Critical patent/CN107697314A/en
Application granted granted Critical
Publication of CN107697314B publication Critical patent/CN107697314B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • 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
    • B64F1/02—Arresting gear; Liquid barriers
    • A—HUMAN NECESSITIES
    • A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
    • A01M—CATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
    • A01M7/00—Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
    • 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
    • B60S—SERVICING, CLEANING, REPAIRING, SUPPORTING, LIFTING, OR MANOEUVRING OF VEHICLES, NOT OTHERWISE PROVIDED FOR
    • B60S5/00—Servicing, maintaining, repairing, or refitting of vehicles
    • B60S5/06—Supplying batteries to, or removing batteries from, vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/70—Energy storage systems for electromobility, e.g. batteries
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10—Technologies relating to charging of electric vehicles
    • Y02T90/14—Plug-in electric vehicles

Abstract

The present invention discloses a kind of unmanned plane lifting gear, belong to unmanned plane landing platform field, including support, platform and localization handspike, the stage+module is in cradle top, the localization handspike is located above platform, localization handspike is slidably connected with platform, localization handspike includes two relative horizontal push rods, two relative longitudinal push rods, the diameter parallel of horizontal push rod is in the horizontal direction of platform, the diameter parallel of longitudinal push rod is in the longitudinal direction of platform, horizontal push rod is slided along the longitudinal direction, and longitudinal push rod is slided in transverse direction；The region for the platform that localization handspike is enclosed is provided with opening, and retractable skylight is provided with opening；The present invention has simultaneously makes unmanned plane rest in specified location, conveniently carry out the follow-up function of ensureing operation to unmanned plane.

Description

A kind of unmanned plane lifting gear
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of unmanned plane lifting gear.
Background technology
The development of rotor wing unmanned aerial vehicle is more and more faster, and usage quantity is more and more, but existing situation, which is unmanned plane, not to be had Special landing platform, it is directly to land on ground mostly, then by manual recovery, then guarantee operation is carried out to unmanned plane, it is complete Into after ensureing operation, then unmanned plane is put into specified location and taken off, this wastes manpower significantly.
The content of the invention
A kind of the present invention is intended to provide unmanned plane landing platform, it would be preferable to support unmanned plane landing, and with automatically by nobody Machine pushes to the function that platform specified location ensure operation.
To reach above-mentioned purpose, the technical solution adopted by the present invention is as follows：A kind of unmanned plane lifting gear, including support, Platform and localization handspike, at the top of support, the localization handspike is located above platform the stage+module, and localization handspike is with putting down Platform is slidably connected, and localization handspike includes two relative horizontal push rods, two relative longitudinal push rods, and the axis of horizontal push rod is put down Row slides along the longitudinal direction in the horizontal direction of platform, the diameter parallel of longitudinal push rod in the longitudinal direction of platform, horizontal push rod, Longitudinal push rod is slided in transverse direction；The region for the platform that localization handspike is enclosed is provided with opening, is provided with opening retractable Skylight.
Preferably, the localization handspike is slidably connected by sliding block, slide rail and platform, and slide rail is arranged on platform, slide rail Including horizontal slide rail, longitudinal slide rail, the horizontal push rod slides along longitudinal slide rail, and transversely slide rail slides the longitudinal push rod.
The localization handspike is driven by the cylinder.
Preferably, be provided with vertical cylinder, horizontal air cylinder below the skylight, vertical cylinder connection skylight, horizontal air cylinder with Vertical cylinder connects, and horizontal air cylinder is arranged on platform lower surface.
Further, in addition to horizontal slide rail, horizontal slide rail are arranged on platform lower surface, and the vertical cylinder is slided with level Sliding block connection on rail.
Preferably, the platform around the opening is provided with keeper, and the upper surface of the keeper is not higher than platform Upper surface, the top of keeper is provided with blind hole, and the side wall of keeper is provided with pin-and-hole, and the pin-and-hole intersects vertically with blind hole, pin Bearing pin is provided with hole.
Further, be provided with positioning foot rest in the blind hole, the top of positioning foot rest is provided with anchor ear, anchor ear diameter parallel in Platform, the side wall of positioning foot rest are provided with fixing hole, and the fixing hole is adapted with bearing pin.
Preferably, the bearing pin has positioning cylinder driving.
Preferably, two opposite edges of the fence are provided with grating, and grating is connected with control device, control device control Make all cylinders.
Preferably, the platform is provided with several pod apertures.
Preferably, the platform includes web plate, and the opening is on the web plate.
Preferably, the skylight is web plate.
Beneficial effects of the present invention are：
1st, web plate has air-flow when dredging rotor wing unmanned aerial vehicle landing, reduces the effect of ground effect；
2nd, grating can detect the landing of unmanned plane in time, and the effect of action signal is provided for control module；
3rd, the setting of localization handspike and putter action module, unmanned plane can be made to be moved to specified location after landing；
4th, the setting of skylight and skylight action module, operation effectively can be conceded for the position below the ventral of unmanned plane Space；
5th, the setting of undercarriage positioning table and undercarriage locating module, it can make unmanned plane can be by effectively solid after landing It is fixed, prevent unmanned plane and the situation for being unfavorable for ensureing operation such as rock；
6th, using cylinder as power, by the control of control device, securely and reliably, it can effectively reduce and be produced because of work accident Raw injury.
Brief description of the drawings
Fig. 1 is schematic structural view of the invention；
Fig. 2 is top view of the present invention；
Fig. 3 is that the present invention removes the top-direction view after the web plate on platform；
Fig. 4 is that the present invention removes the bottom direction view after the web plate on platform；
Fig. 5 is vertical cylinder, horizontal air cylinder connection diagram；
Fig. 6 is positioning foot rest and positioning cylinder schematic diagram.
In figure：1- supports, 2- platforms, 31- keepers, 310- blind holes, 311- pin-and-holes, 312- bearing pins, 32- positioning foot rests, 320- anchor ears, 321- fixing holes, 4- skylights, 5- transverse directions push rod, 6- longitudinal push rods, 8- gratings, 50- longitudinal slide rails, 60- are laterally sliding Rail, 81- vertical cylinders, 810- horizontal slide rails, 82- horizontal air cylinders.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, below in conjunction with accompanying drawing, the present invention is entered Row is further described.
A kind of unmanned plane lifting gear as shown in figures 1 to 6, including support 1, platform 2, localization handspike, the platform 2 are installed At the top of support 1, the localization handspike is located at the top of platform 2, and localization handspike is slidably connected with platform 2, localization handspike bag Two relative 5, two relative longitudinal push rods 6 of horizontal push rod are included, the diameter parallel of horizontal push rod 5 is in the transverse direction side of platform 2 To the diameter parallel of longitudinal push rod 6 is slided along the longitudinal direction in the longitudinal direction of platform 2, horizontal push rod 5, and longitudinal push rod 6 is along horizontal stroke Slided to direction；The platform 2 that localization handspike encloses region is provided with opening, and openable skylight 4 is provided with opening.
The push rod is driven by the cylinder, specifically, vertically moving cylinder including one group of transverse shifting cylinder, one group.Every group Transverse shifting cylinder includes two transverse shifting cylinders, and two transverse shifting cylinders are connected with two longitudinal push rods 6 respectively makes two Individual longitudinal push rod 6 realizes the slip of horizontal direction；Every group vertically moves cylinder and vertically moves cylinder including two, and two longitudinal directions are moved Cylinder of taking offence is connected the slip for making two horizontal push rods 5 realize longitudinal direction with two horizontal push rods 5 respectively.
The localization handspike is slidably connected by sliding block, slide rail and support 1, and slide rail is arranged on platform 2, and slide rail includes horizontal stroke To slide rail 60, longitudinal slide rail 50, the horizontal push rod 5 slides along longitudinal slide rail 50, and the longitudinal push rod 6 transversely slide by slide rail 60 It is dynamic.
The slide rail is located at the lower section of platform 2, and push rod is connected by connector with the sliding block on slide rail.The connector bag Slide attachment plate, the push rod connecting plate of interconnection are included, slide attachment plate is connected with sliding block, and push rod connecting plate is connected with push rod.
The horizontal slide rail 60 has two, and two horizontal slide rails 60 are arranged at intervals, and longitudinal push rod 6 is in two horizontal slide rails 60 Upper slip；The longitudinal slide rail 50 has two, and two longitudinal slide rails 50 are arranged at intervals, and horizontal push rod 5 is in two longitudinal slide rails 50 Upper slip.
The transverse shifting cylinder has two groups, and two groups of transverse shifting cylinders connect with the sliding block in two horizontal slide rails 60 respectively Connect；The cylinder that vertically moves has two groups, and two groups vertically move cylinder and are connected respectively with the slide rail in two longitudinal slide rails 50.
The transverse shifting cylinder 60, the output end for vertically moving cylinder 50 connect corresponding slide attachment plate respectively.
Transverse shifting cylinder, to vertically move cylinder be Rodless cylinder, and the piston of cylinder is connected with slide attachment plate.
Wherein, transverse shifting cylinder arrangement vertically moves cylinder arrangement on sustained height on sustained height, same to make Slide attachment plate under one slide rail does not collide when mobile, between cylinder piston and slide attachment plate and/or sliding block and cunning Be equipped between block connecting plate height not wait increase post.
The lower section of the skylight 4 is provided with vertical cylinder 81, horizontal air cylinder 82, output end and the skylight 4 of vertical cylinder 81 Lower surface connects, and vertical cylinder 81 drives skylight 4 to make movement in vertical direction, output end and the vertical cylinder 81 of horizontal air cylinder 82 Cylinder body connects, and horizontal air cylinder 82 drives vertical cylinder 81 to make horizontal motion, cylinder body and the lower surface of platform 2 of horizontal air cylinder 82 Connection.Also include horizontal slide rail 810, horizontal slide rail 810 is arranged on the lower surface of platform 2, the cylinder body installation of the vertical cylinder 81 On sliding block on horizontal slide rail 810.
The vertical cylinder 81, horizontal slide rail 810 respectively have two, and two vertical cylinders 81 are symmetrically located under skylight 4 Side, described two vertical cylinders 81 are connected with horizontal air cylinder 82.
Two skylights 4 are provided with the opening, two skylights 4 close the opening side by side, and two skylights 4 are in the horizontal direction The upper direction of motion is opposite.
The parameatal platform 2 is provided with several keepers 31, and the number of keeper 31 and position should be with nobody Machine undercarriage is corresponding.Without departing from the upper surface of platform 2, the top of keeper 31 is provided with blind hole for the upper surface of the keeper 31 310, the blind hole 310 is countersunk head blind hole, and the side wall of keeper 31 is provided with pin-and-hole 311, and the pin-and-hole 311 is vertical with blind hole 310 Intersecting, pin-and-hole 311 intersects with the inclined-plane on the top of blind hole 310, and bearing pin 312 is provided with pin-and-hole 311.
Positioning foot rest 32 is provided with the blind hole 310, the bottom of positioning foot rest 32 is adapted with blind hole 310, positioning foot rest 32 top is provided with anchor ear 320, and the diameter parallel of anchor ear 320 is provided with fixing hole 321, institute in platform 2, the side wall of positioning foot rest 32 Fixing hole 321 is stated to be adapted with bearing pin 312.
The bearing pin 312 is driven by positioning cylinder, and the output end of positioning cylinder connects the bearing pin 312.
Two relative edges of the platform 2 are provided with grating 8, and grating 8 is connected with control device, the cylinder connection There is air valve, source of the gas connects cylinder by air valve, and the control device is connected with air valve.
The platform 2 is provided with several pod apertures.The platform 2 includes web plate, and web plate is in platform 2, the skylight 4 For mesh-plate structure.
In use, grating 8 is first it is detected that have unmanned plane landing, and signal is passed into control device, control device leads to Cross two groups of transverse shifting cylinders of Air Valve Control, two groups vertically move cylinder action, most at last unmanned plane from landing place on platform 2 It is pushed into the top of skylight 4；Control device controls air valve vertical cylinder 81, horizontal air cylinder 82 is successively acted again, makes two pieces of skylights 4 Removed again to both sides after sinking, expose the working space of the lower section of platform 2；Finally, control device makes positioning cylinder by air valve again Action, bearing pin 312 is pushed into pin-and-hole, locks unmanned plane undercarriage.
Certainly, the present invention can also have other various embodiments, ripe in the case of without departing substantially from spirit of the invention and its essence Various corresponding changes and deformation, but these corresponding changes and deformation can be made according to the present invention by knowing those skilled in the art The protection domain of appended claims of the invention should all be belonged to.

Claims (10)

  1. A kind of 1. unmanned plane lifting gear, it is characterised in that：Including support (1), platform (2) and localization handspike, the platform (2) Installed in the top of support (1), the localization handspike is located above platform (2), and localization handspike is slidably connected with platform (2), fixed Position push rod includes two relative horizontal push rods (5), two relative longitudinal push rods (6), the diameter parallel of horizontal push rod (5) in The horizontal direction of platform (2), the diameter parallel of longitudinal push rod (6) is in the longitudinal direction of platform (2), and horizontal push rod (5) is along longitudinal direction Direction is slided, and longitudinal push rod (6) is slided in transverse direction；The region for the platform (2) that localization handspike is enclosed is provided with opening, opening It is interior to be provided with retractable skylight (4).
  2. A kind of 2. unmanned plane lifting gear according to claim 1, it is characterised in that：The localization handspike by sliding block, Slide rail is slidably connected with platform (2), and slide rail is arranged on platform (2), and slide rail includes horizontal slide rail (60), longitudinal slide rail (50), The horizontal push rod (5) is slided along longitudinal slide rail (50), and transversely slide rail (60) slides the longitudinal push rod (6).
  3. A kind of 3. unmanned plane lifting gear according to claim 1, it is characterised in that：It is provided with below the skylight (4) perpendicular Straight cylinder (81), horizontal air cylinder (82), vertical cylinder (81) connection skylight (4), horizontal air cylinder (82) connect with vertical cylinder (81) Connect, horizontal air cylinder (82) is arranged on platform (2) lower surface.
  4. A kind of 4. unmanned plane lifting gear according to claim 3, it is characterised in that：Also include horizontal slide rail (810), water Smooth rail (810) is arranged on platform (2) lower surface, and the vertical cylinder (81) is arranged on the sliding block on horizontal slide rail (810).
  5. A kind of 5. unmanned plane lifting gear according to claim 1, it is characterised in that：The parameatal platform (2) Keeper (31) is provided with, the upper surface of the keeper (31) is not higher than the upper surface of platform (2), the top of keeper (31) Provided with blind hole (310), the side wall of keeper (31) is provided with pin-and-hole (311), and pin-and-hole (311) is located at below platform (2), pin-and-hole (311) intersected vertically with blind hole (310), bearing pin (312) is provided with pin-and-hole (311).
  6. A kind of 6. unmanned plane lifting gear according to claim 5, it is characterised in that：It is fixed to be provided with the blind hole (310) Position foot stool (32), the top of positioning foot rest (32) are provided with anchor ear (320), and anchor ear (320) diameter parallel is in platform (2), angle The side wall of frame (32) is provided with fixing hole (321), and the fixing hole (321) is adapted with bearing pin (311).
  7. A kind of 7. unmanned plane lifting gear according to claim 6, it is characterised in that：The bearing pin (312) is by positioning gas Cylinder is driven, and the localization handspike is driven by the cylinder.
  8. A kind of 8. unmanned plane lifting gear according to claim 1-7 any one, it is characterised in that：The platform (2) Two opposite edges on have a grating (8), grating (8) connection control device, control device controls all cylinders.
  9. A kind of 9. unmanned plane lifting gear according to claim 1, it is characterised in that：The platform (2) is provided with several Pod apertures.
  10. A kind of 10. unmanned plane lifting gear according to claim 1, it is characterised in that：The platform (2) includes web plate, The opening is on the web plate.
CN201710851248.2A 2017-05-19 2017-09-20 Unmanned aerial vehicle take-off and landing device Expired - Fee Related CN107697314B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN2017103595169 2017-05-19
CN201710359516 2017-05-19

Publications (2)

Publication Number Publication Date
CN107697314A true CN107697314A (en) 2018-02-16
CN107697314B CN107697314B (en) 2020-04-28

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Family Applications (10)

Application Number Title Priority Date Filing Date
CN201721205975.3U Active CN207243451U (en) 2017-05-19 2017-09-20 A kind of medicine-filling device
CN201721211872.8U Active CN207360600U (en) 2017-05-19 2017-09-20 Unmanned plane battery grips mechanism action device
CN201710851248.2A Expired - Fee Related CN107697314B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle take-off and landing device
CN201721214766.5U Active CN207360602U (en) 2017-05-19 2017-09-20 Unmanned plane battery gripping body
CN201710857322.1A Active CN107651205B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle location battery system
CN201721205974.9U Active CN207141422U (en) 2017-05-19 2017-09-20 A kind of unmanned plane landing platform
CN201710851229.XA Active CN107719329B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle support system
CN201721208723.6U Active CN207355319U (en) 2017-05-19 2017-09-20 A kind of automatic liquid medicine injection system
CN201710855244.1A Active CN107640079B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle endurance guarantee method
CN201721214696.3U Active CN207360291U (en) 2017-05-19 2017-09-20 Unmanned plane takes battery system

Family Applications Before (2)

Application Number Title Priority Date Filing Date
CN201721205975.3U Active CN207243451U (en) 2017-05-19 2017-09-20 A kind of medicine-filling device
CN201721211872.8U Active CN207360600U (en) 2017-05-19 2017-09-20 Unmanned plane battery grips mechanism action device

Family Applications After (7)

Application Number Title Priority Date Filing Date
CN201721214766.5U Active CN207360602U (en) 2017-05-19 2017-09-20 Unmanned plane battery gripping body
CN201710857322.1A Active CN107651205B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle location battery system
CN201721205974.9U Active CN207141422U (en) 2017-05-19 2017-09-20 A kind of unmanned plane landing platform
CN201710851229.XA Active CN107719329B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle support system
CN201721208723.6U Active CN207355319U (en) 2017-05-19 2017-09-20 A kind of automatic liquid medicine injection system
CN201710855244.1A Active CN107640079B (en) 2017-05-19 2017-09-20 Unmanned aerial vehicle endurance guarantee method
CN201721214696.3U Active CN207360291U (en) 2017-05-19 2017-09-20 Unmanned plane takes battery system

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CN (10) CN207243451U (en)

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CN110382362A (en) * 2017-12-28 2019-10-25 深圳市大疆创新科技有限公司 A kind of positioning device of unmanned plane
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CN108482697B (en) * 2018-06-06 2023-09-19 深圳草莓创新技术有限公司 Unmanned aerial vehicle automatic positioning charging device and method thereof
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