CN108128475A - A kind of unmanned plane automatic charging equipment - Google Patents

A kind of unmanned plane automatic charging equipment Download PDF

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Publication number
CN108128475A
CN108128475A CN201711329602.1A CN201711329602A CN108128475A CN 108128475 A CN108128475 A CN 108128475A CN 201711329602 A CN201711329602 A CN 201711329602A CN 108128475 A CN108128475 A CN 108128475A
Authority
CN
China
Prior art keywords
automatic charging
controller
unmanned plane
motivation
mini
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.)
Pending
Application number
CN201711329602.1A
Other languages
Chinese (zh)
Inventor
方佳
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.)
Fuzhou Tang Ying Intelligent Technology Co Ltd
Original Assignee
Fuzhou Tang Ying Intelligent 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 Fuzhou Tang Ying Intelligent Technology Co Ltd filed Critical Fuzhou Tang Ying Intelligent Technology Co Ltd
Priority to CN201711329602.1A priority Critical patent/CN108128475A/en
Publication of CN108128475A publication Critical patent/CN108128475A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F1/00Ground or aircraft-carrier-deck installations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/10Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
    • B60L53/14Conductive energy transfer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/30Constructional details of charging stations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00Type of vehicles
    • B60L2200/10Air crafts
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/70Energy storage systems for electromobility, e.g. batteries
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10Technologies relating to charging of electric vehicles
    • Y02T90/12Electric charging stations
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10Technologies relating to charging of electric vehicles
    • Y02T90/14Plug-in electric vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)
  • Toys (AREA)

Abstract

The invention discloses a kind of unmanned plane automatic charging equipment, structure includes:Automatic charging pedestal,Multifunctional foot stool,Protecting frame,Position indicator,Controller,Propeller,Automatic charging pedestal is set below Multifunctional foot stool,It is connected using electrical contact,Controller is equipped with above Multifunctional foot stool,Using electrical connection,Protecting frame is installed on the outside of propeller,It is connected using lock,Position indicator is installed on above controller,It is connected using button,Controller is in protecting frame in same level,Propeller is installed on four corners of controller,Using threaded connection,Automatic charging pedestal includes,Accumulator,Auxiliary block,Mini motivation,Relief spring block,Conductive lever,Connect contact,Contact head,Conductive trough,Accumulator is installed on left and right ends below mini motivation,It is electrically connected using conducting wire,When using equipment,Pass through the conductive locking bindiny mechanism being equipped with,It can reach simple and light,It is easy for installation,It is firm to lock,Charging more safety and stability.

Description

A kind of unmanned plane automatic charging equipment
Technical field
The present invention is a kind of unmanned plane automatic charging equipment, belongs to automatic charging apparatus field.
Background technology
Unmanned plane is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself, nothing on machine Cockpit, but the equipment such as automatic pilot, presetting apparatus are installed, on ground, naval vessels or machine tool remote control station personnel pass through The equipment such as radar, can be under wireless remotecontrol as conventional airplane one to it into line trace, positioning, remote control, telemetering and Digital Transmission Sample takes off or is launched with booster rocket, can also be taken to by machine tool it is aerial launch flight, during recycling, can with conventional airplane Process the same mode automatic Landing in land can also be recycled by remote control parachute or block, can be reused several times, used extensively In aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc.;
Prior art discloses application No. is a kind of 201621478670.5 use bottom plate, positioning device, driving devices With the structure design of charging unit, using the charging method of scientific optimization, existing unmanned plane charging technique is substantially improved not Foot, positioning when positioning device is landed for unmanned plane ensure dropping in special card slot for unmanned plane safety and precise, drive Dynamic device provides associated power for locking device, and locked and fixed of the locking device for completing to unmanned plane works, and will fill Electrode is accurately aimed at unmanned plane by electrode, multiple because installing when the prior art uses for carrying out charging operation to unmanned plane Miscellaneous, electronic structure is various, leads to weight, and maintenance difficulties are excessive, and inconvenience transport, use condition is limited.
Invention content
In view of the deficienciess of the prior art, it is an object of the present invention to provide a kind of unmanned plane automatic charging equipment, to solve Because installation is complicated when the prior art uses, electronic structure is various, leads to weight, and maintenance difficulties are excessive, inconvenience transport, use condition The problem of limited.
To achieve these goals, the present invention is to realize by the following technical solutions:A kind of unmanned plane automatic charging Equipment, structure include:Automatic charging pedestal, Multifunctional foot stool, protecting frame, position indicator, controller, propeller, it is described automatic Charging base is set below Multifunctional foot stool, is connected using electrical contact, controller is equipped with above the Multifunctional foot stool, using electricity Connection, the protecting frame are installed on the outside of propeller, are connected using lock, and the position indicator is installed on above controller, using button Connection, the controller are in protecting frame in same level, and the propeller is installed on four corners of controller, are used It is threadedly coupled, the automatic charging pedestal includes, accumulator, auxiliary block, mini motivation, relief spring block, conductive lever, connection Contact, contact head, conductive trough, the accumulator is installed on left and right ends below mini motivation, is electrically connected using conducting wire, described auxiliary Help block be set on mini motivation at left and right sides of, using lock connect, the mini motivation be set on relief spring block in side, top interlocking in Automatic charging pedestal, the relief spring block top are socketed with Multifunctional foot stool, the conductive lever by auxiliary block with it is mini Motivation is threadedly coupled, and the connection contact is installed on conductive lever top, and using electrical connection, the contact head is installed on decompression bullet Spring block upper right side, is connected using weldering, and the conductive trough is electrically connected by contact head with conductive lever.
Further, the propeller is equipped with 4 groups.
Further, it is equipped with Multifunctional foot stool below the automatic charging pedestal.
Further, it is equipped with controller below the position indicator.
Further, the protecting frame is equipped with 4 groups.
Advantageous effect
When a kind of unmanned plane automatic charging equipment of the present invention is worked, controlled on controller by main remote control 1 place coordinate position of the locking positioning automatic charging of position indicator 4 pedestal, protecting frame 3 protect propeller 6 to carry out flight rotation work, Landing place is reached, 2 bottom end relief spring block 104 of Multifunctional foot stool contacts 1 top charging connection slot of automatic charging pedestal, nobody Machine is stopped, and accumulator 101 works, and is connected by conducting wire, drives mini motivation 103, and then rotate in auxiliary block 102 The conductive lever 105 positioned at both ends is made to move outward under booster action, locking contact head 107 is squeezed, reaches and limit displacement model It encloses, mini motivation 103 is stopped, and conductive trough 108 connects accumulator 101, and circuit forming circuit carries out unmanned plane charging work, Make equipment in use, locking bindiny mechanism by the conduction being equipped with, can reach simple and light, easy for installation, locking jail It leans on, charging more safety and stability.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention, Objects and advantages will become more apparent upon:
Fig. 1 is a kind of structure diagram of unmanned plane automatic charging equipment of the present invention.
Fig. 2 is a kind of automatic charging understructure schematic diagram of unmanned plane automatic charging equipment of the present invention.
Fig. 3 is the structure diagram of A in Fig. 2.
In figure:Automatic charging pedestal -1, Multifunctional foot stool -2, protecting frame -3, position indicator -4, controller -5, propeller -6, Accumulator -101, auxiliary block -102, mini motivation -103, relief spring block -104, conductive lever -105, connection contact -106, Contact head -107, conductive trough -108.
Specific embodiment
To be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, with reference to Specific embodiment, the present invention is further explained.
- Fig. 3 is please referred to Fig.1, the present invention provides a kind of unmanned plane automatic charging equipment:Its structure includes:Automatic charging bottom Seat 1, Multifunctional foot stool 2, protecting frame 3, position indicator 4, controller 5, propeller 6, the automatic charging pedestal 1 are set on Multifunctional foot 2 lower section of frame, is connected using electrical contact, and 2 top of Multifunctional foot stool is equipped with controller 5, using electrical connection, the protecting frame 3 6 outside of propeller is installed on, is connected using lock, the position indicator 4 is installed on 5 top of controller, is connected using button, the control Device 5 and protecting frame 3 are in same level, and the propeller 6 is installed on four corners of controller 5, using threaded connection, The automatic charging pedestal 1 includes, accumulator 101, auxiliary block 102, mini motivation 103, relief spring block 104, conductive lever 105th, contact 106, contact head 107, conductive trough 108 are connected, the accumulator 101 is installed on mini 103 lower section left and right two of motivation End, is electrically connected using conducting wire, and the auxiliary block 102 is set on mini 103 left and right sides of motivation, is connected using lock, described mini dynamic Machine 103 is set on side in relief spring block 104, and top interlocking is in automatic charging pedestal 1,104 top of the relief spring block socket There is Multifunctional foot stool 2, the conductive lever 105 is threadedly coupled by auxiliary block 102 with mini motivation 103, the connection contact 106 are installed on 105 top of conductive lever, and using electrical connection, the contact head 107 is installed on 104 upper right side of relief spring block, adopts It is connected with weldering, the conductive trough 108 is electrically connected by contact head 107 with conductive lever 105, and the propeller 6 is equipped with 4 groups, institute It states 1 lower section of automatic charging pedestal and is equipped with Multifunctional foot stool 2,4 lower section of position indicator is equipped with controller 5, and the protecting frame 3 is equipped with 4 groups.
User is controlled by main remote control on controller when this equipment is used to carry out the work of unmanned plane automatic charging 1 place coordinate position of the locking positioning of position indicator 4 automatic charging pedestal, protecting frame 3 protects propeller 6 to carry out flight rotation work To make, reach landing place, 2 bottom end relief spring block 104 of Multifunctional foot stool contacts 1 top charging connection slot of automatic charging pedestal, Unmanned plane is stopped, and accumulator 101 works, and is connected by conducting wire, drives mini motivation 103, and then rotate and assisting The conductive lever 105 positioned at both ends is made to move outward under 102 booster action of block, locking contact head 107 is squeezed, reaches and limit position Range is moved, mini motivation 103 is stopped, and conductive trough 108 connects accumulator 101, and circuit forming circuit carries out unmanned plane charging Work.
Automatic charging pedestal of the present invention is equipped with relative to traditional common automatic charging equipment by equipment mini The components compositions such as motivation 103, relief spring block 104, conductive lever 105, connection contact 106, contact head 107, conductive trough 108 Conduction locking connection structure makes equipment more convenient to use quick, and automatic charging is more stablized.
The present invention solves the problems, such as it is because installation is complicated when the prior art uses, and electronic structure is various, leads to weight, safeguards Difficulty is excessive, and inconvenience transport, use condition is limited, and being combined with each other by above-mentioned component of the invention makes equipment in use, passing through The conductive locking bindiny mechanism being equipped with, can reach simple and light, easy for installation, and locking is firm, and charging more safety is steady It is fixed.
The basic principles, main features and the advantages of the invention have been shown and described above, for this field skill For art personnel, it is clear that the present invention is not limited to the details of above-mentioned exemplary embodiment, and without departing substantially from the present invention spirit or In the case of essential characteristic, the present invention can be realized in other specific forms.Therefore, in all respects, should all incite somebody to action Embodiment regards exemplary as, and is non-limiting, the scope of the present invention by appended claims rather than on state Bright restriction, it is intended that including all changes falling within the meaning and scope of the equivalent requirements of the claims in the present invention It is interior.Any reference numeral in claim should not be considered as to the involved claim of limitation.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should It considers the specification as a whole, the technical solutions in each embodiment can also be properly combined, forms those skilled in the art The other embodiment being appreciated that.

Claims (5)

1. a kind of unmanned plane automatic charging equipment, structure include:Automatic charging pedestal (1), Multifunctional foot stool (2), protecting frame (3), position indicator (4), controller (5), propeller (6), the automatic charging pedestal (1) are adopted below Multifunctional foot stool (2) Electricity consumption connects, and controller (5) is equipped with above the Multifunctional foot stool (2), using electrical connection, protecting frame (3) installation On the outside of propeller (6), connected using lock, it is characterised in that:
The position indicator (4) is installed on above controller (5), is connected using button, and the controller (5) is in protecting frame (3) In same level, the propeller (6) is installed on four corners of controller (5), using threaded connection;
The automatic charging pedestal (1) includes, accumulator (101), auxiliary block (102), mini motivation (103), relief spring block (104), conductive lever (105), connection contact (106), contact head (107), conductive trough (108), accumulator (101) installation The left and right ends below mini motivation (103), are electrically connected using conducting wire, and the auxiliary block (102) is set on mini motivation (103) left side Right both sides are connected using lock, and mini motivation (103) side in relief spring block (104), top interlocking is in automatic charging Pedestal (1), relief spring block (104) top are socketed with Multifunctional foot stool (2), and the conductive lever (105) passes through auxiliary Block (102) is threadedly coupled with mini motivation (103), and the connection contact (106) is installed on conductive lever (105) top, uses Electrical connection, the contact head (107) are installed on relief spring block (104) upper right side, are connected using weldering, the conductive trough (108) It is electrically connected by contact head (107) with conductive lever (105).
2. a kind of unmanned plane automatic charging equipment according to claim 1, it is characterised in that:The propeller (6) is equipped with 4 Group.
3. a kind of unmanned plane automatic charging equipment according to claim 2, it is characterised in that:The automatic charging pedestal (1) lower section is equipped with Multifunctional foot stool (2).
4. a kind of unmanned plane automatic charging equipment according to claim 2, it is characterised in that:Below the position indicator (4) Equipped with controller (5).
5. a kind of unmanned plane automatic charging equipment according to claim 2, it is characterised in that:The protecting frame (3) is equipped with 4 Group.
CN201711329602.1A 2017-12-13 2017-12-13 A kind of unmanned plane automatic charging equipment Pending CN108128475A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711329602.1A CN108128475A (en) 2017-12-13 2017-12-13 A kind of unmanned plane automatic charging equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711329602.1A CN108128475A (en) 2017-12-13 2017-12-13 A kind of unmanned plane automatic charging equipment

Publications (1)

Publication Number Publication Date
CN108128475A true CN108128475A (en) 2018-06-08

Family

ID=62390299

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711329602.1A Pending CN108128475A (en) 2017-12-13 2017-12-13 A kind of unmanned plane automatic charging equipment

Country Status (1)

Country Link
CN (1) CN108128475A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114454760A (en) * 2021-12-24 2022-05-10 广州极飞科技股份有限公司 Charging method, apparatus, system, device and medium

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114454760A (en) * 2021-12-24 2022-05-10 广州极飞科技股份有限公司 Charging method, apparatus, system, device and medium

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Application publication date: 20180608