CN108945506A - Energy supply airplane parking area mechanism for unmanned plane - Google Patents

Abstract

The invention discloses a kind of energy supply airplane parking area mechanisms for unmanned plane; belong to air vehicle technique field; including the first airplane parking area, the second airplane parking area and energy supply component, the first airplane parking area includes the first ducted body, the first guide rail, the second guide rail, first servo motor, the first screw rod, the first pedestal, the first support arm, the second support arm, first electrode bar, first electrode plate and control unit；Second airplane parking area includes the second ducted body, third guide rail, the 4th guide rail, the second servo motor, the second screw rod, the second pedestal, third support arm, the 4th support arm, second electrode bar and second electrode plate；Energizing component includes storage assembly and bearing assembly.The present invention reach can reduce unmanned plane charge maintenance needed for manpower and material resources, keep charging process convenient；Improve the technical effect of the working efficiency of unmanned plane.

Description

Energy supply airplane parking area mechanism for unmanned plane

Technical field

The invention belongs to air vehicle technique field, in particular to a kind of energy supply airplane parking area mechanism for unmanned plane.

Background technique

Unmanned unmanned plane referred to as " unmanned plane ", is grasped using radio robot and the presetting apparatus provided for oneself Vertical not manned unmanned plane.Without cockpit on machine, but automatic pilot, presetting apparatus, information collecting device are installed etc. Equipment.On ground, naval vessels or machine tool remote control station personnel are by the equipment such as radar, it is tracked, is positioned, is remotely controlled, telemetering and Digital Transmission.It can take off as common unmanned plane under wireless remotecontrol or be launched with booster rocket, it can also be by machine tool Aerial launch is taken to fly.Unmanned plane be usually used in mountain area and across great rivers transmission line of electricity inspection, and ice damage, Floods, landslide, carry out line walking inspection at earthquake during night.

For unmanned plane, unmanned plane in the prior art.After usually fully charged to unmanned plane, by automobile by nobody Machine is transported to field region to be inspected (by the transmission line of electricity for such as needing inspection)；After unmanned plane reaches region to be inspected, operator Member treats region of patrolling and examining progress line walking inspection to control unmanned plane.But since the battery durable ability of unmanned plane itself is limited, If the electricity of battery is depleted, need operator that unmanned plane is packed into automobile, from field transport to interior, manually to nothing It is man-machine to charge.Region to be inspected is transported after unmanned plane is fully charged, then by unmanned plane, carries out inspection work.This makes Every frame unmanned plane requires to be equipped with special operator and vehicle and carries out charge maintenance to it, the process of transport but also nobody The work times of machine are few.

In conclusion in the prior art, there is the charge maintenances to unmanned plane, waste manpower and material resources, charged Journey is inconvenient；The working efficiency of unmanned plane is low.

Summary of the invention

The technical problem to be solved by the present invention is to the charge maintenances to unmanned plane, waste manpower and material resources, charging process It is inconvenient；The working efficiency of unmanned plane is low.

In order to solve the above technical problems, the present invention provides a kind of energy supply airplane parking area mechanism for unmanned plane, the use In unmanned plane energy supply airplane parking area mechanism include the first airplane parking area, first airplane parking area include the first ducted body, described first Ducted body is provided with first side, second side, third side, the 4th side, the first bottom surface and the first opening face, and described first First interface, second interface and first through hole are provided on side, the first interface and the second interface are relative to described First through hole is symmetrical；Third interface, the 4th interface and first node, the third interface are provided in the second side It is symmetrical relative to the first node with the 4th interface；First guide rail, first guide rail are provided with the first fastening End and the second fastening end, first fastening end are fixedly connected with the first interface, second fastening end and the third Interface is fixedly connected；Second guide rail, second guide rail are provided with third fastening end and the 4th fastening end, the third fastening end It is fixedly connected with the second interface, the 4th fastening end is fixedly connected with the 4th interface；First servo motor, it is described First servo motor includes the first noumenon and first rotating shaft, and the first noumenon is fixedly connected with the first side, and described One shaft passes through the first through hole；First screw rod, first screw rod include the first screw rod and the first sliding block, first spiral shell One end of bar is fixedly connected with the first rotating shaft, and the other end of first screw rod is fixedly connected with the first node；The One pedestal, first pedestal are provided with first movement end, the second mobile terminal and the first conformable region, the first movement end setting There are the first slot and the first spacing zone, first guide rail passes through first slot, and first slot is located at described the Between one fastening end and second fastening end；Second mobile terminal is provided with the second slot and the second spacing zone, and described Two guide rails pass through second slot, and second slot is between the third fastening end and the 4th fastening end； First sliding block is fixed on first conformable region；First support arm, first support arm be provided with the first support end and Second support end, first support end and first spacing zone are hinged；

Second support arm, second support arm are provided with third support end and the 4th support end, the third support end It is hinged with second spacing zone；First electrode bar, the first electrode bar are provided with the first locking end and the second locking end, First locking end is fixedly connected with second support end, second locking end and the fixed company of the 4th support end It connects；First electrode plate, the first electrode plate and first opening face are detachably connected, and the first electrode plate is located at institute It states between the first support end and the third support end；Control unit, the control unit are connected with the first noumenon, and institute First through hole is stated between the first noumenon and the control unit；Wherein, the first side and the second side It is two opposed faces, the third side and the 4th side are two opposed faces, first bottom surface and One opening face is two opposed faces；First fastening end and second fastening end are the two of the first guide rail opposition End；The third fastening end and the 4th fastening end are the both ends of the second guide rail opposition；First sliding block is set in The outside of first screw rod, first screw rod and the first side are vertical, and first screw rod and described second side Face is vertical；The first movement end and second mobile terminal are symmetrical relative to first conformable region；Described first moves Moved end between the first electrode plate and first bottom surface, and second mobile terminal be located at the first electrode plate and Between first bottom surface；Second airplane parking area, second airplane parking area include the second ducted body, and second ducted body is provided with 5th side, the 6th side, heptalateral face, the 8th side, the second bottom surface and the second opening face, are provided on the 5th side 5th interface, the 6th interface and the second through-hole, the 5th interface and the 6th interface are symmetrical relative to second through-hole Distribution；The 7th interface, the 8th interface and second node are provided on 6th side, the 7th interface and the described 8th connect Mouth is symmetrical relative to the second node；Third guide rail, the third guide rail are provided with the 5th fastening end and the 6th fastening End, the 5th fastening end are fixedly connected with the 5th interface, and the 6th fastening end is fixedly connected with the 7th interface； 4th guide rail, the 4th guide rail are provided with the 7th fastening end and the 8th fastening end, and the 7th fastening end and the described 6th connect Mouth is fixedly connected, and the 8th fastening end is fixedly connected with the 8th interface；Second servo motor, second servo motor Including the second ontology and the second shaft, second ontology is fixedly connected with control unit, and second shaft is across described Second through-hole；Second screw rod, second screw rod include the second screw rod and the second sliding block, one end of second screw rod and described Second shaft is fixedly connected, and the other end of second screw rod is fixedly connected with the second node；Second pedestal, described second Pedestal is provided with third mobile terminal, the 4th mobile terminal and the second conformable region, and the third mobile terminal is provided with third slot and Three spacing zones, the third guide rail passes through the third slot, and the third slot is located at the 5th fastening end and described Between 6th fastening end；4th mobile terminal is provided with the 4th slot and the 4th spacing zone, and the 4th guide rail passes through described 4th slot, and the 4th slot is between the 7th fastening end and the 8th fastening end；Second sliding block is solid It is scheduled on second conformable region；Third support arm, the third support arm is provided with the 5th support end and the 6th support end, described 5th support end is connected with the third spacing zone；4th support arm, the 4th support arm are provided with the 7th support end and Eight support ends, the 7th support end are connected with the 4th spacing zone；Second electrode bar, the second electrode bar are provided with Three locking ends and the 4th locking end, the third locking end are connected with the 6th support end, the 4th locking end and described The connection of 8th support end；Second electrode plate, the second electrode plate and second opening face are detachably connected, and described second Electrode plate is between the 5th support end and the 7th support end；Wherein, the 6th side and second side are removable Unload connection；5th side and the 6th side are two opposed faces, heptalateral face and the 8th side It is two opposed faces, second bottom surface and the second opening face are two opposed faces；5th fastening end and institute State the both ends that the 6th fastening end is the third guide rail opposition；7th fastening end and the 8th fastening end are the described 4th The both ends of guide rail opposition；Second sliding block is set in the outside of second screw rod, second screw rod and the 5th side Face is vertical, and second screw rod and the 6th side are vertical；The third mobile terminal and the 4th mobile terminal relative to Second conformable region is symmetrical；The third mobile terminal between the second electrode plate and second bottom surface, and 4th mobile terminal is between the second electrode plate and second bottom surface；Component is energized, the energy supply component includes Storage assembly, the storage assembly are provided with the first charging interface and the second charging interface, first charging interface and first The connection of electric shock area, and first charging interface and the second electric shock area connection, and first charging interface and third electric shock area Connection, and first charging interface and the 4th electric shock area connection；Second charging interface and first touches a connection, and institute It states the second charging interface and second and touches a connection, and second charging interface and third touch a connection, and described second Charging interface and the 4th touches a connection；Bearing assembly, the bearing assembly include memory block and the second firm face, the electric power storage Component is fixed in the memory block, and the second firm face is fixedly connected with the first firm face；Wherein, first electric shock area Between first charging interface and first electrode bar, second electric shock area is located at first charging interface and described Between first electrode bar；Third electric shock area is between first charging interface and second electrode bar, the 4th touching Electric area is between first charging interface and the second electrode bar.

Further, the energy supply airplane parking area mechanism for unmanned plane further includes the first foot pad；Second foot pad；Described One bottom surface is additionally provided with the first corner region and the second corner region, and first foot pad is fixed on first corner region, and described Two foots pad are fixed on second corner region.

Further, the energy supply airplane parking area mechanism for unmanned plane includes that first corner region is located at described first Between foot pad and first opening face, second corner region is between second foot pad and first opening face.

Further, the energy supply airplane parking area mechanism for unmanned plane includes the first detector；Second detector；It is described First opening face is additionally provided with the first detection zone and the second detection zone, and first detector is fixed on first detection zone, Second detector is fixed on second detection zone.

Further, the energy supply airplane parking area mechanism for unmanned plane includes that first detection zone is located at described first Between detector and first bottom surface, second detection zone is between second detector and first bottom surface.

Further, the energy supply airplane parking area mechanism for unmanned plane further includes the first guiding groove, first guidance Slot and the first electrode plate are detachably connected, and first guiding groove and the third side are detachably connected；Described One guiding groove is between first support end and second support end.

Further, the energy supply airplane parking area mechanism for unmanned plane further includes the second guiding groove, second guidance Slot and the first electrode plate are detachably connected, and first guiding groove and the 4th side are detachably connected；Described Two guiding grooves are between the third support end and the 4th support end.

Further, it is cathode that the energy supply airplane parking area mechanism for unmanned plane, which includes the first electrode plate,.

Further, it is anode that the energy supply airplane parking area mechanism for unmanned plane, which includes the first electrode bar,.

Further, it is anode that the energy supply airplane parking area mechanism for unmanned plane, which includes the second electrode bar,.

The utility model has the advantages that the present invention provides a kind of energy supply airplane parking area mechanism for unmanned plane, by the first airplane parking area First through hole is set in the first side of first ducted body, by the first rotating shaft of first servo motor pass through first through hole, first One end of the first screw rod is fixedly connected with first rotating shaft in screw rod, by the first node of the other end of the first screw rod and first side It is fixedly connected.First fastening end of the first guide rail is fixedly connected with the first interface of first side, the second of the first guide rail is tight Fixed end is fixedly connected with the third interface of second side, and the first guide rail passes through first slot at first movement end in the first pedestal； The third fastening end of second guide rail is fixedly connected with the second interface of first side, the 4th fastening end of the second guide rail and second side 4th interface in face is fixedly connected, and the second guide rail passes through the second slot of the second mobile terminal in the first pedestal.By the first support arm The first support end and first spacing zone at first movement end be hinged, the third support end of the second support arm and the second mobile terminal The second spacing zone be hinged.First locking end in first electrode bar is fixedly connected with the second support end, the second locking end and 4th support end is fixedly connected.First electrode plate and the first opening face are detachably connected.Control unit and first servo motor The first noumenon connection, after the first rotating shaft of first servo motor passes through first through hole, the first of first rotating shaft and the first screw rod Screw rod connection, the first conformable region of the first pedestal is fixedly connected with the first sliding block being set in outside the first screw rod, is watched by first The first electrode bar for taking motor band can be towards the direction movement that unmanned plane needs to charge.Then stop when unmanned plane drops to first When on machine level ground, charged by first electrode bar and first electrode plate to unmanned plane.In second in the second airplane parking area The second through-hole is set on 5th side of hollow body, by the second shaft of the second servo motor in the second through-hole, the second screw rod One end of second screw rod is fixedly connected with the second shaft, by the other end of the second screw rod and the fixed company of the second node of the 6th side It connects.5th fastening end of third guide rail is fixedly connected with the 5th interface, the 6th fastening end of third guide rail and the 7th interface are solid Fixed connection, third guide rail pass through the third slot of third mobile terminal in the second pedestal；The 7th fastening end and the 6th of 4th guide rail Interface is fixedly connected, and the 8th fastening end of the 4th guide rail is fixedly connected with the 8th interface, and the 4th guide rail is passed through across the second pedestal In the 4th mobile terminal the 4th slot.Second electrode plate and the second opening face are detachably connected, and control unit and the second ontology connect It connects.Second conformable region of the second pedestal is fixedly connected with the second sliding block for being set in the second screw rod, by the second servo motor band Second electrode bar the direction that charge can be needed mobile towards unmanned plane.Then when unmanned plane drops on the second airplane parking area When, it can be charged by second electrode bar and second electrode plate for unmanned plane.Meanwhile by the way that electric power storage group in component will be energized First charging interface of part and first electric shock area connection, the first charging interface and second electric shock area connection, the first charging interface and Third electric shock area's connection, the first charging interface and the 4th electric shock area connection；Second charging interface and first are touched into a connection, the Two charging interfaces and second touch a connection, and the second charging interface and third touch a connection, and the second charging interface and the 4th touches Contact connection.Storage assembly is fixed in the memory block of bearing assembly again, the firm face of the second of bearing assembly and first consolidates Face is fixedly connected.Then it can charge for unmanned plane.To reach can reduce unmanned plane charge maintenance needed for manpower Material resources keep charging process convenient；Improve the technical effect of the working efficiency of unmanned plane.

Detailed description of the invention

It in order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, below will be to institute in embodiment Attached drawing to be used is needed to be briefly described, it should be apparent that, the accompanying drawings in the following description is only some implementations of the invention Example, for those of ordinary skill in the art, without creative efforts, can also obtain according to these attached drawings Obtain other attached drawings.

Fig. 1 is a kind of overall structure diagram of the charging unit for unmanned plane provided in an embodiment of the present invention；

Fig. 2 is a kind of left view schematic diagram of the charging unit for unmanned plane provided in an embodiment of the present invention；

Fig. 3 is a kind of right view schematic diagram of the charging unit for unmanned plane provided in an embodiment of the present invention；

Fig. 4 provides a kind of the first airplane parking area structural schematic diagram of charging unit for unmanned plane for the embodiment of the present invention；

Fig. 5 provides a kind of structural block diagram of the control unit of charging unit for unmanned plane for the embodiment of the present invention.

Specific embodiment

The invention discloses a kind of energy supply airplane parking area mechanism for unmanned plane, by first hollow in the first airplane parking area First through hole is set in the first side of body, the first rotating shaft of first servo motor is passed through into first through hole, the in the first screw rod One end of one screw rod is fixedly connected with first rotating shaft, by the other end of the first screw rod and the fixed company of the first node of first side It connects.First fastening end of the first guide rail is fixedly connected with the first interface of first side, the second fastening end of the first guide rail and The third interface of second side is fixedly connected, and the first guide rail passes through first slot at first movement end in the first pedestal；Second leads The third fastening end of rail is fixedly connected with the second interface of first side, and the of the 4th fastening end of the second guide rail and second side Four interfaces are fixedly connected, and the second guide rail passes through the second slot of the second mobile terminal in the first pedestal.By the first of the first support arm First spacing zone at support end and first movement end is hinged, and the second of the third support end of the second support arm and the second mobile terminal Spacing zone is hinged.First locking end in first electrode bar is fixedly connected with the second support end, the second locking end and the 4th Support end is fixedly connected.First electrode plate and the first opening face are detachably connected.The first of control unit and first servo motor Body connection, after the first rotating shaft of first servo motor passes through first through hole, the first screw rod of first rotating shaft and the first screw rod connects It connects, the first conformable region of the first pedestal is fixedly connected with the first sliding block being set in outside the first screw rod, by first servo motor The direction that the first electrode bar of band can need to charge towards unmanned plane is mobile.Then when unmanned plane drops on the first airplane parking area When, it is charged by first electrode bar and first electrode plate to unmanned plane.Pass through the second ducted body in the second airplane parking area The second through-hole is set on 5th side, the second shaft of the second servo motor is passed through into the second through-hole, the second spiral shell in the second screw rod One end of bar is fixedly connected with the second shaft, and the second node of the other end of the second screw rod and the 6th side is fixedly connected.It will 5th fastening end of third guide rail is fixedly connected with the 5th interface, the 6th fastening end of third guide rail and the fixed company of the 7th interface It connects, third guide rail passes through the third slot of third mobile terminal in the second pedestal；7th fastening end of the 4th guide rail and the 6th interface It is fixedly connected, the 8th fastening end of the 4th guide rail is fixedly connected with the 8th interface, and the 4th guide rail passes through the in the second pedestal 4th slot of four mobile terminals.Second electrode plate and the second opening face are detachably connected, control unit and the connection of the second ontology.It will Second conformable region of the second pedestal is fixedly connected with the second sliding block for being set in the second screw rod, by the second of the second servo motor band The direction that electrode stem can need to charge towards unmanned plane is mobile.Then when unmanned plane drops on the second airplane parking area, pass through Second electrode bar and second electrode plate can charge for unmanned plane.Meanwhile by the way that storage assembly in component will be energized One charging interface and the first electric shock area connection, the first charging interface and the second electric shock area connection, the first charging interface and third touching Electric area's connection, the first charging interface and the 4th electric shock area connection；Second charging interface and first are touched into a connection, the second charging Interface and second touches a connection, and the second charging interface and third touch a connection, and the second charging interface and the 4th touches a company It connects.Storage assembly is fixed in the memory block of bearing assembly again, the firm face of the second of bearing assembly and the first firm face are fixed Connection.Then it can charge for unmanned plane.To reach can reduce unmanned plane charge maintenance needed for manpower and material resources, make Charging process is convenient；Improve the technical effect of the working efficiency of unmanned plane.

In order to elaborate to a kind of energy supply airplane parking area mechanism for unmanned plane provided by the invention, to support to invent Technical problem to be solved, in the following, being done in detail to the charging unit for unmanned plane first in embodiment provided by the invention Illustrate, then during narration is used for the charging unit of unmanned plane, further targetedly draws provided by the invention A kind of energy supply airplane parking area mechanism for unmanned plane is complete, clear, clear to achieve the purpose that.

Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on Embodiment in the present invention, those of ordinary skill in the art's every other embodiment obtained belong to what the present invention protected Range；Wherein "and/or" keyword involved in this implementation, indicate and or two kinds of situations, in other words, the present invention implement A and/or B mentioned by example, illustrate two kinds of A and B, A or B situations, describe three kinds of states present in A and B, such as A and/or B, indicate: only including A does not include B；Only including B does not include A；Including A and B.Meanwhile in the embodiment of the present invention, when component is claimed For " being fixed on " another component, it can be directly on another component or there may also be components placed in the middle.When a group Part is considered as " connection " another component, it can be directly to another component or may be simultaneously present placed in the middle group Part.When a component is considered as " being set to " another component, it, which can be, is set up directly on another component or can Component placed in the middle can be existed simultaneously.Term "vertical", "horizontal", "left" and "right" used in the embodiment of the present invention and Similar statement is merely for purposes of illustration, and is not intended to the limitation present invention.

It is right first in order to which a kind of charging unit for unmanned plane provided in an embodiment of the present invention is described in detail Technical term involved in the embodiment of the present invention does description below explanation:

Detachable connection, which can be, to be bolted or is bonded；It is fixedly connected and can be welding or integrated molding；Ground Face can be unmanned plane it is parked when ground；It takes off and can be the process that unmanned plane reaches aerial rising from ground；Landing It can be process of the unmanned plane from airborne to ground.

Referring to Figure 1, Fig. 1 is that a kind of overall structure of charging unit for unmanned plane provided in an embodiment of the present invention is shown It is intended to.A kind of charging unit for unmanned plane provided in an embodiment of the present invention includes the first airplane parking area 1000, the second airplane parking area 2000, landing gear 3000 and energy supply component 4000.Now to the first airplane parking area 1000, the second airplane parking area 2000,3000 and of landing gear Energy supply component 4000 carries out following detailed description respectively:

For the first airplane parking area 1000:

First airplane parking area 1000 may include the first ducted body 1100, the first guide rail 1200, the second guide rail 1203, first watch Take motor 1300, the first screw rod, the first pedestal 1500, the first support arm 1600, the second support arm 1603, first electrode bar 1700, first electrode plate 1800 and control unit 1900.

First side 1101, second side 1102, third side 1103, the 4th side has can be set in first ducted body 1100 Face 1104, the first bottom surface 1105 and the first opening face 1106 are provided with first interface 1107, second interface in first side 1101 1108 and first through hole 1109, first interface 1107 and second interface 1108 it is symmetrical relative to first through hole 1109；Second Third interface 1110, the 4th interface 1111 and first node 1112 are provided on side 1102, third interface 1110 and the 4th connects Mouth 1111 is symmetrical relative to first node 1112.Wherein, first side 1101 and second side 1102 can be two phases The face of opposition, third side 1103 and the 4th side 1104 can be two opposed faces, and the first bottom surface 1105 and first open Mouth face 1106 can be two opposed faces.

The first fastening end 1201 and the second fastening end 1202,1201 He of the first fastening end has can be set in first guide rail 1200 First interface 1107 can be fixedly connected, and the second fastening end 1202 can be fixedly connected with third interface 1110；First fastening end 1201 and second fastening end 1202 can be the first guide rail 1200 opposition both ends.It is tight that third has can be set in second guide rail 1203 Fixed end 1204 and the 4th fastening end 1205, third fastening end 1204 can be fixedly connected with second interface 1108, the 4th fastening end 1205 can be fixedly connected with the 4th interface 1111；Third fastening end 1204 and the 4th fastening end 1205 can be the second guide rail The both ends of 1203 opposition.

First servo motor 1300 may include the first noumenon 1301 and first rotating shaft, the first noumenon 1301 and first side 1101 can be fixedly connected, and first rotating shaft can pass through first through hole 1109.

First screw rod may include the first screw rod 1401 and the first sliding block 1402, and one end of the first screw rod 1401 can be with One shaft is fixedly connected, and the other end of the first screw rod 1401 can be fixedly connected with the first node 1112；First sliding block 1402 can be set in the outside of the first screw rod 1401, and the first screw rod 1401 and first side 1101 can be mutually perpendicular to, and First screw rod 1401 and second side 1102 can be mutually perpendicular to.

First movement end 1501, the second mobile terminal 1502 and the first conformable region 1503 has can be set in first pedestal 1500, First movement end 1501 is provided with the first slot 1504 and the first spacing zone 1505, and the first guide rail 1200 passes through the first slot 1504, and the first slot 1504 can be between the first fastening end 1201 and the second fastening end 1202；Second mobile terminal 1502 can be set the second slot 1506 and the second spacing zone 1507, and the second guide rail 1203 can pass through the second slot 1506, And the second slot 1506 can be between third fastening end 1204 and the 4th fastening end 1205；First movement end 1501 can be with It is symmetrical relative to the first conformable region 1503 with the second mobile terminal 1502；First movement end 1501 can be located at first electrode plate 1800 and first between bottom surface 1105, and the second mobile terminal 1502 can be located at first electrode plate 1800 and first bottom surface Between 1105；First sliding block 1402 can be fixed on the first conformable region 1503.

The first support end 1601 and the second support end 1602, the first support end 1601 has can be set in first support arm 1600 It can be hinged with the first spacing zone 1505.Third support end 1604 and the 4th support end has can be set in second support arm 1603 1605, the third support end 1604 and second spacing zone 1507 are hinged.

The first locking end 1701 and the second locking end 1702, the first locking end 1701 has can be set in first electrode bar 1700 It can be fixedly connected with the second support end 1602, the second locking end 1702 can be fixedly connected with the 4th support end 1605.First Electrode plate 1800 and the first opening face 1106 are detachably connected, and first electrode plate 1800 can be located at the first support end 1601 Between third support end 1604.

Control unit 1900 and the first noumenon 1301 connect, and first through hole 1109 can be located at 1301 He of the first noumenon It controls between box.Control unit 1900 can be set the first delivery outlet, the second delivery outlet, third delivery outlet, the 4th delivery outlet, 5th delivery outlet, the 6th delivery outlet, the 7th delivery outlet and the 8th delivery outlet.First delivery outlet can be with first servo motor 1300 The connection of the first input port, the second delivery outlet can connect with the second input port of first electrode plate 1800, and third delivery outlet can To connect with the third delivery outlet of first electrode bar 1700, the 4th delivery outlet can be with the 4th input of the second servo motor 2300 Mouth connection, the 5th delivery outlet can be connected with the 5th input port of second electrode plate 2800, and the 6th delivery outlet can be with the second electricity 6th input port of pole bar 2701 connects, and the 7th delivery outlet can be connected with the 7th input port of the first detector 5000, and the 8th Delivery outlet can be connected with the 8th input port of the second detector 5100.

First airplane parking area 1000 can also include the first foot pad and the second foot pad.First bottom surface 1105 can be set first Corner region and the second corner region, the first foot pad are fixed on the first corner region, and the second foot pad is fixed on the second corner region.Wherein, One corner region can be located between the first foot pad and the first opening face 1106, and the second corner region can be located at the second foot pad and first Between opening face 1106.First airplane parking area 1000 can also include the first detector 5000 and the second detector 5100.First opens Mouthful face 1106 can be set the first detection zone and the second detection zone, and the first detector 5000 is fixed on the first detection zone, and second Detector 5100 is fixed on the second detection zone.Wherein, the first detection zone can be located at the first detector 5000 and the first bottom surface Between 1105, the second detection zone can be between the second detector 5100 and the first bottom surface 1105.First airplane parking area 1000 is also It may include the first guiding groove and the second guiding groove.First guiding groove can be detachably connected with first electrode plate 1800, and First guiding groove can be detachably connected with third side 1103；First guiding groove can be located at the first support end 1601 and second Between support end 1602.Second guiding groove can be detachably connected with first electrode plate 1800, and the first guiding groove can be with 4th side 1104 is detachably connected.Second guiding groove can be between third support end 1604 and the 4th support end 1605. Wherein, first electrode plate 1800 can be cathode, and first electrode bar 1700 can be anode.

Referring to Figure 1 and Fig. 4, Fig. 1 be a kind of charging unit for unmanned plane provided in an embodiment of the present invention entirety Structural schematic diagram, Fig. 4 are that the embodiment of the present invention provides a kind of the first airplane parking area structural representation of charging unit for unmanned plane Figure.First side 1101, second side 1102, third side 1103, the 4th side 1104, the first bottom surface 1105 and the first opening Face 1106 can surround the external shell to form the first airplane parking area 1000.First ducted body 1100 can be used for installing the first guide rail 1200, the second guide rail 1203, the first screw rod and the first pedestal 1500.

First guide rail 1200 can be rendered as cylinder.It first fastening end 1201 of the first guide rail 1200 can be with the first side First interface 1107 on face 1101 is fixedly connected, and the second fastening end 1202 of the first guide rail 1200 can be with second side 1102 On third interface 1110 be fixedly connected, the first guide rail 1200 is supported by first interface 1107 and third interface 1110 respectively, is made First guide rail 1200 is fixed between first side 1101 and second side 1102.First side 1101 and second side 1102 can To be parallel to each other, the first guide rail 1200 can be mutually perpendicular to first side 1101, meanwhile, the first guide rail 1200 can be with second Side 1102 is mutually perpendicular to.The spacing of first guide rail 1200 and the first bottom surface 1105 can be greater than first movement end 1501 and the The spacing of one bottom surface 1105 move freely the first slot 1504 in first movement end 1501 can on the first guide rail 1200.

Second guide rail 1203 can be rendered as cylinder.It the third fastening end 1204 of second guide rail 1203 can be with the first side Second interface 1108 on face 1101 is fixedly connected, and the 4th fastening end 1205 of the second guide rail 1203 can be with second side 1102 On the 4th interface 1111 be fixedly connected, the second guide rail 1203 is supported by second interface 1108 and the 4th interface 1111 respectively, is made Second guide rail 1203 is fixed between first side 1101 and second side 1102.First side 1101 and second side 1102 can To be parallel to each other, the second guide rail 1203 can be mutually perpendicular to first side 1101, meanwhile, the second guide rail 1203 can be with second Side 1102 is mutually perpendicular to.The spacing of second guide rail 1203 and the first bottom surface 1105 can be greater than the second mobile terminal 1502 and the The spacing of one bottom surface 1105 move freely the second slot 1506 in the second mobile terminal 1502 can on the second guide rail 1203.

First guide rail 1200 passes through first slot 1504 at first movement end 1501 in the first pedestal 1500, the second guide rail 1203 pass through the second slot 1506 of the second mobile terminal 1502 in the first pedestal 1500, allow the first pedestal 1500 along the The direction of both ends of one guide rail 1200 mobile (such as towards the direction of the first fastening end 1201) or the first pedestal 1500 can be along The direction of both ends of second guide rail 1203 is mobile (such as towards the direction of third fastening end 1204).

First support end 1601 of the first support arm 1600 can be with of first movement end 1501 in the first pedestal 1500 One spacing zone 1505 is hinged, it can using the contact point of the first support end 1601 and the first spacing zone 1505 as fulcrum, first Support end 1601 towards the first bottom surface 1105 direction, or it is mobile away from the direction of the first bottom surface 1105.

First locking end 1701 of first electrode bar 1700 can be solid with the second support end 1602 of the first support arm 1600 Second locking end 1702 of fixed connection, first electrode bar 1700 can be fixed with the 4th support end 1605 of the second support arm 1603 Connection.First support end 1601 and the second support end 1602 can fix first electrode bar 1700, make 1700 He of first electrode bar First electrode plate 1800 is parallel to each other.Second of first locking end 1701 of first electrode bar 1700 and the first support arm 1600 Support can be mutually insulated between end 1602, to prevent the first support arm 1600 also conductive, then avoid jeopardizing equipment and behaviour Make the safety of personnel.4th support end 1605 of the second locking end 1702 of first electrode bar 1700 and the second support arm 1603 it Between be also possible to mutually insulated, to prevent the second support arm 1603 also conductive, then avoid jeopardizing equipment and operator Safety.

Continuing with being a kind of charging unit for unmanned plane provided in an embodiment of the present invention referring to Fig. 1 and Fig. 4, Fig. 1 Overall structure diagram, Fig. 4 are that the embodiment of the present invention provides a kind of the first airplane parking area structure of charging unit for unmanned plane Schematic diagram.In order to the first support end 1601 to the first support arm 1600 can and the first pedestal 1500 in first movement end 1501 The first spacing zone 1505 be hinged and be explained in detail, following two embodiment is now provided and is described in detail:

The first embodiment.When the second support end 1602 drives first electrode bar 1700 progressively towards the first bottom surface 1105 Direction it is mobile when, the first support arm 1600 can be moved to the orthogonal position of first electrode plate 1800, this position is Position when being worked normally for the first support arm 1600.Meanwhile first support arm 1600 be moved to and 1800 phase of first electrode plate When mutually vertical, the first support end 1601 of the first support arm 1600 can be with 1505 phase of the first spacing zone at first movement end 1501 It is mutually fixed.

Second of embodiment.When the first support end 1601 drives first electrode bar 1700 progressively towards away from the first bottom surface When 1105 direction is mobile, the first support arm 1600 can be moved to the position being parallel to each other with first electrode plate 1800, this position Set position when folding as the first support arm 1600.When first support arm 1600 is in folding, the first support end can reduce Spatial volume occupied by 1601, to reach the technical effect of convenient transportation.

The third support end 1604 of second support arm 1603 can be with of the second mobile terminal 1502 in the first pedestal 1500 Two spacing zones 1507 are hinged, it can using the contact point of third support end 1604 and the second spacing zone 1507 as fulcrum, second Support end 1602 towards the first bottom surface 1105 direction, or it is mobile away from the direction of the first bottom surface 1105.

Continuing with being a kind of charging unit for unmanned plane provided in an embodiment of the present invention referring to Fig. 1 and Fig. 4, Fig. 1 Overall structure diagram, Fig. 4 are that the embodiment of the present invention provides a kind of the first airplane parking area structure of charging unit for unmanned plane Schematic diagram.In order to the third support end 1604 to the second support arm 1603 can and the first pedestal 1500 in the second mobile terminal 1502 The second spacing zone 1507 be hinged and be explained in detail, following two embodiment is now provided and is described in detail:

The first embodiment.When the 4th support end 1605 drives first electrode bar 1700 progressively towards the first bottom surface 1105 Direction it is mobile when, the second support arm 1603 can be moved to the orthogonal position of first electrode plate 1800, this position is Position when being worked normally for the second support arm 1603.Meanwhile second support arm 1603 be moved to and 1800 phase of first electrode plate When mutually vertical, the third support end 1604 of the second support arm 1603 can be with 1507 phase of the second spacing zone of the second mobile terminal 1502 It is mutually fixed.

Second of embodiment.When the 4th support end 1605 drives first electrode bar 1700 progressively towards away from the first bottom surface When 1105 direction is mobile, the second support arm 1603 can be moved to the position being parallel to each other with first electrode plate 1800, this position Set position when folding as the second support arm 1603.When second support arm 1603 is in folding, the second support end can reduce Spatial volume occupied by 1602, to reach the technical effect of convenient transportation.

The first noumenon 1301 of first servo motor 1300 can be fixedly connected with first side 1101, the first noumenon 1301 It can refer to the shell of first servo motor 1300 and the conducting wire of conveying electric current, shell is fixedly connected with first side 1101, So that first servo motor 1300 is fixed in the first side 1101 of the first airplane parking area 1000.Certainly, first servo motor 1300 can also be fixed on second side 1102 or third side 1103 etc..The first rotating shaft of first servo motor 1300 is worn It crosses after first through hole 1109, first rotating shaft can be fixedly connected with one end of the first screw rod 1401；First screw rod 1401 it is another One end can be fixedly connected with first node 1112.The first screw rod 1401 is set to be fixed on first side 1101 and second side 1102 Between, the first screw rod 1401 can be mutually perpendicular to first side 1101, and the first screw rod 1401 can also be with second side 1102 It is mutually perpendicular to.The first screw rod 1401, the first guide rail 1200 and the second guide rail 1203 can be made to be parallel to each other.

First sliding block 1402 can be set in the outside of the first screw rod 1401, i.e. settable and the first spiral shell on the first sliding block 1402 The hole that bar 1401 matches passes through the rotation of the first screw rod 1401, the first sliding block 1402 after so that the first screw rod 1401 is passed through the hole It can be on the first screw rod 1401 towards moving on the direction of first side 1101 or second side 1102.First sliding block 1402 can be consolidated It is scheduled on the first conformable region 1503 of the first pedestal 1500, such as by the outer surface of the first sliding block 1402 and the first conformable region 1503 It is fixedly connected.

Since the first guide rail 1200 passes through first slot 1504 at first movement end 1501 in the first pedestal 1500, second is led Rail 1203 passes through the second slot 1506 of the second mobile terminal 1502 in the first pedestal 1500, and the first sliding block 1402 is set in the first spiral shell The outside of bar 1401, and the first sliding block 1402 is fixed in the first pedestal 1500 on first conformable region 1503.Meanwhile first watches The first rotating shaft for taking motor 1300 is fixedly connected with one end of the first screw rod 1401.If first servo motor 1300 works, the The first rotating shaft of one servo motor 1300 will drive the first screw rod 1401 to rotate together, and the rotation of the first screw rod 1401 will be so that set The first sliding block 1402 being located on the first screw rod 1401 is mobile towards the direction of first side 1101 or second side 1102.

Continuing with being a kind of charging unit for unmanned plane provided in an embodiment of the present invention referring to Fig. 1 and Fig. 4, Fig. 1 Overall structure diagram, Fig. 4 are that the embodiment of the present invention provides a kind of the first airplane parking area structure of charging unit for unmanned plane Schematic diagram.In order to push first motor bar towards the side of first side 1101 or second side 1102 first servo motor 1300 It is described in detail to movement, following two embodiment is now provided and is explained in detail:

The first embodiment.When first servo motor 1300 works, the rotation of the first screw rod 1401 pushes the first sliding block 1402 is mobile towards the direction of second side 1102.Due to the first locking end 1701 of first electrode bar 1700 and the first support arm 1600 the second support end 1602 is fixedly connected, the second locking end 1702 of first electrode bar 1700 and the second support arm 1603 4th support end 1605 is fixedly connected.First support end 1601 of the first support arm 1600 and it is arranged in the first pedestal 1,500 the First spacing zone 1505 of one mobile terminal 1501 is fixedly connected with that (the first support arm 1600 and first electrode plate 1800 mutually hang down at this time Directly, the first support arm 1600 and the first spacing zone 1505 are mutually locked), it the third support end 1604 of the second support arm 1603 and sets The second spacing zone 1507 for setting second mobile terminal 1502 in the first pedestal 1500 is fixedly connected with (1603 He of the second support arm at this time First electrode plate 1800 is mutually perpendicular to, and the second support arm 1603 and the second spacing zone 1507 are mutually locked).First sliding block, 1402 court Second side 1102 direction it is mobile, the first pedestal 1500 will be driven mobile towards the direction of second side 1102, then band Dynamic first electrode bar 1700 is also mobile towards the direction of second side 1102.

Second of embodiment.When first servo motor 1300 works, the rotation of the first screw rod 1401 pushes the first sliding block 1402 is mobile towards the direction of first side 1101.Due to the first locking end 1701 of first electrode bar 1700 and the first support arm 1600 the second support end 1602 is fixedly connected, the second locking end 1702 of first electrode bar 1700 and the second support arm 1603 4th support end 1605 is fixedly connected.First support end 1601 of the first support arm 1600 and it is arranged in the first pedestal 1,500 the First spacing zone 1505 of one mobile terminal 1501 is fixedly connected with that (the first support arm 1600 and first electrode plate 1800 mutually hang down at this time Directly, the first support arm 1600 and the first spacing zone 1505 are mutually locked), it the third support end 1604 of the second support arm 1603 and sets The second spacing zone 1507 for setting second mobile terminal 1502 in the first pedestal 1500 is fixedly connected with (1603 He of the second support arm at this time First electrode plate 1800 is mutually perpendicular to, and the second support arm 1603 and the second spacing zone 1507 are mutually locked).First sliding block, 1402 court First side 1101 direction it is mobile, the first pedestal 1500 will be driven mobile towards the direction of first side 1101, then band Dynamic first electrode bar 1700 is also mobile towards the direction of first side 1101.

First electrode plate 1800 can be that be detachably connected, and first electrode plate 1800 can be with the first opening face 1106 Between the first support end 1601 and third support end 1604.Due to first electrode plate 1800 and first opening face 1106 be can Dismantling connection, so that when the first guide rail 1200 or the second guide rail 1203 that are located in the first ducted body 1100 or the first screw rod, Or first pedestal 1500 it is equal when damage, first electrode plate 1800 can mutually be separated with the first opening face 1106, with progress Maintenance then reaches the maintenance for facilitating equipment, reduces the technical effect of maintenance cost.The surrounding of first electrode plate 1800 and first The surrounding in opening face 1106 can be filled with insulating materials, this makes first electrode plate 1800 and the first opening face 1106 mutually absolutely Edge then reaches and electric current destruction had both been avoided to be located to prevent the electric current in first electrode plate 1800 from flowing through the first opening face 1106 Electronic device in first ducted body 1100 also eliminates the technical effect for leading to the security risk of operating personnel's electric shock.First electricity The making material of pole plate 1800 and first electrode bar 1700 can be copper, to make first electrode plate 1800 and first electrode bar 1700 have good conductive property, and first electrode plate 1800 and first electrode bar 1700 can also be enable in field severe Stable work in natural environment.

The first guiding groove, 1800 He of first electrode plate can be set between first electrode plate 1800 and third side 1103 The second guiding groove can be set between 4th side 1104.Second support end 1602 of the first support arm 1600 can stretch out 4th support end 1605 of one guiding groove, the second support arm 1603 can stretch out the second guiding groove.First support arm 1600 can be with Mobile towards the direction of first side 1101 or second side 1102 in the first guiding groove, the second support arm 1603 can also be It is mobile towards the direction of first side 1101 or second side 1102 in second guiding groove, then it is located at first electrode bar 1700 The top of first electrode plate 1800.First guiding groove can not only make the first support arm 1600 in the first guiding groove towards first Side 1101 or the direction of second side 1102 are mobile, can also be closed in time when the first support arm 1600 is mobile or static Gap in first guiding groove is then reduced extraneous rainwater, dust etc. and is entered in the first ducted body 1100, and corrosion first is hollow Hardware in body 1100 interferes the normal work of the electric elements in the first ducted body 1100.Second guiding groove not only may be used So that the second support arm 1603 is mobile towards the direction of first side 1101 or second side 1102 in the second guiding groove, may be used also To be closed the gap in the second guiding groove in time when the second support arm 1603 is mobile or static, then reduce extraneous rainwater, Dust etc. enters in the first ducted body 1100, corrodes the hardware in the first ducted body 1100, interferes the first ducted body 1100 The normal work of interior electric elements.

First foot pad can refer to two foots pad, and the first bottom surface 1105 can be rendered as rectangle, the first bottom surface 1105 First corner region can refer to positioned at two angles of the same side；Second foot pad, which can be, refers to two foots pad, and the first bottom surface 1105 can To be rendered as rectangle, the second corner region of the first bottom surface 1105 can refer to positioned at two angles of other the same side.I.e. first Corner region and the second corner region can be four angles on 1105 periphery of the first bottom surface.First foot pad and the second foot pad can be with rising-falling tones Section, since the first foot pad is fixed on the first corner region, the second foot pad is fixed on the second corner region, then passes through the first foot pad And/or second foot pad lift adjustment can make the first airplane parking area 1000 place it is more stable, then prevent due to the first bottom surface 1105 it is unstable, be abnormal sliding after causing unmanned plane to drop to the first electrode plate 1800 of the first airplane parking area 1000, very To unmanned plane is dropped to ground, unmanned plane is damaged, so that unmanned plane can not normally be charged.

Continuing with being a kind of charging unit for unmanned plane provided in an embodiment of the present invention referring to Fig. 1 and Fig. 4, Fig. 1 Overall structure diagram, Fig. 4 are that the embodiment of the present invention provides a kind of the first airplane parking area structure of charging unit for unmanned plane Schematic diagram.Control unit 1900 can be fixed in the first ducted body 1100, base station can provide for control unit 1900 The power supply of 220V.Control unit 1900 may include intelligent controller and charger, and intelligent controller can control charger Charging work state.Control unit 1900 can be with the first noumenon 1301 of first servo motor 1300, i.e. control unit 1900 It can be connected with the conducting wire of the first input port in first servo motor 1300, provide electric energy for first servo motor 1300, together When control first servo motor 1300 working condition (such as start and stop, revolving speed).Second delivery outlet of control unit 1900 can be with It is connected with the second input port of first electrode plate 1800,

Fig. 5 is referred to, Fig. 5 is that the embodiment of the present invention provides a kind of control unit 1900 of charging unit for unmanned plane Structural block diagram.Control unit 1900 may include intelligent controller and charger, and intelligent controller can be used to be reached by tall and handsome The TX1 development board of company's production；Charger can be charged using the customization produced by (Shenzhen) Co., Ltd of sky Creative Science and Technology Co. Ltd Device PC520.The third delivery outlet of control unit 1900 can be connected with the third delivery outlet of first electrode bar 1700, be the first electricity Pole bar 1700 provides electric energy, and first electrode bar 1700 can be anode.4th delivery outlet of control unit 1900 can be with second 4th input port of servo motor 2300 connects, and provides electric energy for first electrode plate 1800, first electrode plate 1800 can be negative Pole.First electrode plate 1800 can be anode；First electrode bar 1700 can be anode, and first electrode bar 1700 is also possible to bear Pole.If first electrode bar 1700 is anode, first electrode plate 1800 is cathode, then due to first electrode bar 1700 and extraneous contact Area be less than the area of first electrode plate 1800 and extraneous contact, can effectively prevent anode and extraneous hazard exposure (such as Anode and operator's contact), to reach the technical effect for improving safety.

5th delivery outlet of control unit 1900 can be connected with the 5th input port of second electrode plate 2800, be then Two electrode plates 2800 provide electric energy, and second electrode plate 2800 can be cathode.6th delivery outlet of control unit 1900 can be with 6th input port of second electrode bar 2701 connects, and then provides electric energy for second electrode bar 2701, second electrode plate 2800 can To be anode.7th delivery outlet of control unit 1900 can be connected with the 7th input port of the first detector 5000, then for First detector 5000 provides electric energy.8th delivery outlet of control unit 1900 can be with the 8th input of the second detector 5100 Mouth connection, then provides electric energy for the second detector 5100.

Continuing with the whole knot for referring to Fig. 1, Fig. 1 being a kind of charging unit for unmanned plane provided in an embodiment of the present invention Structure schematic diagram.In first side 1101, and/or, second side 1102, and/or, third side 1103, and/or, the 4th side Indicator light can be set on 1104.Such as indicator light can be installed in first side 1101, or in first side 1101 Indicator light is all installed on third side 1103.If installing indicator light in first side 1101, it assumes that the indicator light can be with Including A1, totally three display lamps, the indicator light can be connected with each other with control unit 1900 by A2, A3.When the charged amount of unmanned plane When accounting for 0%-the 20% of unmanned plane battery total capacity, A1 lamp is bright, and A2 and A3 extinguish；When the charged amount of unmanned plane accounts for unmanned electromechanics Pond total capacity 20% -60% when, A2 lamp is bright, and A1 and A3 extinguish；When the charged amount of unmanned plane accounts for unmanned plane battery total capacity When 60% -100%, A3 lamp is bright, and A1 and A2 extinguish.Alternatively, when the charged amount of unmanned plane accounts for unmanned plane battery total capacity When 0% -20%, A1 lamp is bright, and A2 and A3 extinguish；When the charged amount of unmanned plane accounts for 20%-the 60% of unmanned plane battery total capacity When, A1 and A2 lamp is bright, and A3 extinguishes；When the charged amount of unmanned plane accounts for 60%-the 100% of unmanned plane battery total capacity, A1, A2 It is all bright with A3 lamp.Then more intuitive charging situation can be provided for operator by the display state of indicator light, i.e., will Unmanned plane this moment charged amount the case where timely feedback reach to operator facilitate operator carry out charge maintenance technology Effect.

Continuing with the whole knot for referring to Fig. 1, Fig. 1 being a kind of charging unit for unmanned plane provided in an embodiment of the present invention Structure schematic diagram.First detector 5000 can be fixedly mounted on the first detection zone of the first airplane parking area 1000, third detection Device 5200 is fixedly mounted on the third detection zone of the second airplane parking area 2000, makes the first detector 5000 and third detector 5200 Match, the laser that the first detector 5000 emits such as is received by third detector 5200.By the fixed peace of the second detector 5100 On the second detection zone of the first airplane parking area 1000, the 4th detector 5300 is fixedly mounted on the 4th of the second airplane parking area 2000 On detection zone, the second detector 5100 and the 4th detector 5300 is made to match, such as receives second by the 4th detector 5300 and visit Survey the laser that device 5100 emits.On the first electrode plate 1800 that unmanned plane drops to the first airplane parking area 1000 and/or unmanned plane It drops on the second electrode plate 2800 of the second airplane parking area 2000, the laser letter of the first detector 5000 and third detector 5200 Number reception is interrupted because being hindered；The laser signal of second detector 5100 and the 4th detector 5300 receive also can because by It hinders and interrupts.When the first detector 5000 and third detector 5200 and the second detector 5100 and the 4th detector 5300, while when interrupt signal received time reaches 30S, (is also possible to 50s, 60s etc., to prevent due to falling leaves first Unmanned plane landing is mistaken on airplane parking area 1000 and/or the second airplane parking area 2000), control unit 1900 can control first and watch Motor 1300 and the work of the second servo motor 2300 are taken, keeps first electrode bar 1700 mobile towards the direction of second side 1102, The direction of second electrode bar 2701 towards the 6th side 2102 is mobile, at this time first electrode bar 1700 and second electrode bar 2701 Relative motion can make first electrode bar 1700 and the first area 3102 of getting an electric shock be in contact, meanwhile, first electrode bar 1700 and the Three electric shock areas 3302 are in contact；Second electrode bar 2701 and the second electric shock area 3202 are in contact, meanwhile, 2701 He of second electrode bar 4th electric shock area 3402 is in contact.Then by first electrode bar 1700 and second electrode bar 2701, to connect the first electric shock area 3102, the second electric shock area 3202, electric shock area 3402 of third electric shock area the 3302, the 4th.Also, first electrode bar 1700 and the second electricity After pole bar 2701 clamps unmanned plane, first touch a little 3103 and third touch a little 3303, understand and be contacted with first electrode plate 1800；The Two touch and a little 3203 and the 4th touch a little 3403, can contact with second electrode plate 2800.Due to first electrode bar 1700 and second Electrode stem 2701 is positively charged, and first electrode plate 1800 and second electrode plate 2800 are negatively charged.First electric shock area 3102, second gets an electric shock Area 3202, third electric shock area 3302 and the 4th electric shock area 3402 connect the first charging interface of storage assembly；First touches a little 3103, second touch a little 3203, third touch a little 3303 and the 4th touch a little 3403 connection storage assemblies the second charging interface. At this point, control unit 1900 makes first electrode bar 1700, second electrode bar 2701, first electrode plate 1800 and second electrode plate After 2800 are powered, electric energy can be provided for storage assembly, to be the technical effect that charges of storage assembly of unmanned plane.

For the second airplane parking area 2000:

Second airplane parking area 2000 may include the second ducted body 2100, third guide rail 2200, the 4th guide rail 2201, second watch Take motor 2300, the second screw rod 2400, the second pedestal 2500, third support arm 2600, the 4th support arm 2601, second electrode bar 2701 and second electrode plate 2800.

The 5th side 2101, the 6th side 2102, heptalateral face 2103, the 8th side has can be set in second ducted body 2100 Face 2104, the second bottom surface 2105 and the second opening face 2106.The 5th interface the 2107, the 6th can be set on 5th side 2101 Interface 2108 and the second through-hole 2109, the 5th interface 2107 can symmetrically divide with the 6th interface 2108 relative to the second through-hole 2109 Cloth；The 7th interface 2111, the 8th interface 2112 and second node 2113, the 7th interface can be set on 6th side 2102 2111 can be symmetrical relative to second node 2113 with the 8th interface 2112.Wherein, the 6th side 2102 can be with second Side 1102 is detachably connected；5th side 2101 can be two opposed faces, heptalateral face with the 6th side 2102 2103 can be two opposed faces with the 8th side 2104, and the second bottom surface 2105 can be two with the second opening face 2106 Opposed face.

The 5th fastening end and the 6th fastening end has can be set in third guide rail 2200, and the 5th fastening end can be with the 5th interface 2107 are fixedly connected, and the 6th fastening end can be fixedly connected with the 7th interface 2111.Wherein, the 5th fastening end can be with the 6th tightly Fixed end is the both ends that third guide rail 2200 opposes.The 7th fastening end and the 8th fastening end has can be set in 4th guide rail 2201, the Seven fastening ends can be fixedly connected with the 6th interface 2108, and the 8th fastening end can be fixedly connected with the 8th interface 2112. Wherein, the 7th fastening end can be the both ends of the 4th guide rail 2201 opposition with the 8th fastening end.

Second servo motor 2300 may include the second ontology and the second shaft, and the second ontology can be with control unit 1900 It is fixedly connected, and the second shaft can pass through second through-hole 2109.Second screw rod 2400 may include the second screw rod and Second sliding block.One end of second screw rod can be fixedly connected with the second shaft, the other end of the second screw rod can and second node 2113 are fixedly connected.Wherein, the second sliding block can be set in the outside of the second screw rod, and the second screw rod can be with the 5th side 2101 Vertically, and the second screw rod can be vertical with the 6th side 2102.Third mobile terminal has can be set in second pedestal 2500 2501, the 4th mobile terminal 2502 and the second conformable region.Third slot and third spacing zone has can be set in third mobile terminal 2501, Third guide rail 2200 can pass through third slot, and third slot can be between the 5th fastening end and the 6th fastening end； The 4th slot and the 4th spacing zone has can be set in 4th mobile terminal 2502, and the 4th guide rail 2201 can pass through the 4th slot, and And the 4th slot can be between the 7th fastening end and the 8th fastening end.Wherein, third mobile terminal 2501 can be moved with the 4th Moved end 2502 is symmetrical relative to the second conformable region；Third mobile terminal 2501 can be located at second electrode plate 2800 and the second bottom Between face 2105, and the 4th mobile terminal 2502 can be between second electrode plate 2800 and the second bottom surface 2105；Second is sliding Block can be fixed on the second conformable region.

The 5th support end and the 6th support end has can be set in third support arm 2600, and the 5th support end can be limited with third The connection of position area.The 7th support end and the 8th support end, the 7th support end and the 4th limit has can be set in 4th support arm 2601 Area's connection.Third locking end and the 4th locking end, third locking end and the 6th support end has can be set in second electrode bar 2701 Connection, the 4th locking end can be connected with the 8th support end.Second electrode plate 2800 can be open face 2106 with second can Dismantling connection, and second electrode plate 2800 can be between the 5th support end and the 7th support end.Second airplane parking area 2000 It may include third foot pad and the 4th foot pad.Third corner region and the 4th corner region, third has can be set in second bottom surface 2105 Foot pad can be fixed on third corner region, and the 4th foot pad can be fixed on the 4th corner region.Wherein, third corner region can be located at Between third foot pad and the second opening face 2106, the 4th corner region can be located between the 4th foot pad and the second opening face 2106. Second airplane parking area 2000 may include third detector 5200 and the 4th detector 5300.Second opening face 2106 can be set Third detection zone and the 4th detection zone, third detector 5200 can be fixed on third detection zone, and the 4th detector 5300 can be with It is fixed on the 4th detection zone.Wherein, third detection zone can between third detector 5200 and the second bottom surface 2105, the 4th Detection zone can be between the 4th detector 5300 and the second bottom surface 2105.Second airplane parking area 2000 may include third guidance Slot and the 4th guide channel.Third guiding groove can be detachably connected with second electrode plate 2800, and third guiding groove can be with Heptalateral face 2103 is detachably connected；Third guiding groove can be between the 5th support end and the 6th support end.4th guidance Slot can be detachably connected with second electrode plate 2800, and the 4th guiding groove can be detachably connected with the 8th side 2104； 4th guiding groove can be between the 7th support end and the 8th support end.Wherein, second electrode plate 2800 can be cathode, the Two electrode stems 2701 can be anode.

Referring to Figure 1 and Fig. 3, Fig. 1 be a kind of charging unit for unmanned plane provided in an embodiment of the present invention entirety Structural schematic diagram, Fig. 3 are a kind of right view schematic diagrames of charging unit for unmanned plane provided in an embodiment of the present invention.Second 6th side 2102 of airplane parking area 2000 and the second side 1102 of the first airplane parking area 1000 can be and be detachably connected, such as It is fixed with nut in the second side 1102 of one airplane parking area 1000, is provided on the 6th side 2102 of the second airplane parking area 2000 Bolt makes the 6th side 2102 of two airplane parking areas and the second side 1102 of the first airplane parking area 1000 by the screw bolt and nut It is connected as one.When the second airplane parking area 2000 and the first airplane parking area 1000 are linked together, first electrode plate 1800 and the second electricity Pole plate 2800 can be in the same plane, and first electrode bar 1700 and second electrode bar 2701 can also be generally aligned in the same plane It is interior.At this point, the first guide channel and third guiding groove can be located along the same line, the second guide channel and the 4th guiding groove can also be with It is located along the same line.Second airplane parking area 2000 and the second opening face 2106 can be with the first opening faces of the first airplane parking area 1000 1106 sizes are identical, and shape is identical.The of face 2106 and the first airplane parking area 1000 can be open by the second of the second airplane parking area 2000 One opening face 1106 constitutes rectangular platform, and unmanned plane can land on the platform.

Third guide rail 2200 can be rendered as cylinder.It 5th fastening end of third guide rail 2200 can be with the 5th side The 5th interface 2107 on 2101 is fixedly connected, and the 6th fastening end of third guide rail 2200 can be on the 6th side 2102 Seven interfaces 2111 are fixedly connected, and are supported third guide rail 2200 respectively by the 5th interface 2107 and the 7th interface 2111, are led third Rail 2200 is fixed between the 5th side 2101 and the 6th side 2102.5th side 2101 and the 6th side 2102 can be mutual In parallel, third guide rail 2200 can be mutually perpendicular to the 5th side 2101, meanwhile, third guide rail 2200 can be with the 6th side 2102 are mutually perpendicular to.The spacing of third guide rail 2200 and the second bottom surface 2105 can be greater than third mobile terminal 2501 and the second bottom The spacing in face 2105 move freely third slot in third mobile terminal 2501 can on third guide rail 2200.

4th guide rail 2201 can be rendered as cylinder.It 7th fastening end of the 4th guide rail 2201 can be with the 5th side The 6th interface 2108 on 2101 is fixedly connected, and the 8th fastening end of the 4th guide rail 2201 can be on the 6th side 2102 Eight interfaces 2112 are fixedly connected, and are supported the 4th guide rail 2201 respectively by the 6th interface 2108 and the 8th interface 2112, are made the 4th to lead Rail 2201 is fixed between the 5th side 2101 and the 6th side 2102.5th side 2101 and the 6th side 2102 can be mutual In parallel, the 4th guide rail 2201 can be mutually perpendicular to the 5th side 2101, meanwhile, the 4th guide rail 2201 can be with the 6th side 2102 are mutually perpendicular to.The spacing of 4th guide rail 2201 and the second bottom surface 2105 can be greater than the 4th mobile terminal 2502 and the second bottom The spacing in face 2105 move freely the 4th slot in the 4th mobile terminal 2502 can on the 4th guide rail 2201.

Third guide rail 2200 passes through the third slot of third mobile terminal 2501 in the second pedestal 2500, and the 4th guide rail 2201 is worn The 4th slot for crossing the 4th mobile terminal 2502 in the second pedestal 2500 allows the second pedestal 2500 along third guide rail 2200 Direction of both ends mobile (such as the direction towards the 5th fastening end) or the second pedestal 2500 can be along the 4th guide rail 2201 Direction of both ends is mobile (such as towards the direction of the 7th fastening end).

5th support end of third support arm 2600 can be with the third limit of third mobile terminal 2501 in the second pedestal 2500 Position area is hinged, it can using the contact point of third support end 1604 and third spacing zone as fulcrum, the 5th support end is towards the The direction of two bottom surfaces 2105, or it is mobile away from the direction of the second bottom surface 2105.The third locking end of second electrode bar 2701 can To be fixedly connected with the 6th support end of third support arm 2600, the 4th locking end of second electrode bar 2701 can be with the 4th 8th support end of brace 2601 is fixedly connected.6th support end and the 8th support end can fix second electrode bar 2701, make Second electrode bar 2701 and second electrode plate 2800 are parallel to each other.The third locking end and third support arm of second electrode bar 2701 It can be mutually insulated between 2600 the 6th support end, to prevent third support arm 2600 also conductive, then avoid jeopardizing The safety of equipment and operator.8th support end of the 4th locking end of second electrode bar 2701 and the 4th support arm 2601 it Between be also possible to mutually insulated, to prevent the 4th support arm 2601 also conductive, then avoid jeopardizing equipment and operator Safety.

Continuing with being a kind of charging unit for unmanned plane provided in an embodiment of the present invention referring to Fig. 1 and Fig. 3, Fig. 1 Overall structure diagram, Fig. 3 are a kind of right view schematic diagrames of charging unit for unmanned plane provided in an embodiment of the present invention. In order to the 5th support end to third support arm 2600 can and the second pedestal 2500 in third mobile terminal 2501 third limit Area, which is hinged, to be explained in detail, and is now provided following two embodiment and is described in detail:

The first embodiment.When third support end 1604 drives second electrode bar 2701 progressively towards the second bottom surface 2105 Direction it is mobile when, third support arm 2600 can be moved into the orthogonal position of second electrode plate 2800, this position is Position when third support arm 2600 works normally (when charging for unmanned plane).Meanwhile third support arm 2600 is moved to and the When two electrode plates 2800 are mutually perpendicular to, the 5th support end of third support arm 2600 can be limited with the third of third mobile terminal 2501 Position area is fixed to each other.

Second of embodiment.When third support end 1604 drives second electrode bar 2701 progressively towards away from the second bottom surface When 2105 direction is mobile, third support arm 2600 can be moved to the position being parallel to each other with second electrode plate 2800, this position Set position when folding as third support arm 2600.When third support arm 2600 is in folding, third support end can reduce Spatial volume occupied by 1604, to reach the technical effect of convenient transportation.

7th support end of the 4th support arm 2601 can be with the 4th limit of the 4th mobile terminal 2502 in the second pedestal 2500 Position area is hinged, it can using the contact point of the 7th support end and the 4th spacing zone as fulcrum, the 7th support end is towards the second bottom The direction in face 2105, or it is mobile away from the direction of the second bottom surface 2105.

In order to the 7th support end to the 4th support arm 2601 can and the second pedestal 2500 in the 4th mobile terminal 2502 4th spacing zone, which is hinged, to be explained in detail, and is now provided following two embodiment and is described in detail:

The first embodiment.When the 7th support end drives second electrode bar 2701 progressively towards the side of the second bottom surface 2105 To it is mobile when, the 4th support arm 2601 can be moved to the orthogonal position of second electrode plate 2800, this position is the Position when four support arms 2601 work normally.Meanwhile the 4th support arm 2601 be moved to second electrode plate 2800 mutually hang down When straight, the 7th support end of the 4th support arm 2601 can be fixed to each other with the 4th spacing zone of the 4th mobile terminal 2502.

Second of embodiment.When the 7th support end drives second electrode bar 2701 progressively towards away from the second bottom surface 2105 Direction it is mobile when, the 4th support arm 2601 can be moved to the position being parallel to each other with second electrode plate 2800, this position is Position when being folded for the 4th support arm 2601.When 4th support arm 2601 is in folding, the 4th support end 1605 can reduce Occupied spatial volume, to reach the technical effect of convenient transportation.

Second ontology of the second servo motor 2300 can be fixedly connected with the 5th side 2101, and the second ontology can refer to The shell of second servo motor 2300 and the conducting wire of conveying electric current, shell and the 5th side 2101 are fixedly connected, so that second Servo motor 2300 is fixed on the 5th side 2101 of the second airplane parking area 2000.Certainly, the second servo motor 2300 can also be with Be fixed on heptalateral face 2103 or the 8th side 2104 etc..Second shaft of the second servo motor 2300 passes through the second through-hole After 2109, the second shaft can be fixedly connected with one end of the second screw rod；The other end of second screw rod can and second node 2113 are fixedly connected.It is fixed on the second screw rod between the 5th side 2101 and the 6th side 2102, the second screw rod can be with Five sides 2101 are mutually perpendicular to, and the second screw rod can also be mutually perpendicular to the 6th side 2102.It can make the second screw rod, third Guide rail 2200 and the 4th guide rail 2201 are parallel to each other.

Second sliding block can be set in the outside of the second screw rod, i.e. can be set on the second sliding block and match with the second screw rod Hole so that after the second screw rod passes through the hole, by the rotation of the second screw rod, the second sliding block can be on the second screw rod towards the It is moved on the direction of five sides 2101 or the 6th side 2102.Second sliding block can be fixed on the second fitting of the second pedestal 2500 Qu Shang, such as the outer surface of the second sliding block is fixedly connected with the second conformable region.

Since third guide rail 2200 passes through the third slot of third mobile terminal 2501 in the second pedestal 2500, the 4th guide rail 2201 pass through the 4th slot of the 4th mobile terminal 2502 in the second pedestal 2500, and the second sliding block is set in the outside of the second screw rod, And the second sliding block is fixed in the second pedestal 2500 on second conformable region.Meanwhile second servo motor 2300 the second shaft It is fixedly connected with one end of the second screw rod.If the second servo motor 2300 works, the second shaft of the second servo motor 2300 The second screw rod will be driven to rotate together, the rotation of the second screw rod will make the second sliding block being set on the second screw rod towards the 5th The direction of side 2101 or the 6th side 2102 is mobile.

Continuing with being a kind of charging unit for unmanned plane provided in an embodiment of the present invention referring to Fig. 1 and Fig. 3, Fig. 1 Overall structure diagram, Fig. 3 are a kind of right view schematic diagrames of charging unit for unmanned plane provided in an embodiment of the present invention. In order to push the second motor bar mobile towards the direction of the 5th side 2101 or the 6th side 2,102 second servo motor 2300 It is described in detail, following two embodiment is now provided and is explained in detail:

The first embodiment.When second servo motor 2300 works, the rotation of the second screw rod push the second sliding block towards The direction of 5th side 2101 is mobile.Due to second electrode bar 2701 the first locking end 1701 and third support arm 2600 Six support ends are fixedly connected, the 4th locking end of second electrode bar 2701 and the fixed company of the 8th support end of the 4th support arm 2601 It connects.5th support end of third support arm 2600 and the third spacing zone that third mobile terminal 2501 in the second pedestal 2500 is set Be fixedly connected (third support arm 2600 and second electrode plate 2800 are mutually perpendicular at this time, third support arm 2600 and third limit Area is mutually locked), the 7th support end of the 4th support arm 2601 and the 4th mobile terminal 2502 in the second pedestal 2500 is set 4th spacing zone is fixedly connected with that (the 4th support arm 2601 and second electrode plate 2800 are mutually perpendicular at this time, the 4th support arm 2601 It is mutually locked with the 4th spacing zone).The direction of second sliding block towards the 5th side 2101 is mobile, will drive 2500 court of the second pedestal The 5th side 2101 direction it is mobile, then drive second electrode bar 2701 also mobile towards the direction of the 5th side 2101.

Second of embodiment.When second servo motor 2300 works, the rotation of the second screw rod push the second sliding block towards The direction of 6th side 2102 is mobile.Due to second electrode bar 2701 the first locking end 1701 and third support arm 2600 Six support ends are fixedly connected, the 4th locking end of second electrode bar 2701 and the fixed company of the 8th support end of the 4th support arm 2601 It connects.5th support end of third support arm 2600 and the third spacing zone that third mobile terminal 2501 in the second pedestal 2500 is set Be fixedly connected (third support arm 2600 and second electrode plate 2800 are mutually perpendicular at this time, third support arm 2600 and third limit Area is mutually locked), the 7th support end of the 4th support arm 2601 and the 4th mobile terminal 2502 in the second pedestal 2500 is set 4th spacing zone is fixedly connected with that (the 4th support arm 2601 and second electrode plate 2800 are mutually perpendicular at this time, the 4th support arm 2601 It is mutually locked with the 4th spacing zone).The direction of second sliding block towards the 6th side 2102 is mobile, will drive 2500 court of the second pedestal The 6th side 2102 direction it is mobile, then drive second electrode bar 2701 also mobile towards the direction of the 6th side 2102.

Second electrode plate 2800 can be that be detachably connected, and second electrode plate 2800 can be with the second opening face 2106 Between the 5th support end and the 7th support end.Since second electrode plate 2800 and the second opening face 2106 are detachably to connect It connects, so that when the third guide rail 2200 or the 4th guide rail 2201 that are located in the second ducted body 2100 or the second screw rod 2400, or When second pedestal 2500 etc. damages, second electrode plate 2800 can mutually be separated with the second opening face 2106, to be tieed up It repairs, then reaches the maintenance for facilitating equipment, reduce the technical effect of maintenance cost.The surrounding of second electrode plate 2800 and second is opened The surrounding in mouth face 2106 can be filled with insulating materials, this makes second electrode plate 2800 and the second opening face 2106 mutually absolutely Edge then reaches and electric current destruction had both been avoided to be located to prevent the electric current in second electrode plate 2800 from flowing through the second opening face 2106 Electronic device in second ducted body 2100 also eliminates the technical effect for leading to the security risk of operating personnel's electric shock.Second electricity The making material of pole plate 2800 and second electrode bar 2701 can be copper, to make second electrode plate 2800 and second electrode bar 2701 have good conductive property, and second electrode plate 2800 and second electrode bar 2701 can also be enable in field severe Stable work in natural environment.

Third guiding groove, 2800 He of second electrode plate can be set between second electrode plate 2800 and heptalateral face 2103 The 4th guiding groove can be set between 8th side 2104.6th support end of third support arm 2600 can stretch out second and draw 8th support end of guide groove, the 4th support arm 2601 can stretch out the 4th guiding groove.Third support arm 2600 can draw in third Mobile towards the direction of the 5th side 2101 or the 6th side 2102 in guide groove, the 4th support arm 2601 can also be in the 4th guidance It is mobile towards the direction of the 5th side 2101 or the 6th side 2102 in slot, so that second electrode bar 2701 is located at second electrode The top of plate 2800.Third guiding groove can not only make third support arm 2600 in third guiding groove towards the 5th side 2101 Or the 6th side 2102 direction it is mobile, third guidance can also be closed in time when third support arm 2600 is mobile or static Gap in slot is then reduced extraneous rainwater, dust etc. and is entered in the second ducted body 2100, corrodes in the second ducted body 2100 Hardware, interfere the second ducted body 2100 in electric elements normal work.4th guiding groove can not only make the 4th Support arm 2601 is mobile towards the direction of the 5th side 2101 or the 6th side 2102 in the 4th guiding groove, can also be the 4th When support arm 2601 is mobile or static, be closed the gap in the 4th guiding groove in time, then reduce extraneous rainwater, dust etc. into Enter in the second ducted body 2100, corrode the hardware in the second ducted body 2100, interferes the electric appliance in the second ducted body 2100 The normal work of element.

Third foot pad can refer to two foots pad, and the second bottom surface 2105 can be rendered as rectangle, the second bottom surface 2105 Third corner region can refer to positioned at two angles of the same side；4th foot pad can refer to two foots pad, and the second bottom surface 2105 can To be rendered as rectangle, the 4th corner region of the second bottom surface 2105 can refer to positioned at two angles of other the same side.That is third Corner region and the 4th corner region can be four angles on 2105 periphery of the second bottom surface.Third foot pad and the 4th foot pad can be with rising-falling tones Section, since the first foot pad is fixed on the first corner region, the second foot pad is fixed on the second corner region, and third foot pad is fixed on the On three corner regions, the 4th foot pad is fixed on the 4th corner region, then by the first foot pad, and/or, the second foot pad, and/or, the Three foots pad, and/or, the lift adjustment of the 4th foot pad can make the second airplane parking area 2000 place it is more stable, then prevent due to Second bottom surface 2105 it is unstable, be abnormal after causing unmanned plane to drop to the second electrode plate 2800 of the second airplane parking area 2000 Sliding, or even drop unmanned plane to ground, unmanned plane is damaged, so that unmanned plane can not normally be charged.

In the 5th side 2101, and/or, the 6th side 2102, and/or, heptalateral face 2103, and/or, the 8th side Indicator light can be set on 2104.Such as indicator light can be installed on the 5th side 2101, or in the 5th side 2101 Indicator light is all installed on heptalateral face 2103.If installing indicator light on the 5th side 2101, it assumes that the indicator light can be with Including B1, totally three display lamps, the indicator light can be connected with each other with control unit 1900 by B2, B3.When the charged amount of unmanned plane When accounting for 0%-the 20% of unmanned plane battery total capacity, B1 lamp is bright, and B2 and B3 extinguish；When the charged amount of unmanned plane accounts for unmanned electromechanics Pond total capacity 20% -60% when, B2 lamp is bright, and B1 and B3 extinguish；When the charged amount of unmanned plane accounts for unmanned plane battery total capacity When 60% -100%, B3 lamp is bright, and B1 and B2 extinguish.Alternatively, when the charged amount of unmanned plane accounts for unmanned plane battery total capacity When 0% -20%, B1 lamp is bright, and B2 and B3 extinguish；When the charged amount of unmanned plane accounts for 20%-the 60% of unmanned plane battery total capacity When, B1 and B2 lamp is bright, and B3 extinguishes；When the charged amount of unmanned plane accounts for 60%-the 100% of unmanned plane battery total capacity, B1, B2 It is all bright with B3 lamp.Then more intuitive charging situation can be provided for operator by the display state of indicator light, i.e., will Unmanned plane this moment charged amount the case where timely feedback reach to operator facilitate operator carry out charge maintenance technology Effect.

Third detector 5200 can be fixedly mounted on the third detection zone of the second airplane parking area 2000, make the first detection Device 5000 and third detector 5200 match, and such as receive the laser that the first detector 5000 emits by third detector 5200. 4th detector 5300 is fixedly mounted on the 4th detection zone of the second airplane parking area 2000, makes the second detector 5100 and the 4th Detector 5300 matches, and such as receives the laser that the second detector 5100 emits by the 4th detector 5300.When unmanned plane lands On the second electrode plate 2800 of the second airplane parking area 2000 and/or unmanned plane drops to the first electrode of the first airplane parking area 1000 On plate 1800, the laser signal reception of the first detector 5000 and third detector 5200 is interrupted because being hindered；Second visits The laser signal reception for surveying device 5100 and the 4th detector 5300 can also be interrupted because being hindered.When 5000 He of the first detector Third detector 5200 and the second detector 5100 and the 4th detector 5300, while the interrupt signal received time reaches When 30S, control unit 1900 can control the second servo motor 2300 and first servo motor 1300 works, and make second electrode bar 2701 move towards the direction of the 6th side 2102, and first electrode bar 1700 is mobile towards the direction of second side 1102, at this time The relative motion of first electrode bar 1700 and second electrode bar 2701 can make first electrode bar 1700 and the first electric shock area 3102 are in contact, meanwhile, first electrode bar 1700 and third electric shock area 3302 are in contact；Second electrode bar 2701 and the second electric shock Area 3202 is in contact, meanwhile, second electrode bar 2701 and the 4th electric shock area 3402 are in contact.Then by 1700 He of first electrode bar Second electrode bar 2701, to connect electric shock area 3202 of the first electric shock area 3102, second, electric shock area of third electric shock area the 3302, the 4th 3402.Also, after first electrode bar 1700 and second electrode bar 2701 clamp unmanned plane, first touch a little 3103 and third touch Point 3303 can be contacted with first electrode plate 1800；Second touches and a little 3203 and the 4th touches a little 3403, can and second electrode plate 2800 contacts.Since first electrode bar 1700 and second electrode bar 2701 are positively charged, first electrode plate 1800 and second electrode plate 2800 is negatively charged.First electric shock area 3202 of electric shock area 3102, second, third electric shock area 3302 and the 4th electric shock area 3402 connection store First charging interface of electrical component；First touch a little 3103, second touch a little 3203, third touches and a little 3303 and the 4th touches a little Second charging interface of 3403 connection storage assemblies.At this point, control unit 1900 makes first electrode bar 1700, second electrode bar 2701, after first electrode plate 1800 and second electrode plate 2800 are powered, electric energy can be provided for storage assembly, to be reached for nothing The technical effect that man-machine storage assembly charges.

For landing gear 3000:

Landing gear 3000 may include the first foot prop 3100, the second foot prop, third foot prop 3300, the 4th foot prop 3400 and branch Seat 3500.First foot prop 3100 can be set the first clamping joint 3101, first electric shock area 3102 and first and touch a little 3103, the One electric shock area 3102 can be located at the first clamping joint 3101 and first and touch a little between 3103.Wherein, the first electric shock area 3102 can To connect with first electrode bar 1700, first touches and 3103 can a little connect with first electrode plate 1800；First electric shock area 3102 It can phase at a distance from the distance that a little 3103 can be touched with first, with first electrode bar 1700 and the first electrode plate 1800 Deng.

Second foot prop can be set the second clamping joint 3201, second electric shock area 3202 and second and touch a little 3203.Second Electric shock area 3202 can be located at the second clamping joint 3201 and second and touch a little between 3203；Wherein, the second electric shock area 3202 can be with It is connected with second electrode bar 2701, second touches and 3203 can a little connect with first electrode plate 1800；Second electric shock area 3202 can To touch a little 3203 distance with second, with being equidistant for first electrode bar 1700 and first electrode plate 1800.

Third foot prop 3300 can be set third clamping joint 3301, third electric shock area 3302 and third and touch a little 3303. Third electric shock area 3302 can be located at third clamping joint 3301 and third and touch a little between 3303.Wherein, third electric shock area 3302 It can be connected with second electrode bar 2701, third is touched 3303 can a little connect with second electrode plate 2800；Third electric shock area 3302 can touch a little 3303 distance with third, with being equidistant for second electrode bar 2701 and second electrode plate 2800.

4th foot prop 3400 can be set the 4th clamping joint the 3401, the 4th electric shock area 3402 and the 4th and touch a little 3403. 4th electric shock area 3402 can be located at the 4th clamping joint 3401 and the 4th and touch a little between 3403.Wherein, the 4th electric shock area 3402 It can be connected with second electrode bar 2701, the 4th touches and 3403 can a little connect with second electrode plate 2800；4th electric shock area 3402 can touch a little 3403 distance with the 4th, with being equidistant for second electrode bar 2701 and second electrode plate 2800.Its In, first touch a little 3103 and third touch a little 3303 distance, with second touch a little 3203 and the 4th touch a little 3403 away from From equal.

It is steady that the first clamping groove, the second clamping groove, third clamping groove, the 4th clamping groove and first has can be set in support 3500 Gu face.First clamping groove can be connected with the first clamping joint 3101, and the second clamping groove can be connected with the second clamping joint 3201, the Three clamping grooves can be connected with third clamping joint 3301, and the 4th clamping groove can be connected with the 4th clamping joint 3401；First electric shock Area 3102 and the 4th electric shock area 3402 are distributed relative to the central symmetry of support 3500；Second electric shock area 3202 and third electric shock area 3302 can be distributed relative to the central symmetry of the support 3500.

Continuing with referring to figure 1, figure 2 and figure 3, Fig. 1 is that a kind of charging for unmanned plane provided in an embodiment of the present invention fills The overall structure diagram set, Fig. 2 are a kind of left view diagrams of charging unit for unmanned plane provided in an embodiment of the present invention It is intended to, Fig. 3 is a kind of right view schematic diagram of charging unit for unmanned plane provided in an embodiment of the present invention.Support 3500 can Be present be square, rectangle etc..The center of support 3500, which can be, criticizes rectangular geometric center or rectangular several What center.The firm face of the first of support 3500 can be fixedly connected with the second firm face of bearing assembly 4200, the second firm face It can refer to the bottom of unmanned plane, i.e., support 3500 is mounted on to the bottom of unmanned plane.On support 3500 and the first firm face The first clamping groove, the second clamping groove, third clamping groove and the can be set on the face (close to a face on ground) being away from each other Four clamping grooves, the first clamping groove can be fixedly connected with the first clamping joint 3101 of the first foot prop 3100, and the second clamping groove can be with It is fixedly connected with the second clamping joint 3201 of the second foot prop, third clamping groove can be with the third clamping joint of third foot prop 3300 3301 are fixedly connected, and the 4th clamping groove can be fixedly connected with the 4th clamping joint 3401 of the 4th foot prop 3400, then at nobody It, can be by the first foot prop 3100, the second foot prop, when machine is dropped on the first airplane parking area 1000 and/or the second airplane parking area 2000 Tripod 3300 and the 4th foot prop 3400 provide support force for unmanned plane, and unmanned plane is made to be stably placed at the first airplane parking area 1000 And/or second on airplane parking area 2000.

After unmanned plane is parked on the first airplane parking area 1000 and/or the second airplane parking area 2000, pass through first electrode bar 1700 and second electrode bar 2701 relative movement, the first of the first foot prop 3100 can be made to touch a little 3103 and first electrode Plate 1800 connects, and the second of the second foot prop touches a little 3203 and the connection of second electrode plate 2800, and the third of third foot prop 3300 touches Contact 3303 and first electrode plate 1800 connect, and the 4th of the 4th foot prop 3400 touches a little 3403 can be with first electrode plate 1800 Connection；Meanwhile first electric shock area 3102, third electric shock area 3302 all with first electrode bar 1700 connect, second electric shock area 3202, 4th electric shock area 3402 is all connected with second electrode bar 2701.

First touch a little 3103, second touch a little 3203, third touches and a little 3303 and the 4th touches and 3403 can a little use Metal material is made, such as is all copper material, can be conducive to first electrode plate 1800 and/or second electrode plate in this way 2800, good conduction is carried out with the storage assembly of unmanned plane.It can be by the first conduction.First touch a little 3103 and third touch The distance of point 3303 touches with second and a little 3203 and the 4th touches and a little 3403 be equidistant, can make first touch a little 3103, second touch a little 3203, third touch and a little 3303 and the 4th touch and a little 3403 constitute a rectangles or square, this has Conducive to providing stable support force for unmanned plane.

It is provided with shutdown canopy on the first airplane parking area 1000 and the second airplane parking area 2000, the columns of the shutdown canopy two sides can be with It is connected respectively with first side 1101, the 5th side 2101, such as shutting down canopy may include that the first covering and second cover.Assuming that the One column covered is C1, and the second column covered is C2, and one end of C1 column can be hinged with first side 1101, The other end of C1 column can be covered with first and is fixedly connected；One end of C2 column can be hinged with second side 1102, C2 The other end of column can be covered with second and is fixedly connected.It is shut down when unmanned plane is parked in the first airplane parking area 1000 and/or second After on level ground 2000, C1 column can be moved to can be moved to the orthogonal position of first electrode plate 1800, C2 column With the orthogonal position of second electrode plate 2800, at this point, C1 column will drive first to cover, C2 column will drive second to cover It makes a relative move, is closely combined until the first covering is covered with second, can then be formed and be hidden in the surrounding of unmanned plane Keep off the rain snow, travel fatigue shutdown canopy.Reach and reduces field extreme environment factor to unmanned plane, the first airplane parking area 1000 and the second shutdown The technical effect of the adverse effect on level ground 2000.After unmanned plane is fully charged, the first covering can be towards 1101 side of first side To movement, second covers and can then provide the top convenient for taking off for unmanned plane towards the movement of the direction of the 5th side 2101 Space.Reach the technical effect for not interfering unmanned plane normally to take off.

For energizing component 4000:

Energizing component 4000 may include storage assembly and bearing assembly 4200.The first charging has can be set in storage assembly Interface and the second charging interface.First charging interface can be connected with the first electric shock area 3102, and the first charging interface can be with It is connected with the second electric shock area 3202, and the first charging interface can be connected with third electric shock area 3302, and the first charging Mouth can be connected with the 4th electric shock area 3402；Second charging interface can touch a little 3103 connection, and the second charging with first Interface can touch a little 3203 connection with second, and the second charging interface can be touched with third and a little 3303 be connected, and the Two charging interfaces can touch a little 3403 connection with the described 4th.

Bearing assembly 4200 may include memory block 4201 and the second firm face.Storage assembly can be fixed on memory block In 4201, the second firm face can be fixedly connected with the first firm face.Wherein, the first electric shock area 3102 can be located at the first charging Between interface and first electrode bar 1700, the second electric shock area 3202 can be located at the first charging interface and first electrode bar 1700 it Between；Third gets an electric shock area 3302 can be positioned at the first charging interface and second electrode bar 2701 between, and the 4th gets an electric shock area 3402 can be with Between the first charging interface and second electrode bar 2701；First touches and a little 3103 can be located at first electrode plate 1800 and the Between two charging interfaces, second touch a little 3203 can be between first electrode plate 1800 and the second charging interface；Third is touched Contact 3303 can between second electrode plate 2800 and the second charging interface, the 4th touch a little 3403 can be located at second electricity Between pole plate 2800 and the second charging interface.

Energizing component 4000 can also include induction locator and photoemitter.Incuding locator can consolidate with second Face is fixedly connected；Photoemitter can be fixed on first electrode plate 1800 and/or second electrode plate 2800.

Continuing with referring to figure 1, figure 2 and figure 3, Fig. 1 is that a kind of charging for unmanned plane provided in an embodiment of the present invention fills The overall structure diagram set, Fig. 2 are a kind of left view diagrams of charging unit for unmanned plane provided in an embodiment of the present invention It is intended to, Fig. 3 is a kind of right view schematic diagram of charging unit for unmanned plane provided in an embodiment of the present invention.Storage assembly can To be to provide the battery of electric energy for unmanned plane.Bearing assembly 4200 can refer to that the fuselage of unmanned plane, storage assembly can be consolidated It is scheduled in the memory block 4201 of bearing assembly 4200.Storage assembly can follow unmanned plane to move together.First electric shock area 3102, Second electric shock area 3202, third electric shock area 3302 and the 4th electric shock area 3402 can be with the first charging interfaces of storage assembly (can be anode interface) connection, first touch a little 3103, second touch a little 3203, third touches and a little 3303 and the 4th touches a little 3403 can connect with the second charging interface (can be cathode interface) of storage assembly.Then storage assembly is led to The first charging interface is crossed, is connected with first electrode bar 1700 and second electrode bar 2701；Storage assembly can be filled by second Electrical interface is connected with first electrode plate 1800 and second electrode plate 2800.Control unit 1900 can pass through first electrode bar 1700 and second electrode bar 2701 provide cathode voltage for storage assembly, first electrode plate 1800 and second electrode plate can be passed through 2800 provide cathode voltage for storage assembly.The technical effect to charge to the storage assembly for unmanned plane.

First touch a little 3103 and first electric shock area 3102 spacing, with first electrode bar 1700 and first electrode plate 1800 Spacing it is equal；Second touch a little 3203 and second electric shock area 3202 spacing, can with second electrode bar 2701 and second electricity The spacing of pole plate 2800 is equal；Third touch a little 3303 and third electric shock area 3302 spacing, can be with first electrode bar 1700 It is equal with the spacing of first electrode plate 1800；4th touch a little 3403 and the 4th electric shock area 3402 spacing, can with second electricity Pole bar 2701 is equal with the spacing of second electrode plate 2800.It can be preferably first electrode bar 1700 and first electrode plate 1800 Spacing range is 180mm -220mm, such as first touch a little 3103 and first get an electric shock area 3102 spacing be also possible to 180mm or Person 220mm.This makes first electrode bar 1700 and the first electric shock area 3102 have good be in contact.To be reached for the first touching Electric area 3102 conveys the technical effect of efficient electric energy.

The fuselage height of unmanned plane can be greater than the spacing of first electrode bar 1700 and first electrode plate 1800, such as carrying group The spacing in the second of part 4200 firm face and first electrode plate 1800 can be greater than first electrode bar 1700 and first electrode plate 1800 spacing.This can prevent the contact of the fuselage obstruction first electrode bar 1700 of unmanned plane with the first electric shock area 3102.The Maximum spacing between one electrode stem 1700 and second electrode bar 2701 can be greater than in unmanned plane first and touch a little 3103 and the The two maximum spacing touched between a little 3203 spacing, such as first electrode bar 1700 and second electrode bar 2701 can be 40cm.To reach make the first of unmanned plane touch a little 3103 and third touch a little 3303, can connect with first electrode plate 1800 It connects；Second touches and a little 3203 and the 4th touches a little 3403, the technical effect that can be connect with first electrode plate 1800.

Photoemitter can match with induction locator, i.e. induction locator can detecte locating for photoemitter Position.Photoemitter can be mounted on first electrode plate 1800 and/or second electrode plate 2800, locator will be incuded It is mounted on the second firm face of bearing assembly 4200, such as induction locator is mounted on to the fuselage bottom of unmanned plane.It makes a return voyage Unmanned plane to be charged can be directed to the first airplane parking area 1000 and/or second by RTK (carrier phase difference technology) and shut down After the top of level ground 2000, accurately unmanned plane can be guided to drop to first electrode plate by laser that photoemitter is emitted 1800 and/or second electrode plate 2800 on.It avoids unmanned plane and drops to the first airplane parking area 1000 and/or the second airplane parking area 2000 Edge (the adjacent region in such as third side 1103 and first electrode plate 1800) when, unmanned plane parks shakiness, can be slipped to ground Face damages unmanned plane, causes to charge to unmanned plane.Make unmanned plane can be with stable landing to first electrode to reach On plate 1800 and/or second electrode plate 2800, be conducive to when first electrode bar 1700 and second electrode bar 2701 relatively move, Make the first electric shock area 3102 and third electric shock area 3302, is completely attached to first electrode bar 1700；Second electric shock area 3202 and the Four electric shock areas 3402, completely attach to second electrode bar 2701.So that the first charging interface and the second charging of storage assembly Mouth can be linked into charging circuit, the technical effect charged normal to unmanned plane.

The present invention provides a kind of energy supply airplane parking area mechanism for unmanned plane, passes through the first ducted body in the first airplane parking area First side on first through hole is set, the first rotating shaft of first servo motor is passed through into first through hole, first in the first screw rod One end of screw rod is fixedly connected with first rotating shaft, and the other end of the first screw rod is fixedly connected with the first node of first side. First fastening end of the first guide rail is fixedly connected with the first interface of first side, the second fastening end of the first guide rail and second The third interface of side is fixedly connected, and the first guide rail passes through first slot at first movement end in the first pedestal；Second guide rail Third fastening end is fixedly connected with the second interface of first side, and the 4th fastening end of the second guide rail and the 4th of second side connect Mouth is fixedly connected, and the second guide rail passes through the second slot of the second mobile terminal in the first pedestal.By the first support of the first support arm First spacing zone at end and first movement end is hinged, the third support end of the second support arm and the second limit of the second mobile terminal Area is hinged.First locking end in first electrode bar is fixedly connected with the second support end, the second locking end and the 4th support end It is fixedly connected.First electrode plate and the first opening face are detachably connected.Control unit and the first noumenon of first servo motor connect It connecing, after the first rotating shaft of first servo motor passes through first through hole, first rotating shaft is connected with the first screw rod of the first screw rod, the First conformable region of one pedestal is fixedly connected with the first sliding block being set in outside the first screw rod, by the of first servo motor band The direction that one electrode stem can need to charge towards unmanned plane is mobile.Then when unmanned plane drops on the first airplane parking area, lead to It crosses first electrode bar and first electrode plate charges to unmanned plane.Pass through the 5th side of the second ducted body in the second airplane parking area Second through-hole is set on face, the second shaft of the second servo motor is passed through into the second through-hole, the one of the second screw rod in the second screw rod End is fixedly connected with the second shaft, and the second node of the other end of the second screw rod and the 6th side is fixedly connected.Third is led 5th fastening end of rail is fixedly connected with the 5th interface, and the 6th fastening end of third guide rail is fixedly connected with the 7th interface, third Guide rail passes through the third slot of third mobile terminal in the second pedestal；7th fastening end of the 4th guide rail and the fixed company of the 6th interface It connects, the 8th fastening end of the 4th guide rail is fixedly connected with the 8th interface, and the 4th guide rail passes through the 4th movement in the second pedestal 4th slot at end.Second electrode plate and the second opening face are detachably connected, control unit and the connection of the second ontology.By the second base Second conformable region of seat is fixedly connected with the second sliding block for being set in the second screw rod, by the second electrode bar of the second servo motor band The direction that can need to charge towards unmanned plane is mobile.Then when unmanned plane drops on the second airplane parking area, pass through the second electricity Pole bar and second electrode plate can charge for unmanned plane.Meanwhile first by that will energize storage assembly in component charges Interface and the first electric shock area connection, the first charging interface and the second electric shock area connection, the first charging interface and third electric shock area connect It connects, the first charging interface and the 4th electric shock area connection；Second charging interface and first are touched into connection, the second charging interface and Second touches a connection, and the second charging interface and third touch a connection, and the second charging interface and the 4th touch a connection.Again will Storage assembly is fixed in the memory block of bearing assembly, and the firm face of the second of bearing assembly is fixedly connected with the first firm face.After And it can charge for unmanned plane.To reach can reduce unmanned plane charge maintenance needed for manpower and material resources, make to charge Journey is convenient；Improve the technical effect of the working efficiency of unmanned plane.

It should be noted last that the above specific embodiment is only used to illustrate the technical scheme of the present invention and not to limit it, Although being described the invention in detail referring to example, those skilled in the art should understand that, it can be to the present invention Technical solution be modified or replaced equivalently, without departing from the spirit and scope of the technical solution of the present invention, should all cover In the scope of the claims of the present invention.

Claims (10)

1. a kind of energy supply airplane parking area mechanism for unmanned plane, which is characterized in that the energy supply airplane parking area machine for unmanned plane Structure includes:

First airplane parking area, first airplane parking area include:

First ducted body, first ducted body are provided with first side, second side, third side, the 4th side, the first bottom Face and the first opening face, are provided with first interface, second interface and first through hole in the first side, the first interface and The second interface is symmetrical relative to the first through hole；Third interface, the 4th interface are provided in the second side And first node, the third interface and the 4th interface are symmetrical relative to the first node；

First guide rail, first guide rail are provided with the first fastening end and the second fastening end, first fastening end and described One interface is fixedly connected, and second fastening end is fixedly connected with the third interface；

Second guide rail, second guide rail are provided with third fastening end and the 4th fastening end, the third fastening end and described Two interfaces are fixedly connected, and the 4th fastening end is fixedly connected with the 4th interface；

First servo motor, the first servo motor include the first noumenon and first rotating shaft, the first noumenon and described One side is fixedly connected, and the first rotating shaft passes through the first through hole；

First screw rod, first screw rod include the first screw rod and the first sliding block, one end of first screw rod and described first Shaft is fixedly connected, and the other end of first screw rod is fixedly connected with the first node；

First pedestal, first pedestal are provided with first movement end, the second mobile terminal and the first conformable region, the first movement End is provided with the first slot and the first spacing zone, and first guide rail passes through first slot, and first slot is located at Between first fastening end and second fastening end；Second mobile terminal is provided with the second slot and the second spacing zone, Second guide rail passes through second slot, and second slot is located at the third fastening end and the 4th fastening end Between；First sliding block is fixed on first conformable region；

First support arm, first support arm are provided with the first support end and the second support end, first support end and institute The first spacing zone is stated to be hinged；

Second support arm, second support arm are provided with third support end and the 4th support end, the third support end and institute The second spacing zone is stated to be hinged；

First electrode bar, the first electrode bar are provided with the first locking end and the second locking end, first locking end and institute It states the second support end to be fixedly connected, second locking end is fixedly connected with the 4th support end；

First electrode plate, the first electrode plate and first opening face are detachably connected, and the first electrode plate is located at Between first support end and the third support end；

Control unit, the control unit are connected with the first noumenon, and the first through hole be located at the first noumenon and Between the control unit；

Wherein, the first side and the second side are two opposed faces, the third side and the 4th side Face is two opposed faces, and first bottom surface and the first opening face are two opposed faces；First fastening end and Second fastening end is the both ends of the first guide rail opposition；The third fastening end and the 4th fastening end are described The both ends of two guide rails opposition；First sliding block is set in the outside of first screw rod, first screw rod and described first Side is vertical, and first screw rod and the second side are vertical；The first movement end and second mobile terminal are opposite It is symmetrical in first conformable region；The first movement end between the first electrode plate and first bottom surface, And second mobile terminal is between the first electrode plate and first bottom surface；

Second airplane parking area, second airplane parking area include:

Second ducted body, second ducted body are provided with the 5th side, the 6th side, heptalateral face, the 8th side, the second bottom Face and the second opening face, are provided with the 5th interface, the 6th interface and the second through-hole on the 5th side, the 5th interface and 6th interface is symmetrical relative to second through-hole；The 7th interface, the 8th interface are provided on 6th side And second node, the 7th interface and the 8th interface are symmetrical relative to the second node；

Third guide rail, the third guide rail are provided with the 5th fastening end and the 6th fastening end, the 5th fastening end and described Five interfaces are fixedly connected, and the 6th fastening end is fixedly connected with the 7th interface；

4th guide rail, the 4th guide rail are provided with the 7th fastening end and the 8th fastening end, the 7th fastening end and described Six interfaces are fixedly connected, and the 8th fastening end is fixedly connected with the 8th interface；

Second servo motor, second servo motor include the second ontology and the second shaft, second ontology and control unit Part is fixedly connected, and second shaft passes through second through-hole；

Second screw rod, second screw rod include the second screw rod and the second sliding block, one end of second screw rod and described second Shaft is fixedly connected, and the other end of second screw rod is fixedly connected with the second node；

Second pedestal, second pedestal are provided with third mobile terminal, the 4th mobile terminal and the second conformable region, and the third is mobile End is provided with third slot and third spacing zone, and the third guide rail passes through the third slot, and the third slot is located at Between 5th fastening end and the 6th fastening end；4th mobile terminal is provided with the 4th slot and the 4th spacing zone, 4th guide rail passes through the 4th slot, and the 4th slot is located at the 7th fastening end and the 8th fastening end Between；Second sliding block is fixed on second conformable region；

Third support arm, the third support arm are provided with the 5th support end and the 6th support end, the 5th support end and institute State the connection of third spacing zone；

4th support arm, the 4th support arm are provided with the 7th support end and the 8th support end, the 7th support end and institute State the connection of the 4th spacing zone；

Second electrode bar, the second electrode bar are provided with third locking end and the 4th locking end, the third locking end and institute The connection of the 6th support end is stated, the 4th locking end is connected with the 8th support end；

Second electrode plate, the second electrode plate and second opening face are detachably connected, and the second electrode plate is located at Between 5th support end and the 7th support end；

Wherein, the 6th side and second side are detachably connected；5th side and the 6th side are two phases The face of opposition, heptalateral face and the 8th side are two opposed faces, second bottom surface and the second opening face It is two opposed faces；5th fastening end and the 6th fastening end are the both ends of the third guide rail opposition；It is described 7th fastening end and the 8th fastening end are the both ends of the 4th guide rail opposition；Second sliding block is set in described second The outside of screw rod, second screw rod and the 5th side are vertical, and second screw rod and the 6th side are vertical；Institute It is symmetrical relative to second conformable region to state third mobile terminal and the 4th mobile terminal；The third mobile terminal is located at institute It states between second electrode plate and second bottom surface, and the 4th mobile terminal is located at the second electrode plate and second bottom Between face；

Component is energized, the energy supply component includes:

Storage assembly, the storage assembly are provided with the first charging interface and the second charging interface, first charging interface and First electric shock area connection, and first charging interface and the second electric shock area connection, and first charging interface and third touching Electric area's connection, and first charging interface and the 4th electric shock area connection；Second charging interface and first touches a connection, And second charging interface and second touches a connection, and second charging interface and third touch a connection, and described Second charging interface and the 4th touches a connection；

Bearing assembly, the bearing assembly include memory block and the second firm face, and the storage assembly is fixed on the memory block Interior, the second firm face is fixedly connected with the first firm face；

Wherein, first electric shock area is between first charging interface and first electrode bar, second electric shock position Between first charging interface and the first electrode bar；Third electric shock area is located at first charging interface and the Between two electrode stems, the 4th electric shock area is between first charging interface and the second electrode bar.

2. be used for the energy supply airplane parking area mechanism of unmanned plane as described in claim 1, which is characterized in that described for unmanned plane Energize airplane parking area mechanism further include:

First foot pad；

Second foot pad；

First bottom surface is additionally provided with the first corner region and the second corner region, and first foot pad is fixed on first corner Area, second foot pad are fixed on second corner region.

3. be used for the energy supply airplane parking area mechanism of unmanned plane as claimed in claim 2, which is characterized in that described for unmanned plane Energizing airplane parking area mechanism includes:

Between first foot pad and first opening face, second corner region is located at described for first corner region Between second foot pad and first opening face.

4. be used for the energy supply airplane parking area mechanism of unmanned plane as claimed in claim 3, which is characterized in that described for unmanned plane Energizing airplane parking area mechanism includes:

First detector；

Second detector；

First opening face is additionally provided with the first detection zone and the second detection zone, and first detector is fixed on described first Detection zone, second detector are fixed on second detection zone.

5. be used for the energy supply airplane parking area mechanism of unmanned plane as claimed in claim 4, which is characterized in that described for unmanned plane Energizing airplane parking area mechanism includes:

Between first detector and first bottom surface, second detection zone is located at described first detection zone Between second detector and first bottom surface.

6. be used for the energy supply airplane parking area mechanism of unmanned plane as claimed in claim 5, which is characterized in that described for unmanned plane Energize airplane parking area mechanism further include:

First guiding groove, first guiding groove and the first electrode plate are detachably connected, and first guiding groove and institute Third side is stated to be detachably connected；First guiding groove is between first support end and second support end.

7. be used for the energy supply airplane parking area mechanism of unmanned plane as claimed in claim 6, which is characterized in that described for unmanned plane Energize airplane parking area mechanism further include:

Second guiding groove, second guiding groove and the first electrode plate are detachably connected, and first guiding groove and institute The 4th side is stated to be detachably connected；Second guiding groove is between the third support end and the 4th support end.

8. be used for the energy supply airplane parking area mechanism of unmanned plane as claimed in claim 7, which is characterized in that described for unmanned plane Energizing airplane parking area mechanism includes:

The first electrode plate is cathode.

9. be used for the energy supply airplane parking area mechanism of unmanned plane as claimed in claim 8, which is characterized in that described for unmanned plane Energizing airplane parking area mechanism includes:

The first electrode bar is anode.

10. being used for the energy supply airplane parking area mechanism of unmanned plane as claimed in claim 9, which is characterized in that described to be used for unmanned plane Energy supply airplane parking area mechanism include:

The second electrode bar is anode.