CN206485585U - A kind of unmanned plane relay - Google Patents
A kind of unmanned plane relay Download PDFInfo
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- CN206485585U CN206485585U CN201720174828.8U CN201720174828U CN206485585U CN 206485585 U CN206485585 U CN 206485585U CN 201720174828 U CN201720174828 U CN 201720174828U CN 206485585 U CN206485585 U CN 206485585U
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- battery
- clamping plate
- type clamping
- unmanned plane
- parking area
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Abstract
The utility model is related to a kind of unmanned plane relay; which solve existing multi-rotor unmanned aerial vehicle and can not realize and continue, efficiently extensive area is cruised; existing relaying technique Fit Models are single; unmanned plane must carry out the technical problem that prolonged charging is waited, and it includes airplane parking area, limiting fixing mechanism, battery depressed place and battery changing mechanism；Limiting fixing mechanism is provided with the first V-type clamping plate, the second V-type clamping plate and relative motion transmission device; first V-type clamping plate and the second V-type clamping plate are oppositely arranged and are located at the top on airplane parking area deck; battery changing mechanism includes cantilever, electromagnet and is vertically connected on the linear module of horizontal direction and the linear module of vertical direction together; cantilever is connected with the vertical direction sliding block on the linear module of vertical direction; electromagnet is connected with cantilever, and battery depressed place is provided with battery case.The utility model is widely used in unmanned plane relay system.
Description
Technical field
The utility model is related to the relay station service system of unmanned plane, more particularly to a kind of unmanned plane relay.
Background technology
In recent years, with unmanned air vehicle technique maturation and development, multi-rotor unmanned aerial vehicle because its VTOL, freely hover,
The features such as manipulation convenience, strong adaptability, is widely used in power-line patrolling, pipeline inspection, forest fire protection inspection, border inspection, agriculture
The fields such as field acquisition of information.
In terms of navigation and location technology, multi-rotor unmanned aerial vehicle flight control system has radio communication, sensor integration and sky
Between the function such as positioning, wherein, differential GPS location technology (double frequencies RTK) can reach the positioning precision of Centimeter Level, and magnetic compass is determined
To trueness error within ± 5 °, barometertic altimeter, sonar, infrared distance measurement combine height detecting module range accuracy ±
Within 1%~± 5%.In addition, under the auxiliary that specialty is taken photo by plane with vision system, the landing precision of multi-rotor unmanned aerial vehicle can be entered
One step is guaranteed.
In terms of battery technology, existing multi-rotor unmanned aerial vehicle mainly uses lithium polymer battery, the carrying mode of battery
Mostly horizontal hanging, battery capacity is 10000mAh~15000mAh, due to by battery energy under existing battery technology
Charging and cool time needed for the restriction of metric density and charge efficiency, unmanned plane be about 1.2 hours, and fully charged is taken off again
Cruising time is also only 30 minutes or so, greatly reduces the cruise efficiency of unmanned plane.Therefore, explore and provide continuous for unmanned plane
Boat relaying simultaneously avoids the low efficiency problem of charge-carrying belt from turning into those skilled in the art's technical problem urgently to be resolved hurrily simultaneously.
At present, the use of charging relay station is that unmanned plane continuation of the journey is a kind of feasible program, Maximum Endurance radius can be overcome
Limitation.But, unmanned plane need to be parked about 1.2 hours after station in charging to be charged, and efficiency is very low, not yet from truly
Break away from voyage limitation, it is impossible to which realization is efficiently cruised extensive area.In addition, charging relay station Fit Models are more single
One, without versatility.
, can also be in someone's relay station by manually changing battery, this technical side in addition to charging relay station is used
Case cost is high, and efficiency is also very low.
The content of the invention
The utility model is exactly that can not be realized persistently, efficiently to extensive area to solve existing multi-rotor unmanned aerial vehicle
Cruised, existing relaying technique Fit Models are single, unmanned plane must carry out the technical problem that prolonged charging is waited, and carry
Having supplied one kind can continue, efficiently extensive area is cruised, the unmanned plane relay of highly versatile.
The technical solution of the utility model is to provide a kind of unmanned plane relay, including airplane parking area, spacing fixed machine
Structure, battery depressed place and battery changing mechanism；
Airplane parking area includes airplane parking area deck and the airplane parking area support frame linked together；
Limiting fixing mechanism includes the first V-type clamping plate, the second V-type clamping plate and relative motion transmission device, the first V-type clamping plate
Provided with the first V-type press section, the second V-type clamping plate is provided with the second V-type press section；First V-type clamping plate and the second V-type clamping plate respectively with
Relative motion transmission device is connected, and relative motion transmission device is used to drive the first V-type clamping plate and the relative fortune of the second V-type clamping plate
It is dynamic；
First V-type clamping plate and the second V-type clamping plate are oppositely arranged and are located at the top on airplane parking area deck；
Battery changing mechanism includes the linear module of horizontal direction, the linear module of vertical direction, cantilever and electromagnet, level side
Horizontal direction sliding block is provided with to linear module, the linear module of vertical direction is provided with vertical direction sliding block；The linear module of vertical direction
End be connected with horizontal direction sliding block, cantilever is connected with vertical direction sliding block, and electromagnet is connected with cantilever；
Battery depressed place is provided with battery case, and battery depressed place is located between the battery changing mechanism and airplane parking area.
Technical scheme preferably is that airplane parking area deck is provided with two guide channels being oppositely arranged, and is the first bullport
Road and the second guide channel；
Relative motion transmission device includes line slideway component, contiguous block, retractor device, first connecting rod, second connecting rod, the
One V-type clamping plate connector and the second V-type clamping plate connector；Line slideway component is provided with the first sliding block and the second sliding block, the first V-type
Clamping plate is connected by the first V-type clamping plate connector with the first sliding block, and the second V-type clamping plate passes through the second V-type clamping plate connector and
Two sliding blocks are connected, and contiguous block is connected by first connecting rod with the first sliding block, and contiguous block is connected by second connecting rod with the second sliding block,
Retractor device is provided with expansion link, and expansion link is connected with contiguous block；First V-type clamping plate connector passes through the first guide channel, the 2nd V
Type clamping plate connector passes through the second guide channel.
Technical scheme further preferably is that the two ends of the first V-type press section are connected to rib, and the second V-type is squeezed
The two ends of splenium are connected to rib.
Technical scheme further preferably is that the center line of the center line of the first V-type press section and the second V-type press section is same
On one straight line.
Technical scheme further preferably is that battery depressed place includes battery and places cylinder, motor, base and connecting shaft；Even
One end of spindle is placed cylinder with battery and is connected, and the other end is connected by bearing with base；Motor is by transmission mechanism with being connected
Axle is connected, and battery places cylinder and is provided with an at least row battery case group from top to bottom, and battery case group is provided with least two battery cases；
Battery case is included before housing, back plate, contact and two spring latch locks, the rear end connection of back plate and housing, housing
End opening, two spring latch locks are connected to the both sides of housing；The inner side connection of contact and back plate, back plate is provided with cabling
Hole.
Technical scheme further preferably is that battery places cylinder and is provided with three row battery case groups, adjacent two from top to bottom
Angle between row battery case group is 120 °, and each column battery case group is provided with three battery cases.
Technical scheme further preferably is, in addition to switch board, switch board include central processing unit, power module and
Wireless communication module, power module is connected with central processing unit, and wireless communication module is connected with central processing unit；Central processing unit
Power output signal end be connected with electromagnet；The drive signal end of central processing unit respectively with retractor device, motor, level side
To linear module and the linear module connection of vertical direction.
The beneficial effects of the utility model are：
(1) automatic exchange battery operation is realized, unmanned plane residence time on relay is no more than 5 minutes, greatly
The residence time is shortened greatly, and because the electric energy loss that empty driving is brought is low, one is passed through by rationally laying relay point and really realizing
Efficient cruise of the frame unmanned plane to extensive area.
(2) changing the technical scheme of battery has versatility, it is adaptable to the unmanned plane of all setting undercarriages.
The utility model further feature, by the description of detailed description below, is clearly stated that.
Brief description of the drawings
Fig. 1 is the stereogram of unmanned plane relay；
Fig. 2 is the front view of unmanned plane relay；
Fig. 3 is the left view of unmanned plane relay；
Fig. 4 is the top view of unmanned plane relay；
Fig. 5 is the stereogram of airplane parking area；
Fig. 6 is the front view of airplane parking area；
Fig. 7 is the left view of airplane parking area；
Fig. 8 is the top view of airplane parking area；
Fig. 9 is the structural representation of limiting fixing mechanism；
Figure 10 is the structural representation of limiting fixing mechanism；
The structural representation of Figure 11 the first V-type clamping plate connectors；
Figure 12 is the first V-type clamping plate connector, the second V-type clamping plate connector respectively from the first guide channel, the second guiding
The schematic diagram that duct is passed through；
Figure 13 is the structural representation of the first V-type clamping plate；
Figure 14 is the structural representation that the first V-type clamping plate installs roller；
Figure 15 is the stereogram in battery depressed place；
Figure 16 is the front view in battery depressed place；
Figure 17 is the left view in battery depressed place；
Figure 18 is the battery case structure schematic diagram in battery depressed place；
Figure 19 is the sectional view in battery depressed place；
Figure 20 is the schematic internal view that top cover is removed in battery depressed place；
Figure 21 is the stereogram of battery case；
Figure 22 is the front view of battery case；
Figure 23 is the left view of battery case；
Figure 24 is the right view of battery case；
Figure 25 is the explosive view of battery case；
Figure 26 is the stereogram of battery component；
Figure 27 is the front view of battery component；
Figure 28 is battery component left view；
Figure 29 is battery component right view；
Figure 30 is the explosive view of battery component；
Figure 31 is the stereogram of battery changing mechanism；
Figure 32 is the front view of battery changing mechanism；
Figure 33 is the right view of battery changing mechanism；
Figure 34 is the top view of battery changing mechanism；
Figure 35 is the schematic diagram of switch board；
Figure 36 is the stereogram of rack；
Figure 37 is the schematic diagram under rack open mode；
Figure 38 is the top view under rack open mode；
Figure 39 is the view that multi-rotor unmanned aerial vehicle is dropped on airplane parking area deck；
Figure 40 is the top view of fixation procedure state during limiting fixing mechanism is adjusted to multi-rotor unmanned aerial vehicle；
Figure 41 is the stereogram of fixation procedure state during limiting fixing mechanism is adjusted to multi-rotor unmanned aerial vehicle；
Figure 42 is that the top view under state is fixed during limiting fixing mechanism adjusts multi-rotor unmanned aerial vehicle；
Figure 43 is that the stereogram under state is fixed during limiting fixing mechanism adjusts multi-rotor unmanned aerial vehicle.
Symbol description in figure：
100. airplane parking area；200. limiting fixing mechanism；300. battery depressed places；400. battery component；500. battery changing mechanism；
600. switch board；700. rack；800. multi-rotor unmanned aerial vehicle；110. airplane parking area deck；111. the first guide channel；112. second
Guide channel；120. airplane parking area support frame；130. airplane parking area bottom plate；210. first V-type clamping plates；220. second V-type clamping plates；
211. first V-type press sections；212. first ribs；213. second ribs；230. line slideway components；231. first sliding blocks；
232. second sliding blocks；240. contiguous block；250. retractor device fixed plates；260. retractor device；270a. first connecting rod；270b. the
Two connecting rods；280a. the first L-type risers；280b. the second L-type risers；290a. the first V-type clamping plate connectors；The V-types of 290b. second
Clamping plate connector；310. batteries place cylinder, 320. stepper motors；330. synchronous belt drive mechanism；340. base；350. connection
Axle；360. battery case；361. upper shell；362. lower house；363. back plate；364. spring latch lock；365. contact；Battery on 410.
Shell；420. times battery cases；430. magnet suction pieces；440. contact；421. magnet suction piece mounting grooves；422. lock groove；510. level
Dimension linear module；The linear module of 520. vertical direction；530. cantilever；540. crawl arm；550. electromagnet；610. center processing
Device；620. power module；630. wireless communication module；640. battery；650. charging module；660. unmanned plane battery components fill
Electrical equipment；710. cabinet；720. solar panel outer covers；810. undercarriage.
Embodiment
Referring to the drawings, the utility model is described in further detail with specific embodiment.
As Figure 1-4, unmanned plane relay includes airplane parking area 100, limiting fixing mechanism 200, battery depressed place 300, electricity
Change mechanism 500, switch board 600 in pond.
Airplane parking area 100 is used to park unmanned plane.Limiting fixing mechanism 200 be used in the tune of different model unmanned plane, it is right
It is neat and fixed, by tune, alignment action by unmanned plane be moved to airplane parking area 100 center and by battery cephalosome just to battery more
Converting mechanism 500.The function in battery depressed place 300 is the full electric battery of storage and is without battery charging on the machine taken out.Switch board 600 is made
For the control section of whole relay, it is responsible for control other components action.
As viewed in figures 5-8, airplane parking area 100 includes airplane parking area deck 110, airplane parking area support frame 120, airplane parking area bottom plate
130, airplane parking area deck 110 is connected with the top of airplane parking area support frame 120, airplane parking area bottom plate 130 and airplane parking area support frame
120 bottom connection.Airplane parking area deck 110 is provided with two guide channels being oppositely arranged, and is the He of the first guide channel 111 respectively
Second guide channel 112.Preferably, the first guide channel 111 and the second guide channel 112 be on the same line.
As shown in figure 9, limiting fixing mechanism 200 includes the first V-type clamping plate 210, the second V-type clamping plate 220, line slideway group
Part 230, contiguous block 240, retractor device fixed plate 250, retractor device 260, first connecting rod 270a, second connecting rod 270b, the first L
Type riser 280a, the second L-type riser 280b, the first V-type clamping plate connector 290a, the second V-type clamping plate connector 290b.Straight line is led
Rail assembly 230 is fixedly mounted in airplane parking area support frame 120, and two sliding blocks are connected with line slideway component 230, are respectively
First sliding block 231 and the second sliding block 232.First L-type riser 280a is connected with the first sliding block 231, the second L-type riser 280b and
Two sliding blocks 232 are connected.First V-type clamping plate 210 is connected by the first V-type clamping plate connector 290a with the first L-type riser 280a, the
Two V-type clamping plates 220 are connected by the second V-type clamping plate connector 290b with the second L-type riser 280b.As shown in figs. 10-11, first
V-type clamping plate connector 290a top is connected with the first V-type clamping plate 210, and bottom is connected with the first L-type riser 280a.Second V-type
Clamping plate connector 290b is identical with the first V-type clamping plate connector 290a structure.As shown in figure 12, the first V-type clamping plate connector
290a bottom is passed through from the first guide channel 111, and the second V-type clamping plate connector 290b bottom is from the second guide channel 112
Through (it should be noted that the first V-type clamping plate connector 290a bottom can be not passed through the first guide channel 111, but from
The side on airplane parking area deck 110 is bypassed；Similarly, the second V-type clamping plate connector 290b bottom can be not passed through the second bullport
Road 112, but bypassed from the side on airplane parking area deck 110.In this case, avoid the need for setting on airplane parking area deck 110
First guide channel 111 and the second guide channel 112).First V-type clamping plate 210 and the second V-type clamping plate 220 are located at airplane parking area first
At the locus faced up of plate 110, the first V-type clamping plate 210, the second V-type clamping plate 220 are oppositely arranged in the horizontal plane.
Contiguous block 240 is connected by first connecting rod 270a with the first L-type riser 280a, and contiguous block 240 passes through second connecting rod 270b and
Two L-type riser 280b connections.The expansion link of retractor device 260 is connected with contiguous block 240, and retractor device 260, which is fixedly mounted on, to be stretched
In compression apparatus fixed plate 250.Retractor device fixed plate 250 is fixedly connected on the back side on airplane parking area deck 110, and retractor device is fixed
Plate 250 is used to retractor device 260 is fixedly mounted.Retractor device fixed plate 250 can also be fixed on airplane parking area support frame 120
On.
As shown in figure 13, the first V-type clamping plate 210 includes the first V-type press section 211, the two ends of the first V-type press section 211
It is connected to the first rib 212, the second rib 213.The V-type angle [alpha] of first V-type press section 211 is 110 °~150 °.First
Rib 212, the effect of the second rib 213 are to avoid multi-rotor unmanned aerial vehicle from departing from airplane parking area deck 110.
The structure of second V-type clamping plate 220 is identical with the first V-type clamping plate 210, and provided with the second V-type press section, the second V-type is squeezed
The two ends of splenium are connected to rib.
It should be noted that the first V-type clamping plate 210 and the second V-type clamping plate 220 set rib to be preferred plan, can be only
Set V-type press section to be not provided with rib, can also complete corresponding function.
In order to improve the accuracy in being adjusted to unmanned plane, the center line and the second V-type folder of the first V-type press section 211 can be made
On the same line, two dotted lines as shown in Figure 8 represent two center lines to the center line of second V-type press section of plate 220.
In a word, line slideway component 230, contiguous block 240, retractor device 260, first connecting rod 270a, second connecting rod are set
270b, the first L-type riser 280a, the second L-type riser 280b, the first V-type clamping plate connector 290a, the second V-type clamping plate connector
290b and make the first V-type clamping plate connector 290a, the second V-type clamping plate connector 290b be each passed through the first guide channel 111,
The structure of second guide channel 112, the purpose is to drive the first V-type clamping plate 210, the relative motion of the second V-type clamping plate 220, also
It is the reciprocating motion for making the first V-type clamping plate 210, the second V-type clamping plate 220 be drawn close, opened.Therefore, as long as this can be realized
The relative motion transmission device of function is all suitable for.
As shown in figure 14, in order that the first V-type clamping plate 210, the movement of the second more steady and smooth of V-type clamping plate 220, Ke Yi
Its back side is installed by two rollers.Roller supporting is on airplane parking area deck 110.
Retractor device 260 can be electric pushrod component, cylinder component or cylinder assembly.
As shown in figs. 15 to 20, battery depressed place 300 includes battery placement cylinder 310, stepper motor 320, synchronous belt drive mechanism
330th, base 340, connecting shaft 350, one end and the battery of connecting shaft 350 are placed cylinder 310 and are connected, and the other end passes through bearing and bottom
Seat 340 is connected, and stepper motor 320 is connected by synchronous belt drive mechanism 330 with connecting shaft 350.Battery places cylinder 310 by this
Body, top cover and bottom plate are formed by connecting.Base 340 is arranged on the airplane parking area bottom plate 130 of airplane parking area 100, and stepper motor 320 also leads to
Support is crossed on airplane parking area bottom plate 130.Battery place cylinder 31 bottom plate on be connected with three risers, each riser from
Top to bottm is provided with a row battery case group, and one has three row battery case groups, and (it is A, secondary series battery to define first row battery case group
Groove group is B, and the 3rd row battery case group is C), the angle between adjacent two row battery case group is 120 °, and each column battery case group is by three
The individual battery case 360 for placing battery component is constituted.
It should be noted that battery case group is not limited to three row, can be a row, two row or more multiple row.Each column is not limited to
Three battery cases are set, can be two or more.The particular number of battery case can lay place according to relay
Neighbouring unmanned plane quantity and unmanned plane change the frequency of battery to determine.
As shown in Figure 21-25, battery case 360 includes upper shell 361, lower house 362, back plate 363, two spring latch locks
364 and six contacts 365, upper shell 361 and lower house 362 link together composition housing, back plate 363 with after the housing
End connection, the front opening of the housing.Two spring latch locks 364 are connected to the both sides of lower house 362.Back plate 363 it is interior
Side is connected in contact mounting groove provided with six contact mounting grooves, six contacts 365, and six contacts 365 are used for battery component
400 chargings.Back plate 363 is provided with six cable holes.The riser that the outside of back plate 363 is placed with battery on the bottom plate of cylinder 31 connects
Connect.Six roots of sensation charge cable one is connected through six cable holes in back plate 363 with six contacts 365, and other end passes through connection
The central through hole of axle 350 is connected to the unmanned plane battery component charger 660 in switch board 600.
Stepper motor 320 is acted, and drives connecting shaft 350 to rotate in the presence of synchronous belt drive mechanism 330, connecting shaft
350, which rotate drive battery placement cylinder 310, rotates, so as to adjust the orientation of three row battery case groups.
It should be noted that battery depressed place 300 is not limited on the airplane parking area bottom plate 130 of airplane parking area 100, it can also pacify
Outside mounted in airplane parking area 100, at battery changing mechanism 500.
As shown in Figure 26-30, battery component 400 in multi-rotor unmanned aerial vehicle include upper battery case 410, lower battery case 420,
Magnet suction piece 430, contact 440, upper battery case 410 and lower battery case 420 link together composition battery container, lower battery case
420 front end is provided with magnet suction piece mounting groove 421, and the both sides of lower battery case 420 are respectively equipped with lock groove 422.Contact 440 is installed
In the rear end of lower battery case 420, magnet suction piece 430 is arranged in magnet suction piece mounting groove 421.Battery is provided with battery container
Body, contact 440 is connected with battery core body.The quantity of contact 440 could be arranged to six, and two of which is used to use when discharging,
With six during charging.
When battery component 400 is inserted into the battery case 360 in battery depressed place 300, two spring latch locks of battery case 360
364 match with lock groove 422, to fix battery component 400.Contact 440 is contacted with the contact 365 of battery case 360, thus
Foring the unmanned plane battery component charger 660 in charge circuit, switch board 600 can just charge to battery component 400.
The battery compartment of battery component 400 is accommodated in multi-rotor unmanned aerial vehicle, can be with existing conventional techniques means to battery pack
Part is fixed, and can also use such as the structure of upper shell 361, lower house 362 and two compositions of spring latch lock 364 in Figure 25.
It is used for the structure with the contact pad of battery component in multi-rotor unmanned aerial vehicle, using existing conventional techniques.
As shown in Figure 31-34, battery changing mechanism 500 includes the linear module 510 of horizontal direction, the linear module of vertical direction
520th, cantilever 530, crawl arm 540, electromagnet 550, the linear module 510 of horizontal direction are provided with horizontal direction sliding block, vertical direction
The end of linear module 520 is connected with horizontal direction sliding block, and the linear module 520 of vertical direction is provided with vertical direction sliding block, cantilever
530 are connected with vertical direction sliding block, and crawl arm 540 is connected with cantilever 530, and electromagnet 550 is connected with crawl arm 540.Need
Bright, electromagnet 550 can also be connected directly with cantilever 530.
The linear module 510 of horizontal direction and the linear module 520 of vertical direction constitute X-direction, Z-direction travel mechanism,
Cantilever 530 is arranged on Y direction.
The linear module 510 of horizontal direction can be that, by motor-driven screw pair, the motor can be stepper motor or watch
Take motor.The linear module 520 of vertical direction can be that, by motor-driven screw pair, the motor can be stepper motor or servo
Motor.
As shown in figure 35, switch board 600 includes central processing unit 610, power module 620, wireless communication module 630, storage
Battery 640, charging module 650, unmanned plane battery component charger 660, power module 620 is connected with central processing unit 610, nothing
Line communication module 630 is connected with central processing unit 610.Battery 640 is connected with central processing unit 610, and charging module 650 is with storing
Battery 640 is connected.Unmanned plane battery component charger 660 is connected with power module 620.
The drive signal end of central processing unit 610 is connected with stepper motor 320, retractor device 260, central processing unit 610
Power output signal end is connected with electromagnet 550.The drive signal end of central processing unit 610 drives horizontal direction linear with being used for
The motor connection of the linear module 520 of module 510, vertical direction.
The effect of wireless communication module 630 is, receives the landing arriving signal that multi-rotor unmanned aerial vehicle is sent, and by the signal
Send central processing unit 610 to, then the retractor device 260 of the control of central processing unit 610 limiting fixing mechanism 200 is acted.
As shown in figs. 36-38, rack 700 includes cabinet 710 and two pieces of solar panel outer covers 720, two blocks of solar energy
Cell panel outer cover 720 is connected with the top of cabinet 710.In the presence of transmission mechanism, two pieces of solar panel outer covers 720 are closed
Cabinet 710 can be covered in when together, two pieces of solar panel outer covers 720 can be reserved when separating allows unmanned plane to enter
Entrance inside cabinet 710.
The current output terminal of solar panel outer cover 720 is connected with charging module 650, is finally charged to battery 640.
Two pieces of solar panel outer covers 720 can not only provide part electric energy, while may act as weather shield.
During using rack 700, unmanned plane relay is arranged in rack 700.
The course of work of unmanned plane relay is described below：
Under original state, as shown in figure 9, the first V-type clamping plate 210 and the second V-type clamping plate 220 of limiting fixing mechanism 200
Positioned at two relative lateral locations of airplane parking area deck 110.As shown in figure 1, the linear mould of the vertical direction of battery changing mechanism 500
Group 520 is located at the leftmost side, away from airplane parking area 100；Cantilever 530 is located at topmost.With reference to shown in Fig. 1 and 18, the of battery depressed place 300
Two A2, A3 battery cases place full electric battery component (fully charged by battery depressed place 300) below one row battery case group A, most upper
The A1 battery cases in face are empty, and electric battery component is not piled, and two are expired electric battery components towards the direction of cantilever 530.Other two row
Battery case in battery case group B, C places full electric battery component.Secondary series battery case group B is B1 batteries successively from top to bottom
Groove, B2 battery cases, B3 battery cases, the 3rd row battery case group C is C1 battery cases, C2 battery cases, C3 battery cases successively from top to bottom.
The first step：As shown in figure 39, multi-rotor unmanned aerial vehicle 800 is dropped on airplane parking area deck 110, made without electric battery pack
Part is towards battery changing mechanism 500.Under normal circumstances, multi-rotor unmanned aerial vehicle 800 will not just drop to airplane parking area deck 110
Center, multi-rotor unmanned aerial vehicle 800 be located between the first V-type clamping plate 210 and the second V-type clamping plate 220, now many rotors nobody
The undercarriage of machine 800 is not contacted with the first V-type clamping plate 210 and the second V-type clamping plate 220.
Multi-rotor unmanned aerial vehicle 800 sends arriving signal to the wireless communication module 630 of switch board 600, and the signal is transmitted
To central processing unit 610.
Second step：Central processing unit 610 is received after the signal that multi-rotor unmanned aerial vehicle 800 is sent, and spacing fixation is controlled first
Mechanism 200 multi-rotor unmanned aerial vehicle 800 is adjusted in, it is fixed.
Detailed process is that the control retractor device 260 of central processing unit 610 is acted, and the expansion link of retractor device 260, which stretches out, to be pushed away
Dynamic contiguous block 240 is moved to the left in (direction in Fig. 9), and contiguous block 240 drives the first L-type riser 280a by first connecting rod 270a
Moved with the first sliding block 231 to the center of line slideway component 230, while contiguous block 240 drives the by second connecting rod 270b
Two L-type riser 280b and the second sliding block 232 are moved to the center of line slideway component 230.First L-type riser 280a drives first
(the first V-type clamping plate is connected to the center movement of line slideway component 230 for V-type clamping plate connector 290a and the first V-type clamping plate 210
Part 290a is moved along the first guide channel 111), at the same the second L-type riser 280b drive the second V-type clamping plate connector 290b and
(the second V-type clamping plate connector 290b is along the second bullport to the center movement of line slideway component 230 for second V-type clamping plate 220
Move in road 112), that is to say, that the first V-type clamping plate 210 and the second V-type clamping plate 220 are simultaneously to the centre bit on airplane parking area deck 110
Rest against.
As shown in Figure 40 and 41, during the first V-type clamping plate 210 and the movement of the second V-type clamping plate 220, the first V-type folder
Undercarriage 810 of the plate 210 gradually with neighbouring multi-rotor unmanned aerial vehicle 800 is contacted, the second V-type clamping plate 220 also gradually with it is neighbouring
Undercarriage is contacted.As shown in Figure 42 and 43, after the first V-type clamping plate 210 and the second V-type clamping plate 220 are moved a certain distance, the first V
Two hypotenuse undercarriages adjacent with two of the V-type press section 211 of type clamping plate 210 are contacted, while the V of the second V-type clamping plate 220
Two adjacent undercarriages of two hypotenuses and opposite side of type press section are contacted, and so, multi-rotor unmanned aerial vehicle 800 is just adjusted to
The center on airplane parking area deck 110, and be clamped and fixed.
3rd step：After multi-rotor unmanned aerial vehicle 800 is fixed in being adjusted, battery changing mechanism is controlled by central processing unit 610
500 actions, will be removed and placed in battery depressed place 300, then take from battery depressed place 300 in multi-rotor unmanned aerial vehicle 800 without electric battery component
Go out in the battery component insertion multi-rotor unmanned aerial vehicle 800 of full electricity.
Detailed process is, with reference to shown in Fig. 1,4 and 31, and the horizontal direction sliding block on the linear module 510 of horizontal direction drives
The linear module 520 of vertical direction is moved under original state to the direction of multi-rotor unmanned aerial vehicle 800, at the same time, perpendicular directional line
Property module 520 on vertical direction sliding block drive cantilever 530 moved from up to down from original state, thus make on cantilever 530
The electromagnet 550 of connection battery bin location from X-direction to multi-rotor unmanned aerial vehicle 800 move, Z-direction to many rotors without
Man-machine 800 battery bin location movement.In Y direction, the length of cantilever 530 and the installation site of electromagnet 550 are advance
It is good according to Setup Experiments.In a word, in the horizontal direction under the interoperation of linear module 510 and the linear module 520 of vertical direction,
Electromagnet 550 is moved to the battery bin location of multi-rotor unmanned aerial vehicle 800, close to without electric battery component.
When electromagnet 550 is close to battery component, it is powered under the control of central processing unit 610 to electromagnet 550, electromagnetism
Iron 550 is held without the magnet suction piece on electric battery component, then electromagnet 550 linear module 510 and Vertical Square in the horizontal direction
The position of battery depressed place 300 is moved to the interoperation of linear module 520, battery depressed place 300 will be put into without electric battery component hollow
A1 battery cases in (contact pad on contact and battery case without electric battery component, start to charge up), and then to electromagnet
550 power-off, then DM 550 are moved at full electric battery component (below empty A1 battery cases at A2 battery cases), then give
Electromagnet 550 is powered so as to hold electromagnetism suction piece on full electric battery component, then linear module 510 and vertical in the horizontal direction
Under the interoperation of dimension linear module 520, full electric battery component is taken out and the battery compartment of multi-rotor unmanned aerial vehicle 800 is inserted
In.Finally, powered off to electromagnet 550, the linear module 510 of horizontal direction and the linear module 520 of vertical direction is returned to initial bit
Put.
4th step, the expansion link of the retractor device 260 of limiting fixing mechanism 200 is retracted, and makes the first V-type clamping plate 210 and the
Two V-type clamping plates 220 open, and are moved to two sides on airplane parking area deck 110, return to original state.
When change battery component action next time, battery component of the multi-rotor unmanned aerial vehicle without electricity is put into vacant A2
Charged in battery case, take out full electric battery component in A3 battery cases and be put into multi-rotor unmanned aerial vehicle.
When changing battery component next time again, take out multi-rotor unmanned aerial vehicle and vacant A3 battery cases are put into without electric battery component
Interior charging, drives battery to place cylinder 310 and rotates 120 °, by secondary series battery case group B towards electromagnetism by stepper motor 320 afterwards
Iron 550, the full electric battery component taken out in B1 battery cases is put into multi-rotor unmanned aerial vehicle.Afterwards by that analogy.
When the full electric battery component in the 3rd row battery case group C C3 battery cases be removed 3 it is small when (battery component full charge
The maximum time needed) after, unmanned plane battery component charger 660 will be automatically powered off, and save the energy.
It is described above to be not limited to the utility model only to preferred embodiment of the present utility model, for this
For the technical staff in field, the utility model can have various modifications and variations.
Claims (7)
1. a kind of unmanned plane relay, it is characterised in that including airplane parking area, limiting fixing mechanism, battery depressed place and battery altering
Mechanism；
The airplane parking area includes airplane parking area deck and the airplane parking area support frame linked together；
The limiting fixing mechanism includes the first V-type clamping plate, the second V-type clamping plate and relative motion transmission device, first V-type
Clamping plate is provided with the first V-type press section, and the second V-type clamping plate is provided with the second V-type press section；The first V-type clamping plate and the 2nd V
Type clamping plate is connected with relative motion transmission device respectively, and the relative motion transmission device is used to drive the first V-type clamping plate and the
Two V-type clamping plate relative motions；
The first V-type clamping plate and the second V-type clamping plate are oppositely arranged and are located at the top on the airplane parking area deck；
The battery changing mechanism includes the linear module of horizontal direction, the linear module of vertical direction, cantilever and electromagnet, the water
Flat dimension linear module is provided with horizontal direction sliding block, and the linear module of vertical direction is provided with vertical direction sliding block；It is described vertical
The end of dimension linear module is connected with horizontal direction sliding block, and the cantilever is connected with vertical direction sliding block, the electromagnet with
Cantilever is connected；
The battery depressed place is provided with battery case, and the battery depressed place is located between the battery changing mechanism and airplane parking area.
2. unmanned plane relay according to claim 1, it is characterised in that the airplane parking area deck is relative provided with two
The guide channel of setting, is the first guide channel and the second guide channel respectively；
The relative motion transmission device includes line slideway component, contiguous block, retractor device, first connecting rod, second connecting rod, the
One V-type clamping plate connector and the second V-type clamping plate connector；The line slideway component is provided with the first sliding block and the second sliding block, institute
State the first V-type clamping plate to be connected with the first sliding block by the first V-type clamping plate connector, the second V-type clamping plate is pressed from both sides by the second V-type
Plate connector is connected with the second sliding block, and the contiguous block is connected by first connecting rod with the first sliding block, and the contiguous block passes through
Two connecting rods are connected with the second sliding block, and the retractor device is provided with expansion link, and the expansion link is connected with contiguous block；First V
Type clamping plate connector passes through first guide channel, and the second V-type clamping plate connector passes through second guide channel.
3. unmanned plane relay according to claim 1 or 2, it is characterised in that the two ends of the first V-type press section
Rib is connected to, the two ends of the second V-type press section are connected to rib.
4. unmanned plane relay according to claim 3, it is characterised in that the center line of the first V-type press section and
The center line of second V-type press section is on the same line.
5. unmanned plane relay according to claim 2, it is characterised in that the battery depressed place includes battery placing tube
Body, motor, base and connecting shaft；One end of the connecting shaft is placed cylinder with battery and is connected, and the other end passes through bearing and base
Connection；The motor is connected by transmission mechanism with connecting shaft, and the battery places cylinder from top to bottom provided with least one row electricity
Pond groove group, the battery case group is provided with least two battery cases；
The battery case includes housing, back plate, contact and two spring latch locks, and the back plate is connected with the rear end of the housing,
The front opening of the housing, described two spring latch locks are connected to the both sides of housing；The contact and the back plate
Inner side is connected, and the back plate is provided with cable hole.
6. unmanned plane relay according to claim 5, it is characterised in that the battery is placed cylinder and set from top to bottom
It is 120 ° to have the angle between three row battery case groups, adjacent two row battery case group, and each column battery case group is provided with three battery cases.
7. unmanned plane relay according to claim 5, it is characterised in that also including switch board, the switch board bag
Central processing unit, power module and wireless communication module are included, the power module is connected with central processing unit, the wireless telecommunications
Module is connected with central processing unit；The power output signal end of the central processing unit is connected with electromagnet；The center processing
The drive signal end of device is connected with retractor device, motor, the linear module of horizontal direction and the linear module of vertical direction respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720174828.8U CN206485585U (en) | 2017-02-24 | 2017-02-24 | A kind of unmanned plane relay |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720174828.8U CN206485585U (en) | 2017-02-24 | 2017-02-24 | A kind of unmanned plane relay |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206485585U true CN206485585U (en) | 2017-09-12 |
Family
ID=59762379
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720174828.8U Expired - Fee Related CN206485585U (en) | 2017-02-24 | 2017-02-24 | A kind of unmanned plane relay |
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| Country | Link |
|---|---|
| CN (1) | CN206485585U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109118136A (en) * | 2018-07-28 | 2019-01-01 | 江苏苏宁物流有限公司 | A kind of relay station method and system for planning for logistics unmanned plane |
| US10875665B2 (en) | 2017-08-07 | 2020-12-29 | Cainiao Smart Logistics Holding Limited | Aerial vehicle charging method and device |
| CN113859045A (en) * | 2021-11-22 | 2021-12-31 | 北京图维科技有限公司 | Automatic replacing method for vehicle-mounted unmanned aerial vehicle parking apron battery |
-
2017
- 2017-02-24 CN CN201720174828.8U patent/CN206485585U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10875665B2 (en) | 2017-08-07 | 2020-12-29 | Cainiao Smart Logistics Holding Limited | Aerial vehicle charging method and device |
| CN109118136A (en) * | 2018-07-28 | 2019-01-01 | 江苏苏宁物流有限公司 | A kind of relay station method and system for planning for logistics unmanned plane |
| CN109118136B (en) * | 2018-07-28 | 2022-03-29 | 江苏苏宁物流有限公司 | Relay station planning method and system for logistics unmanned aerial vehicle |
| CN113859045A (en) * | 2021-11-22 | 2021-12-31 | 北京图维科技有限公司 | Automatic replacing method for vehicle-mounted unmanned aerial vehicle parking apron battery |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170912 Termination date: 20200224 |