CN213083524U - Unmanned aerial vehicle power supply basic station with unmanned aerial vehicle descending platform - Google Patents

Unmanned aerial vehicle power supply basic station with unmanned aerial vehicle descending platform Download PDF

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Publication number
CN213083524U
CN213083524U CN202020991291.6U CN202020991291U CN213083524U CN 213083524 U CN213083524 U CN 213083524U CN 202020991291 U CN202020991291 U CN 202020991291U CN 213083524 U CN213083524 U CN 213083524U
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China
Prior art keywords
aerial vehicle
unmanned aerial
platform
groove
power supply
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CN202020991291.6U
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Chinese (zh)
Inventor
张伟
刘俊萌
马杰
冯美玲
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Nanjing Weize Chuangli Electronic Technology Co ltd
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Nanjing Weize Chuangli Electronic Technology Co ltd
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/70Energy storage systems for electromobility, e.g. batteries
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10Technologies relating to charging of electric vehicles
    • Y02T90/14Plug-in electric vehicles

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Abstract

The utility model discloses an unmanned aerial vehicle power supply base station with unmanned aerial vehicle descending platform, including main part and work platform, the inside first cross slot of having seted up of main part, the inside work platform that is provided with of first cross slot, the inside first groove of erecting of having seted up of work platform, the first inslot portion sliding connection that erects has first diaphragm, and the work groove has been seted up to the work platform bottom, a plurality of damping spring of work groove bottom fixedly connected with. The utility model discloses a damping spring drives the motion of second diaphragm, then makes the second diaphragm drive the resistance to compression board, through the resistance to compression board that slides from top to bottom of first spout, the resistance to compression board moves damping spring, through the second slider at the inside horizontal slip of second transverse trough, drives the riser simultaneously through the connecting rod and drives spacing spring, the device possesses secondary buffer structure, the impact force that conveniently brings unmanned aerial vehicle carries out the secondary and unloads the power to the inside part of effectual protection unmanned aerial vehicle does not receive the damage.

Description

Unmanned aerial vehicle power supply basic station with unmanned aerial vehicle descending platform
Technical Field
The utility model relates to an unmanned aerial vehicle descending field, concretely relates to unmanned aerial vehicle power supply base station with unmanned aerial vehicle descending platform.
Background
Unmanned aerial vehicle is an unmanned aircraft, and unmanned aerial vehicle can divide into two kinds, a for military use unmanned aerial vehicle, a civilian unmanned aerial vehicle, along with scientific and technological development, civilian unmanned aerial vehicle slowly gets into in people's the life, and people carry out operations such as high altitude shooting with unmanned aerial vehicle.
However, do not possess unmanned aerial vehicle descending platform when using at current unmanned aerial vehicle power supply basic station, unmanned aerial vehicle descending platform need separately carry when using simultaneously, and it is comparatively troublesome to use to unmanned aerial vehicle descending platform does not possess secondary buffer structure, receives the easy part that damages inside of anti-seismic force when unmanned aerial vehicle descends fast.
Therefore, it is necessary to invent a power supply base station for an unmanned aerial vehicle with an unmanned aerial vehicle landing platform to solve the above problems.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an unmanned aerial vehicle power supply base station with unmanned aerial vehicle descending platform, the current unmanned aerial vehicle descending platform that does not possess, unmanned aerial vehicle descending platform need separately carry when using simultaneously, it is comparatively troublesome to use to unmanned aerial vehicle descending platform does not possess secondary buffer structure, receive the problem that the inside part was damaged easily to the counter-seismic force when unmanned aerial vehicle descends fast, and the unmanned aerial vehicle power supply base station with unmanned aerial vehicle descending platform that provides.
In order to achieve the above object, the present invention provides the following technical solutions: the utility model provides an unmanned aerial vehicle power supply basic station with unmanned aerial vehicle descending platform, includes main part and work platform, first cross slot has been seted up to the main part is inside, the inside work platform that is provided with of first cross slot, the inside first perpendicular groove of having seted up of work platform, first perpendicular inslot portion sliding connection has first diaphragm, and the work groove has been seted up to the work platform bottom, a plurality of damping spring of work tank bottom fixedly connected with, it is a plurality of the second diaphragm is all installed at the damping spring top, the top of second diaphragm is provided with the resistance to compression board, second diaphragm and resistance to compression board closely laminate, the first slider of resistance to compression board both sides fixedly connected with, first slider and first spout sliding connection, the second cross slot has been seted up to the work platform bottom, the inside sliding connection of second cross slot has the second slider.
Preferably, the second slider is provided with two, two second slider one side all is connected with the backup pad, two the inside rotation of backup pad is connected with work bearing, and the benefit convenience of customers who sets up like this passes through.
Preferably, the first transverse plate and the compression-resistant plate are arranged in parallel, and the compression-resistant plate and the working platform are arranged vertically, so that the set advantages are convenient for a user to pass through.
Preferably, two second slider one end all has two connecting rods, the second spout has been seted up to work platform's inside, two connecting rod slidable mounting is inside the second spout, two the connecting rod top is connected with perpendicular piece, two perpendicular piece and third horizontal groove sliding connection.
Preferably, the vertical block top fixedly connected with limit spring, vertical block and second spout sliding connection, the benefit convenience of customers who sets up like this passes through.
Preferably, the wire bin is arranged inside the main body, the number of the wire bins is two, the outer wall of each wire bin is connected with a first bearing, and the first bearings are movably connected with the baffle.
In the technical scheme, the utility model provides a technological effect and advantage:
1. through the first diaphragm of first vertical slot slip, installation damping spring through the work groove of first diaphragm bottom, drive the motion of second diaphragm through damping spring simultaneously, then make the second diaphragm drive the resistance to compression board, thereby when the resistance to compression board meets with gravity, through the resistance to compression board that slides from top to bottom of first spout, resistance to compression board moves damping spring, thereby effectually protect unmanned aerial vehicle, through the second slider in the inside horizontal slip of second horizontal slot, simultaneously through second spout sliding connection pole, the connecting rod drives the riser and drives spacing spring through the connecting rod simultaneously, compared with the prior art, the device possesses secondary buffer structure, the impact force that conveniently brings unmanned aerial vehicle carries out the secondary and unloads the power, thereby the inside part of effectual protection unmanned aerial vehicle does not receive the damage.
2. Drive the line storehouse through the main part, drive the baffle through first bearing simultaneously and rotate, make the line storehouse open to convenience of customers takes the connecting wire from the line storehouse is inside, carries out charging connection through the connector at main part top simultaneously, compares with prior art, and the device connecting wire does not set up inside the device, charges through external connecting wire convenience of customers high-speed joint, has improved the work efficiency of device.
Drawings
In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings needed to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments described in the present invention, and other drawings can be obtained by those skilled in the art according to these drawings.
Fig. 1 is a schematic side view of the cross-sectional structure of the present invention;
FIG. 2 is a schematic side view of the present invention;
FIG. 3 is a schematic view of the front cross-sectional structure of the working platform of the present invention;
fig. 4 is an enlarged schematic structural diagram of a in fig. 3 according to the present invention.
Description of reference numerals:
1. a main body; 2. a first transverse slot; 3. a working platform; 4. a first vertical slot; 5. a first transverse plate; 6. a working groove; 7. a damping spring; 8. a second transverse plate; 9. a pressure resistant plate; 10. a first slider; 11. a first chute; 12. a second transverse groove; 13. a second slider; 14. a support plate; 15. a working bearing; 16. a second chute; 17. a connecting rod; 18. a vertical block; 19. a third transverse groove; 20. a wire bin; 21. a first bearing; 22. and a baffle plate.
Detailed Description
In order to make the technical solution of the present invention better understood by those skilled in the art, the present invention will be further described in detail with reference to the accompanying drawings.
The utility model provides an unmanned aerial vehicle power supply base station with an unmanned aerial vehicle landing platform, as shown in figures 1-4, which comprises a main body 1 and a working platform 3, a first transverse groove 2 is arranged in the main body 1, the working platform 3 is arranged in the first transverse groove 2, a first vertical groove 4 is arranged in the working platform 3, a first transverse plate 5 is connected in the first vertical groove 4 in a sliding way, a working groove 6 is arranged at the bottom of the working platform 3, a plurality of damping springs 7 are fixedly connected at the bottom of the working groove 6, a second transverse plate 8 is arranged at the top of each damping spring 7, a pressure resisting plate 9 is arranged at the top of each second transverse plate 8, the second transverse plate 8 is tightly jointed with the pressure resisting plate 9, a first slide block 10 is fixedly connected at two sides of the pressure resisting plate 9, the first slide block 10 is connected with a first slide groove 11 in a sliding way, a second transverse groove 12 is arranged at the bottom of the working platform, a second sliding block 13 is connected inside the second transverse groove 12 in a sliding manner.
Further, in above-mentioned technical scheme, second slider 13 is provided with two, second spout 16 has been seted up to work platform 3's inside, two second slider 13 one side all is connected with backup pad 14, two the inside rotation of backup pad 14 is connected with work bearing 15, and the benefit convenience of customers who sets up like this passes through work bearing 15 through second slider 13 and drives the motion of backup pad 14, avoids 14 rigidity of backup pad, causes great impact force.
Further, in above-mentioned technical scheme, first diaphragm 5 and resistance to compression board 9 parallel arrangement, resistance to compression board 9 sets up with work platform 3 is perpendicular, and the benefit convenience of customers who sets up like this drives resistance to compression board 9 through first diaphragm 5, places resistance to compression board 9 through work platform 3, and convenience of customers uses.
Further, in above-mentioned technical scheme, two second slider 13 one end all has two connecting rods 17, two connecting rod 17 slidable mounting is inside second spout 16, two connecting rod 17 top is connected with riser 18, two riser 18 and third transverse groove 19 sliding connection, the benefit convenience of customers who sets up like this drives spacing spring motion through connecting rod 17 to the secondary cushions the impact force that the device received.
Further, in the above technical solution, the top of the vertical block 18 is fixedly connected with a limiting spring, and the vertical block 18 is slidably connected with the second sliding groove 16, so that the advantage of the arrangement is that a user can slide the vertical block 18 through the second sliding groove 16, thereby limiting the sliding position.
The implementation mode is specifically as follows: in practical use, the damping spring 7 is installed through the working groove 6 at the bottom of the first transverse plate 5, the second transverse plate 8 is driven to move through the damping spring 7, then the second transverse plate 8 drives the pressure-resistant plate 9, meanwhile, the first slider 10 slides with the first chute 11 by driving the first slider 10, so that when the pressure-resistant plate 9 encounters gravity, the pressure-resistant plate 9 slides up and down through the first chute 11, the pressure-resistant plate 9 drives the damping spring 7, thereby effectively protecting the unmanned aerial vehicle, meanwhile, the support plate 14 rotates through the fixed block at the bottom of the first transverse plate 5, the support plate 14 drives the second slider 13 through the working bearing 15, the second slider 13 slides left and right inside the second transverse groove 12, meanwhile, the connecting rod 17 slides through the second chute 16, the connecting rod 17 drives the vertical block 18, the vertical block 18 drives the third transverse groove 19, thereby, the movable position of the connecting rod 17 is regulated, drive spacing spring through connecting rod 17 simultaneously, the device that exists among the prior art has specifically been solved to this embodiment does not possess secondary buffer structure, leads to unmanned aerial vehicle to descend fast and makes the impaired problem of internals to the device removes the comparatively trouble problem in street.
Further, 1 inside line storehouse 20 of having seted up of main part, line storehouse 20 is provided with two, two 20 outer walls in line storehouse all are connected with first bearing 21, two the equal swing joint baffle 22 of first bearing 21, the benefit convenience of customers who sets up like this opens baffle 22 through first bearing 21 to convenience of customers takes internal connection line, convenient and fast uses.
The implementation mode is specifically as follows: the utility model discloses when the in-service use, drive line storehouse 20 through main part 1, line storehouse 20 drives first bearing 21, and first bearing 21 drives baffle 22 simultaneously and rotates to convenience of customers follows the inside connecting wire of taking in line storehouse 20, installs through the connector at 1 top of main part simultaneously, and this embodiment has specifically solved the unable categorised connecting wire of placing of unmanned aerial vehicle that exists among the prior art, and connects comparatively troublesome problem.
This practical theory of operation:
referring to the attached drawings 1-4 of the specification, when using the device, a user firstly moves the device to a proper position through a handle outside a main body 1, then pulls a working platform 3 through a first transverse groove 2, slides a first transverse plate 5 through a first vertical groove 4, installs a damping spring 7 through a working groove 6 at the bottom of the first transverse plate 5, drives a second transverse plate 8 to move through the damping spring 7, then drives a pressure resisting plate 9 through the second transverse plate 8, simultaneously drives a first sliding block 10, the first sliding block 10 slides with a first sliding groove 11, so that when the pressure resisting plate 9 meets gravity, the pressure resisting plate 9 slides up and down through the first sliding groove 11, the pressure resisting plate 9 drives the damping spring 7, thereby effectively protecting an unmanned aerial vehicle, and simultaneously rotates a supporting plate 14 through a fixed block at the bottom of the first transverse plate 5, the supporting plate 14 drives a second sliding block 13 through a working bearing 15, the second sliding block 13 slides left and right in the second transverse groove 12, the connecting rod 17 slides through the second sliding groove 16, the connecting rod 17 drives the vertical block 18, the vertical block 18 drives the third transverse groove 19, so that the moving position of the connecting rod 17 is regulated, and the connecting rod 17 drives the limiting spring, so that the impact force brought to the unmanned aerial vehicle is conveniently subjected to secondary force unloading, and parts in the unmanned aerial vehicle are effectively protected from being damaged;
referring to specification attached drawing 1-2, when the user need continue a journey to unmanned aerial vehicle and charge, can drive line storehouse 20 through main part 1, line storehouse 20 drives first bearing 21, and first bearing 21 drives baffle 22 simultaneously and rotates to convenience of customers takes the connecting wire from line storehouse 20 inside, installs through the connector at main part 1 top simultaneously, thereby has improved the work efficiency of device.
While certain exemplary embodiments of the present invention have been described above by way of illustration only, it will be apparent to those of ordinary skill in the art that the described embodiments may be modified in various different ways without departing from the spirit and scope of the present invention. Accordingly, the drawings and description are illustrative in nature and should not be construed as limiting the scope of the invention.

Claims (6)

1. The utility model provides an unmanned aerial vehicle power supply basic station with unmanned aerial vehicle descending platform, includes main part (1) and work platform (3), its characterized in that: a first transverse groove (2) is formed in the main body (1), a working platform (3) is arranged in the first transverse groove (2), a first vertical groove (4) is formed in the working platform (3), a first transverse plate (5) is connected in the first vertical groove (4) in a sliding manner, a working groove (6) is formed in the bottom of the working platform (3), a plurality of damping springs (7) are fixedly connected to the bottom of the working groove (6), a second transverse plate (8) is installed at the tops of the damping springs (7), a pressure resisting plate (9) is arranged at the top of the second transverse plate (8), the second transverse plate (8) is tightly attached to the pressure resisting plate (9), first sliding blocks (10) are fixedly connected to two sides of the pressure resisting plate (9), the first sliding blocks (10) are connected with the first sliding grooves (11) in a sliding manner, a second transverse groove (12) is formed in the bottom of the working platform (3), and a second sliding block (13) is connected inside the second transverse groove (12) in a sliding manner.
2. The unmanned aerial vehicle power supply base station with unmanned aerial vehicle landing platform of claim 1, characterized in that: the two second sliding blocks (13) are arranged, one side of each second sliding block (13) is connected with a supporting plate (14), and the two supporting plates (14) are rotatably connected with working bearings (15) inside.
3. The unmanned aerial vehicle power supply base station with unmanned aerial vehicle landing platform of claim 2, characterized in that: the first transverse plate (5) and the pressure resisting plate (9) are arranged in parallel, and the pressure resisting plate (9) is perpendicular to the working platform (3).
4. The unmanned aerial vehicle power supply base station with unmanned aerial vehicle landing platform of claim 2, characterized in that: two second slider (13) one end all has two connecting rods (17), second spout (16) have been seted up to work platform (3) inside, two connecting rod (17) slidable mounting is inside second spout (16), two connecting rod (17) top is connected with riser (18), two riser (18) and third transverse groove (19) sliding connection.
5. The unmanned aerial vehicle power supply base station with unmanned aerial vehicle landing platform of claim 4, characterized in that: the top of the vertical block (18) is fixedly connected with a limiting spring, and the vertical block (18) is connected with the second sliding groove (16) in a sliding mode.
6. The unmanned aerial vehicle power supply base station with unmanned aerial vehicle landing platform of claim 1, characterized in that: the wire bin (20) is arranged inside the main body (1), two wire bins (20) are arranged, the outer walls of the two wire bins (20) are connected with first bearings (21) and two first bearings (21) are movably connected with a baffle (22).
CN202020991291.6U 2020-06-03 2020-06-03 Unmanned aerial vehicle power supply basic station with unmanned aerial vehicle descending platform Active CN213083524U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202020991291.6U CN213083524U (en) 2020-06-03 2020-06-03 Unmanned aerial vehicle power supply basic station with unmanned aerial vehicle descending platform

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202020991291.6U CN213083524U (en) 2020-06-03 2020-06-03 Unmanned aerial vehicle power supply basic station with unmanned aerial vehicle descending platform

Publications (1)

Publication Number Publication Date
CN213083524U true CN213083524U (en) 2021-04-30

Family

ID=75617807

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Application Number Title Priority Date Filing Date
CN202020991291.6U Active CN213083524U (en) 2020-06-03 2020-06-03 Unmanned aerial vehicle power supply basic station with unmanned aerial vehicle descending platform

Country Status (1)

Country Link
CN (1) CN213083524U (en)

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