CN105914844A - Multi-dimensional shock-absorbing unmanned aerial vehicle charging station - Google Patents

Multi-dimensional shock-absorbing unmanned aerial vehicle charging station Download PDF

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Publication number
CN105914844A
CN105914844A CN201610491286.7A CN201610491286A CN105914844A CN 105914844 A CN105914844 A CN 105914844A CN 201610491286 A CN201610491286 A CN 201610491286A CN 105914844 A CN105914844 A CN 105914844A
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CN
China
Prior art keywords
damping
mounting post
trigonid
push rod
electric push
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Granted
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CN201610491286.7A
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Chinese (zh)
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CN105914844B (en
Inventor
吴燕
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Hakda robotics group (Guangzhou) intellectual property Klc Holdings Ltd, Harbin branch
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Anqing Baisite Electronic Technology Co Ltd
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Priority to CN201610491286.7A priority Critical patent/CN105914844B/en
Priority to CN201810359828.4A priority patent/CN108336798B/en
Publication of CN105914844A publication Critical patent/CN105914844A/en
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Publication of CN105914844B publication Critical patent/CN105914844B/en
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    • H02J7/0027
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/0042Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

The invention relates to a multi-dimensional shock-absorbing unmanned aerial vehicle charging station, which comprises shock-absorbing devices, a parking base and a charging device, wherein the parking base is located at the upper parts of the shock-absorbing devices; the parking base is fixedly connected with the shock-absorbing devices; the charging device is located at the upper part of the parking base and comprises a battery box, a lithium battery, a conduit tube, a connecting line and adjustable charging bases; the lithium battery is arranged in the battery box; one end of the conduit tube is fixed at the upper part of the lithium battery; the other end of the conduit tube passes through a round hole in the center position of the parking base; the adjustable charging bases are symmetrically arranged at the front side and the back side of the conduit tube respectively; the lower end of a connecting line is connected with the lithium battery; and the upper end of the connecting line is connected with the adjustable charging bases. The multi-dimensional shock-absorbing unmanned aerial vehicle charging station integrates double shock-absorbing, parking and fixing and multi-station charging, so that the multifunctional effect is achieved; the problems that energy supplement for an unmanned aerial vehicle is difficult and high in cost are solved; the endurance of the unmanned aerial vehicle is improved; and the work capacity of the unmanned aerial vehicle is improved.

Description

A kind of multidimensional damping type unmanned plane charging station
Technical field
The present invention relates to aircraft field, specifically a kind of multidimensional damping type unmanned plane charging station.
Background technology
Aircraft be by the mankind manufacture, can fly away from ground, space flight and by people control in endoatmosphere or exoatmosphere The apparatus flying object flown in space (space), aircraft is divided into airborne vehicle, spacecraft, rocket, guided missile and guided weapon;Nothing Man-machine is also the one of aircraft, and unmanned plane is utilize that radio robot and the presetting apparatus provided for oneself handle the most manned Aircraft, can be divided into depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship from technical standpoint definition With unmanned parasol etc.;Can be divided into military and civilian by application, military aspect unmanned plane is divided into reconnaissance plane and target drone;At present, Unmanned plane can be widely applied to country's ecological environmental protection, aeroplane photography, mapping, mineral resources exploration, the condition of a disaster supervision, traffic Patrol, power-line patrolling, security monitoring, emergent mitigation, emergency command, rain making, national defense safety, land resources exploration, Town planning, seismic survey, environmental monitoring, forest fire protection, Crop Estimation, protection zone wild animal monitoring, air sampling, Maritime affairs scout, border make an inspection tour, the prohibition of drug scouting, fire inspection, ecological environmental protection, marine environmental monitoring, land use survey, Water resources development, crop growth monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, urban planning and municipal administration pipe The fields such as the protection of reason, forest disease and pest and monitoring, digital city.
Unmanned plane belongs to the one of aircraft, unmanned plane have relatively strong, the motion less than normal, popular of compact conformation, build flexibly and The advantages such as flight stability are widely used in civil and military, and the most popular;But unmanned plane faces maximum at present Problem demanding prompt solution is continued a journey exactly, and continuation of the journey decides time and the stability of the flight of unmanned plane, indirectly decides unmanned plane The efficiency of operation and quality, for the energy supplementary question of unmanned plane, military unmanned air vehicle many employings air refuelling solves, due to This kind of supplementary energy mode spends too big, therefore not application on civilian unmanned plane, and civilian unmanned plane is the most also without very well Settling mode, the most also have and set up charging base station the unmanned plane of operation on the way is carried out energy supplement, but current unmanned Machine charging base station exists that damping performance is poor, it is inconvenient to stop, charging needs the problems such as manual operation, in consideration of it, present invention offer A kind of multidimensional damping type unmanned plane charging station.
Summary of the invention
In order to make up the deficiencies in the prior art, the invention provides a kind of multidimensional damping type unmanned plane charging station.
The present invention to solve its technical problem and realize by the following technical solutions.
A kind of multidimensional damping type unmanned plane charging station, including damping device, stops pedestal and charging device;Described stop pedestal Being positioned at directly over damping device, and stop between pedestal and damping device connected, charging device is positioned at above stop pedestal.
Further, described damping device includes lower fixed seat, upper fixed seat, Stewart parallel institution and damping;Institute The Stewart parallel institution stated is between lower fixed seat and upper fixed seat, and Stewart parallel institution lower end and lower fixed seat Being connected, Stewart parallel institution upper end is connected with upper fixed seat, and damping quantity is eight, and damping lays respectively at Outside Stewart parallel institution, and damping is uniformly arranged circumferentially about along the central axis of Stewart parallel institution.
Further, described Stewart parallel institution include fixed platform, moving platform, trigonid, upper Triangulum, spherical hinge, Sleeve, expansion link and limit spring, trigonid and upper Trianguli quantity are three, the number of spherical hinge, sleeve and limit spring Amount is 12, and the quantity of expansion link is six;Described fixed platform and moving platform the most rounded shape structure, trigonid is arranged on fixed On the upper surface of platform, and trigonid on fixed platform in equilateral triangle location arrangements, upper Triangulum is arranged on moving platform lower end On face, and the installation site between upper Triangulum and trigonid is interlocked two-by-two, and trigonid is equilateral triangle column structure, under Triangulum is respectively symmetrically along its vertical center line and is provided with inclined plane, inclined plane offers and matches with spherical hinge lower end external screw thread Installation screwed hole, and upper Trianguli structure is identical with the structure of trigonid;Described spherical hinge is separately mounted to lower triangle On seat and upper Triangulum, sleeve one end is connected with spherical hinge, and the sleeve other end is connected with expansion link, and limit spring is around being enclosed within On expansion link;Stewart parallel institution has that compact conformation, bearing capacity be strong and advantage, the energy in space such as damping performance is good Enough carry out three translations three and rotate the motion in six-freedom degree direction altogether, and it is in parallel to improve Stewart further by limit spring The damping performance of mechanism, it is ensured that the unmanned plane stability when dropping to stop pedestal, jitter is little, shakes when reducing landing The dynamic damage to unmanned aerial vehicle body.
Further, described damping includes mounting post, lower mounting post and damping stage clip;Described upper mounting post and lower peace The dress the most T-shaped structure of post, upper mounting post upper end and lower mounting post lower end be provided with external screw thread respectively, upper mounting post lower end and under Mounting post upper end is provided with lock sleeve respectively, uses the mode of threaded engagement to carry out even between upper mounting post upper end and upper fixed seat Connecing, between lower mounting post lower end and lower fixed seat, the mode also by threaded engagement is attached, and damping stage clip two ends are respectively mounted In upper mounting post lower end and lower mounting post upper end;Damping serves the effect of secondary shock-absorbing to damping device so that damping fills Putting the effect with dual shock absorption, damping performance is greatly improved.
Further, described stop base bottom is octagon slab construction, and stops the left and right sides of pedestal upper surface respectively Symmetry offers semicircle screens groove, the unmanned plane dropped on stop pedestal can be carried out position by semicircle screens groove solid Fixed, the center position stopping pedestal upper surface offers circular hole, and the outside stopping pedestal is provided with surrounding edge, outside surrounding edge successively Being evenly arranged with signal lamp, signal lamp serves the effect at night to position indicating of the present invention.
Further, described charging device includes battery case, lithium battery, conduit, connecting line and adjustable recharging base;Described Lithium battery be arranged in battery case, conduit one end is fixed on above lithium battery, the conduit other end through stop base central The circular hole of position, conduit uses rubber hose, and connecting line and adjustable recharging base quantity are two, and adjustable recharging base divides Not being symmetrically mounted on both sides before and after conduit, connecting line lower end is connected with lithium battery, connecting line upper end and adjustable recharging base phase Connect.
Further, described adjustable recharging base include base plate, lock-screw, longitudinal electric push rod, lifter plate, vertical guide rail, Slide block, transverse electric push rod and charging contact, longitudinal electric push rod, slide block, transverse electric push rod and the number of charging contact Amount is two;Described base plate is fixed on stop pedestal by lock-screw, and longitudinal electric push rod is respectively along the longitudinal direction of base plate Mandrel line is arranged symmetrically in the lock-screw left and right sides, and longitudinal electric push rod bottom is connected with base plate, longitudinal electric push rod top Being connected with lifter plate, vertical guide rail is fixed on lifter plate upper surface, and slide block is arranged on vertical guide rail front, and transverse electric pushes away Bar one end is connected with slide block, and the transverse electric push rod other end is connected with charging contact;Adjustable recharging base is on the vertical plane Highly can regulate, and lateral attitude and lengthwise position all can regulate in the horizontal plane, go for different type of machines unmanned plane Charging, during charging, contraposition is convenient and swift, and uses many chargings contact to charge, and charge efficiency is high.
Compared with prior art, the invention have the advantages that
(1) present invention integrates dual shock absorption, stop is fixing and multistation charges, it is achieved that the effect of one-machine-multi-function, solves The unmanned plane energy supplements difficulty and expends big problem, improves the cruising time of unmanned plane, improves the energy of unmanned plane operation Power.
(2) damping device of the present invention uses Stewart parallel institution and damping, has dual shock absorption effect, and Stewart parallel institution has that compact conformation, bearing capacity be strong and the advantage such as damping performance is good, can carry out three flat in space Move the motion in three rotations six-freedom degree direction altogether, and improved the damping of Stewart parallel institution by limit spring further Performance, it is ensured that the unmanned plane stability when dropping to stop pedestal, jitter is little, and when reducing landing, vibration is to unmanned plane The damage of fuselage.
(3) charging device of the present invention the most highly can regulate, and lateral attitude and lengthwise position are equal in the horizontal plane Can regulate, go for the charging of different type of machines unmanned plane, during charging, contraposition is convenient and swift, and uses many chargings contact Charging, charge efficiency is high.
Accompanying drawing explanation
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the perspective view of the present invention;
Fig. 2 is the perspective view of damping device of the present invention;
Fig. 3 is charging device of the present invention and stops perspective view when pedestal coordinates;
Fig. 4 is the perspective view of Stewart parallel institution of the present invention;
The perspective view of Fig. 5 present invention is adjustable recharging base.
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and be easy to understand with effect, below in conjunction with tool Body illustrates, and the present invention is expanded on further.
As shown in Figures 1 to 5, a kind of multidimensional damping type unmanned plane charging station, including damping device 1, stop pedestal 3 and fill Electric installation 4;Described stop pedestal 3 is positioned at directly over damping device 1, and stops between pedestal 3 and damping device 1 connected, Charging device 4 is positioned at above stop pedestal 3.
As in figure 2 it is shown, described damping device 1 includes lower fixed seat 11, upper fixed seat 12, Stewart parallel institution 13 With damping 14;Described Stewart parallel institution 13 is between lower fixed seat 11 and upper fixed seat 12, and Stewart Parallel institution 13 lower end is connected with lower fixed seat 11, and Stewart parallel institution 13 upper end is connected with upper fixed seat 12, Damping 14 quantity is eight, and damping 14 lays respectively at outside Stewart parallel institution 13, and damping 14 edge The central axis of Stewart parallel institution 13 is uniformly arranged circumferentially about.
As shown in Figure 4, described Stewart parallel institution 13 include fixed platform 131, moving platform 132, trigonid 133, Upper Triangulum 134, spherical hinge 135, sleeve 136, expansion link 137 and limit spring 138, trigonid 133 and upper triangle The quantity of seat 134 is three, and the quantity of spherical hinge 135, sleeve 136 and limit spring 138 is 12, the number of expansion link 137 Amount is six;Described fixed platform 131 and moving platform 132 the most rounded shape structure, trigonid 133 is arranged on fixed platform 131 Upper surface on, and trigonid 133 on fixed platform 131 in equilateral triangle location arrangements, upper Triangulum 134 is arranged on dynamic On platform 132 lower surface, and the installation site between upper Triangulum 134 and trigonid 133 is interlocked two-by-two, trigonid 133 In equilateral triangle column structure, trigonid 133 is respectively symmetrically along its vertical center line and is provided with inclined plane, and inclined plane is offered There is an installation screwed hole matched with spherical hinge 135 lower end external screw thread, and the structure of upper Triangulum 134 and trigonid 133 Structure is identical;Described spherical hinge 135 is separately mounted on trigonid 133 and upper Triangulum 134, sleeve 136 one end with Spherical hinge 135 is connected, and sleeve 136 other end is connected with expansion link 137, and limit spring 138 is around being enclosed within expansion link 137 On;Stewart parallel institution 13 has that compact conformation, bearing capacity be strong and the advantage such as damping performance is good, can enter in space Row three translates the motion in three rotations six-freedom degree direction altogether, and it is in parallel to improve Stewart further by limit spring 138 The damping performance of mechanism 13, it is ensured that the unmanned plane stability when dropping to stop pedestal 3, jitter is little, reduces landing The Shi Zhendong damage to unmanned aerial vehicle body.
As in figure 2 it is shown, described damping 14 includes mounting post 141, lower mounting post 142 and damping stage clip 143;Institute The upper mounting post 141 stated and the lower the most T-shaped structure of mounting post 142, upper mounting post 141 upper end and lower mounting post 142 lower end are equal It is respectively arranged with external screw thread, upper mounting post 141 lower end and lower mounting post 142 upper end and is provided with lock sleeve, upper mounting post respectively The mode using threaded engagement between 141 upper ends and upper fixed seat 12 is attached, lower mounting post 142 lower end and lower fixed seat 11 Between be attached also by the mode of threaded engagement, damping stage clip 143 two ends be separately mounted to mounting post 141 lower end and under Mounting post 142 upper end;Damping 14 serves the effect of secondary shock-absorbing to damping device so that damping device 1 has dual The effect of damping, damping performance is greatly improved.
As it is shown in figure 5, described stop pedestal 3 bottom is octagon slab construction, and stop the left and right of pedestal 3 upper surface Both sides are respectively symmetrically and offer semicircle screens groove, can be to dropping to stop the unmanned plane on pedestal 3 by semicircle screens groove Carrying out position to fix, the center position stopping pedestal 3 upper surface offers circular hole, and the outside stopping pedestal 3 is provided with surrounding edge, Being evenly arranged with signal lamp outside surrounding edge successively, signal lamp serves the effect at night to position indicating of the present invention.
As shown in Figure 3 and Figure 5, described charging device 4 includes battery case 41, lithium battery 42, conduit 43, connecting line 44 and adjustable recharging base 45;Described lithium battery 42 is arranged in battery case 41, and conduit 43 one end is fixed on lithium battery Above in the of 42, conduit 43 other end is through the circular hole of stop pedestal 45 center position, and conduit 43 uses rubber hose, Connecting line 44 and adjustable recharging base 45 quantity are two, and adjustable recharging base 45 is respectively symmetrically before and after being arranged on conduit 43 Both sides, connecting line 44 lower end is connected with lithium battery 42, and connecting line 44 upper end is connected with adjustable recharging base 45.
As shown in Figure 3 and Figure 5, described adjustable recharging base 45 includes that base plate 451, lock-screw 452, longitudinal electric push away Bar 453, lifter plate 454, vertical guide rail 455, slide block 456, transverse electric push rod 457 and charging contact 458, longitudinally The quantity of electric pushrod 453, slide block 456, transverse electric push rod 457 and charging contact 458 is two;Described base plate 451 are fixed on stop pedestal 3 by lock-screw 452, and longitudinal electric push rod 453 is respectively along the longitudinal center of base plate 451 Axisymmetrical is arranged in lock-screw 452 left and right sides, and longitudinal electric push rod 453 bottom is connected with base plate 451, longitudinally electricity Dynamic push rod 453 top is connected with lifter plate 454, and vertical guide rail 455 is fixed on lifter plate 454 upper surface, slide block 456 Being arranged on vertical guide rail 455 front, transverse electric push rod 457 one end is connected with slide block 456, and transverse electric push rod 457 is another One end is connected with charging contact 458;Adjustable recharging base 45 the most highly can regulate, and horizontal in the horizontal plane All can regulate to position and lengthwise position, go for the charging of different type of machines unmanned plane, during charging, contraposition is convenient and swift, And using many chargings contact to charge, charge efficiency is high.
The general principle of the present invention, principal character and advantage have more than been shown and described.Skilled person will appreciate that of the industry, The present invention is not restricted to the described embodiments, the principle that the present invention is simply described of the description in above-described embodiment and specification, Without departing from the spirit and scope, the present invention also has various changes and modifications, and these changes and improvements both fall within In scope of the claimed invention.Claimed scope is defined by appending claims and equivalent thereof.

Claims (3)

1. a multidimensional damping type unmanned plane charging station, it is characterised in that: include damping device, stop pedestal and charging device; Described stop pedestal is positioned at directly over damping device, and stops between pedestal and damping device connected, and charging device is positioned at stop Above pedestal;Wherein:
Described damping device includes lower fixed seat, upper fixed seat, Stewart parallel institution and damping;Described Stewart Parallel institution is between lower fixed seat and upper fixed seat, and Stewart parallel institution lower end is connected with lower fixed seat, Stewart parallel institution upper end is connected with upper fixed seat, and damping quantity is eight, and damping lays respectively at Stewart Outside parallel institution, and damping is uniformly arranged circumferentially about along the central axis of Stewart parallel institution;
Described Stewart parallel institution include fixed platform, moving platform, trigonid, upper Triangulum, spherical hinge, sleeve, Expansion link and limit spring, trigonid and upper Trianguli quantity are three, and the quantity of spherical hinge, sleeve and limit spring is ten Two, the quantity of expansion link is six;Described fixed platform and moving platform the most rounded shape structure, trigonid is arranged on fixed platform On upper surface, and trigonid on fixed platform in equilateral triangle location arrangements, upper Triangulum is arranged on moving platform lower surface, And the installation site between upper Triangulum and trigonid interlocks two-by-two, trigonid is equilateral triangle column structure, trigonid It is respectively symmetrically along its vertical center line and is provided with inclined plane, inclined plane offers the installation matched with spherical hinge lower end external screw thread Screwed hole, and upper Trianguli structure is identical with the structure of trigonid;Described spherical hinge is separately mounted to trigonid and upper On Triangulum, sleeve one end is connected with spherical hinge, and the sleeve other end is connected with expansion link, and limit spring is around being enclosed within expansion link On;
Described charging device includes battery case, lithium battery, conduit, connecting line and adjustable recharging base;Described lithium battery Being arranged in battery case, conduit one end is fixed on above lithium battery, and the conduit other end is through stopping base central position Circular hole, connecting line and adjustable recharging base quantity are two, and adjustable recharging base is respectively symmetrically and is arranged on both sides before and after conduit, Connecting line lower end is connected with lithium battery, and connecting line upper end is connected with adjustable recharging base;
Described adjustable recharging base include base plate, lock-screw, longitudinal electric push rod, lifter plate, vertical guide rail, slide block, Transverse electric push rod and charging contact, the quantity of longitudinal electric push rod, slide block, transverse electric push rod and charging contact is Two;Described base plate is fixed on stop pedestal by lock-screw, and longitudinal electric push rod is respectively along longitudinal center's axis of base plate It is arranged symmetrically in the lock-screw left and right sides, and longitudinal electric push rod bottom is connected with base plate, longitudinal electric push rod top and lifting Plate is connected, and vertical guide rail is fixed on lifter plate upper surface, and slide block is arranged on vertical guide rail front, transverse electric push rod one end Being connected with slide block, the transverse electric push rod other end is connected with charging contact.
A kind of multidimensional damping type unmanned plane charging station the most according to claim 1, it is characterised in that: described damping Including upper mounting post, lower mounting post and damping stage clip;Described upper mounting post and the lower the most T-shaped structure of mounting post, upper mounting post Upper end and lower mounting post lower end are provided with external screw thread, upper mounting post lower end and lower mounting post upper end respectively and are provided with locking respectively Set, uses the mode of threaded engagement to be attached between upper mounting post upper end and upper fixed seat, lower mounting post lower end and lower fixed seat Between be attached also by the mode of threaded engagement, damping stage clip two ends are separately mounted in mounting post lower end and lower mounting post End.
A kind of multidimensional damping type unmanned plane charging station the most according to claim 1, it is characterised in that: described stop pedestal Bottom is octagon slab construction, and the left and right sides stopping pedestal upper surface is respectively symmetrically and offers semicircle screens groove, stops Center position by pedestal upper surface offers circular hole, and the outside stopping pedestal is provided with surrounding edge, the most uniformly sets outside surrounding edge It is equipped with signal lamp.
CN201610491286.7A 2016-06-28 2016-06-28 A kind of multidimensional damping type unmanned plane charging station Active CN105914844B (en)

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CN201810359828.4A CN108336798B (en) 2016-06-28 2016-06-28 Charging station

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CN106737571A (en) * 2016-11-15 2017-05-31 常州大学 A kind of multidimensional vibration reduction tensioning entirety parallel institution
WO2020019109A1 (en) * 2018-07-23 2020-01-30 上海峰飞航空科技有限公司 Landing platform and method for unmanned aerial vehicle, and charging system

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CN103511549A (en) * 2013-08-19 2014-01-15 燕山大学 None-angular displacement parallel damping device
CN203497145U (en) * 2013-08-26 2014-03-26 北京自动化控制设备研究所 Anti-shock device based on Stewart structure
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Publication number Priority date Publication date Assignee Title
CN106426107A (en) * 2016-11-15 2017-02-22 常州大学 Tension overall vibration isolation mechanism
CN106737571A (en) * 2016-11-15 2017-05-31 常州大学 A kind of multidimensional vibration reduction tensioning entirety parallel institution
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WO2020019109A1 (en) * 2018-07-23 2020-01-30 上海峰飞航空科技有限公司 Landing platform and method for unmanned aerial vehicle, and charging system
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