CN105914844A - Multi-dimensional shock-absorbing unmanned aerial vehicle charging station - Google Patents
Multi-dimensional shock-absorbing unmanned aerial vehicle charging station Download PDFInfo
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- 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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- 238000007600 charging Methods 0.000 title claims abstract description 50
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 16
- 238000013016 damping Methods 0.000 claims description 61
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 33
- 238000009434 installation Methods 0.000 claims description 7
- 238000010276 construction Methods 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 10
- 239000013589 supplement Substances 0.000 abstract description 3
- 238000012544 monitoring process Methods 0.000 description 7
- 230000008901 benefit Effects 0.000 description 6
- 230000009977 dual effect Effects 0.000 description 4
- 230000007613 environmental effect Effects 0.000 description 4
- 238000010521 absorption reaction Methods 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 238000007689 inspection Methods 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 241000607479 Yersinia pestis Species 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 201000010099 disease Diseases 0.000 description 1
- 208000037265 diseases, disorders, signs and symptoms Diseases 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
- 230000014616 translation Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- H02J7/0027—
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/0042—Circuit 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
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.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610491286.7A CN105914844B (en) | 2016-06-28 | 2016-06-28 | A kind of multidimensional damping type unmanned plane charging station |
| CN201810359828.4A CN108336798B (en) | 2016-06-28 | 2016-06-28 | Charging station |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610491286.7A CN105914844B (en) | 2016-06-28 | 2016-06-28 | A kind of multidimensional damping type unmanned plane charging station |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810359828.4A Division CN108336798B (en) | 2016-06-28 | 2016-06-28 | Charging station |
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| Publication Number | Publication Date |
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| CN105914844A true CN105914844A (en) | 2016-08-31 |
| CN105914844B CN105914844B (en) | 2018-08-24 |
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| CN201610491286.7A Active CN105914844B (en) | 2016-06-28 | 2016-06-28 | A kind of multidimensional damping type unmanned plane charging station |
| CN201810359828.4A Active CN108336798B (en) | 2016-06-28 | 2016-06-28 | Charging station |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201810359828.4A Active CN108336798B (en) | 2016-06-28 | 2016-06-28 | Charging station |
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| 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 |
| CN106426107B (en) * | 2016-11-15 | 2019-01-25 | 常州大学 | A kind of tensioning integral vibration isolation mechanism |
| 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 |
| EP3828087A4 (en) * | 2018-07-23 | 2022-03-09 | Shanghai Autoflight Co., Ltd. | Landing platform and method for unmanned aerial vehicle, and charging system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108336798A (en) | 2018-07-27 |
| CN108336798B (en) | 2021-09-07 |
| CN105914844B (en) | 2018-08-24 |
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