CN105914844B - A kind of multidimensional damping type unmanned plane charging station - Google Patents
A kind of multidimensional damping type unmanned plane charging station Download PDFInfo
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- CN105914844B CN105914844B CN201610491286.7A CN201610491286A CN105914844B CN 105914844 B CN105914844 B CN 105914844B CN 201610491286 A CN201610491286 A CN 201610491286A CN 105914844 B CN105914844 B CN 105914844B
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- push rod
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- 238000013016 damping Methods 0.000 title claims abstract description 62
- 238000007600 charging Methods 0.000 title claims abstract description 47
- 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 abstract description 38
- 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
- 238000009434 installation Methods 0.000 claims description 7
- 230000006835 compression Effects 0.000 claims description 6
- 238000007906 compression Methods 0.000 claims description 6
- 238000010276 construction Methods 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 7
- 230000009977 dual effect Effects 0.000 abstract description 5
- 230000035939 shock Effects 0.000 abstract description 5
- 238000010521 absorption reaction Methods 0.000 abstract description 4
- 239000013589 supplement Substances 0.000 abstract description 4
- 238000012544 monitoring process Methods 0.000 description 8
- 238000010586 diagram Methods 0.000 description 5
- 230000007613 environmental effect Effects 0.000 description 4
- 230000008859 change Effects 0.000 description 2
- 238000013519 translation Methods 0.000 description 2
- 230000014616 translation Effects 0.000 description 2
- 241000607479 Yersinia pestis Species 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
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- 230000007812 deficiency Effects 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
- 238000005516 engineering process Methods 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
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- 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
Abstract
The present invention relates to a kind of multidimensional damping type unmanned plane charging stations, including damping device, stop pedestal and charging unit；The stop pedestal is located at right over damping device, and it stops and is connected between pedestal and damping device, charging unit, which is located at, to be stopped above pedestal, charging unit includes battery case, lithium battery, conduit, connecting line and adjustable recharging base, lithium battery is mounted in battery case, conduit one end is fixed on above lithium battery, the conduit other end passes through the circular hole stopped at base central position, adjustable recharging base is respectively symmetrically mounted on conduit front and rear sides, connecting line lower end is connected with lithium battery, and connecting line upper end is connected with adjustable recharging base.The present invention integrates dual shock absorption, stops the charging of fixed and multistation, realizes the effect of one-machine-multi-function, solves the problems, such as that unmanned plane energy supplement is difficult and it is big to expend, improves the cruise duration of unmanned plane, improve the ability of unmanned machine operation.
Description
Technical field
The present invention relates to aircraft field, a kind of specifically multidimensional damping type unmanned plane charging station.
Background technology
Aircraft is by mankind's manufacture, can fly away from ground, controls in endoatmosphere or big in space flight and by people
The instrument flying object of the gas-bearing formation external space (space) flight, aircraft are divided into aircraft, spacecraft, rocket, guided missile and guided weapon；
Unmanned plane is also one kind of aircraft, and unmanned plane is manipulated not using radio robot and the presetting apparatus provided for oneself
Manned aircraft, from technical standpoint definition can be divided into unmanned helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, nobody
Dirigible and unmanned parasol etc.；By application field can be divided into it is military with it is civilian, military aspect unmanned plane is divided into reconnaissance plane and target drone；
Currently, unmanned plane can be widely applied to national ecological environmental protection, aeroplane photography, mapping, mineral resources exploration, the condition of a disaster monitoring,
Traffic patrolling, 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, the monitoring of protection zone wild animal, air sampling, sea
Thing scouting, border tour, prohibition of drug scouting, fire inspection, ecological environmental protection, marine environmental monitoring, land use survey, water money
It is source exploitation, crop growth monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, urban planning and municipal administration, gloomy
Woods pest and disease damage protects and the fields such as monitoring, digital city.
Unmanned plane belongs to one kind of aircraft, and unmanned plane is with compact-sized, build is less than normal, popular relatively strong, movement spirit
The advantages that living and flight stability, is widely used in civil and military, and quite popular；But current unmanned machine side
It is exactly to continue a journey to face maximum urgent problem to be solved, and continuation of the journey decides time and the stability of the flight of unmanned plane, indirectly determines
The efficiency and quality for unmanned machine operation, for the energy supplementary question of unmanned plane, military unmanned air vehicle mostly uses air refuelling
It solves, since the cost of such supplement energy mode is too big, there is no applying on civilian unmanned plane, civilian unmanned plane is current
Still also without good settling mode, generally also has and charging base station is added to carry out energy supplement to the unmanned plane of operation on the way, but
To be that there are damping performances for current unmanned plane charging base station poor, stops inconvenient, the problems such as needing manual operation of charging, in view of
This, the present invention provides a kind of multidimensional damping type unmanned plane charging stations.
Invention content
In order to make up for the deficiencies of the prior art, the present invention provides a kind of multidimensional damping type unmanned plane charging stations.
The present invention to be solved its technical problem and be realized using following technical scheme.
A kind of multidimensional damping type unmanned plane charging station, including damping device, stop pedestal and charging unit；The stop
Pedestal is located at right over damping device, and stops and be connected between pedestal and damping device, and charging unit, which is located at, to be stopped above pedestal.
Further, the damping device includes lower fixed seat, upper fixed seat, Stewart parallel institutions and damping；
The Stewart parallel institutions are between lower fixed seat and upper fixed seat, and Stewart parallel institutions lower end and lower fixation
Seat is connected, and Stewart parallel institutions upper end is connected with upper fixed seat, and damping quantity is eight, and damping distinguishes position
On the outside of Stewart parallel institutions, and damping is uniformly arranged circumferentially about along the central axis of Stewart parallel institutions.
Further, the Stewart parallel institutions include fixed platform, moving platform, trigonid, upper Triangulum, flexural pivot
Chain, sleeve, telescopic rod and limit spring, trigonid and upper Trianguli quantity is three, spherical hinge, sleeve and limit spring
Quantity is 12, and the quantity of telescopic rod is six；The fixed platform and moving platform structure in rounded shape, trigonid are mounted on
On the upper surface of fixed platform, and trigonid is in equilateral triangle location arrangements on fixed platform, and upper Triangulum is mounted on moving platform
On lower face, and the installation site between upper Triangulum and trigonid is interlocked two-by-two, and trigonid is in equilateral triangle cylinder knot
Structure, trigonid have been symmetrically arranged inclined surface along its vertical center line, are offered on inclined surface and spiral shell outside spherical hinge lower end
The matched installation threaded hole of line, and upper Trianguli structure is identical as the structure of trigonid；The spherical hinge is pacified respectively
On trigonid and upper Triangulum, sleeve one end is connected with spherical hinge, and the sleeve other end is connected with telescopic rod, limit
Spring is around being sleeved on telescopic rod；Stewart parallel institutions have many advantages, such as that compact-sized, bearing capacity is strong and damping performance is good,
The movement in the total six-freedom degree direction of three translations three rotation can be carried out in space, and is further improved by limit spring
The damping performance of Stewart parallel institutions, it is ensured that unmanned plane is dropping to stability when stopping pedestal, and jitter is small, subtracts
Damage of the vibration to unmanned aerial vehicle body when small landing.
Further, the damping includes upper mounting post, lower mounting post and damping compression spring；The upper mounting post and
The lower T-shaped structure of mounting post, upper mounting post upper end and lower mounting post lower end are respectively provided with external screw thread, upper mounting post lower end
It is respectively provided with lock sleeve with lower mounting post upper end, between upper mounting post upper end and upper fixed seat by the way of screw-thread fit
It is attached, is attached also by the mode of screw-thread fit between lower mounting post lower end and lower fixed seat, damping compression spring both ends
It is separately mounted to mounting post lower end and lower mounting post upper end；Damping plays damping device the effect of secondary shock-absorbing,
So that damping device has the effect of that dual shock absorption, damping performance are greatly improved.
Further, the stop base bottom is in octagon slab construction, and stops the left and right two of pedestal upper surface
Side respectively symmetrically offers semicircle screens slot, by semicircle screens slot can to drop to stop pedestal on unmanned plane into
Line position sets fixation, and the center position for stopping pedestal upper surface offers circular hole, stops and is provided with surrounding edge on the outside of pedestal, surrounding edge
Outside is evenly arranged with signal lamp successively, and signal lamp plays the role of at night to position indicating of the present invention.
Further, the charging unit includes battery case, lithium battery, conduit, connecting line and adjustable recharging base；Institute
The lithium battery stated is mounted in battery case, and conduit one end is fixed on above lithium battery, and the conduit other end, which passes through, stops pedestal
The circular hole of center position, conduit use rubber hose, and connecting line and adjustable recharging base quantity are two, adjustable charging base
Seat is respectively symmetrically mounted on conduit front and rear sides, and connecting line lower end is connected with lithium battery, connecting line upper end and adjustable charging
Pedestal is connected.
Further, the adjustable recharging base includes bottom plate, lock-screw, longitudinal electric push rod, lifter plate, vertically leads
Rail, sliding block, transverse electric push rod and charging contact, longitudinal electric push rod, sliding block, transverse electric push rod and charging contact
Quantity is two；The bottom plate is fixed on by lock-screw and is stopped on pedestal, and longitudinal electric push rod is respectively along the vertical of bottom plate
It is arranged symmetrically at left and right sides of lock-screw to central axis, and longitudinal electric push rod bottom end is connected with bottom plate, longitudinal electric pushes away
Bar top is connected with lifter plate, and vertical guide rail is fixed on lifter plate upper surface, and sliding block is mounted in front of vertical guide rail, laterally
Electric pushrod one end is connected with sliding block, and the transverse electric push rod other end is connected with charging contact；Adjustable recharging base exists
Height can be adjusted on vertical plane, and lateral position and lengthwise position can be adjusted in the horizontal plane, can be adapted for difference
The charging of type unmanned plane, when charging, align convenient and efficient, and are charged using more charging contacts, charge efficiency is high.
Compared with prior art, the present invention has the following advantages：
(1) present invention integrates dual shock absorption, stops the charging of fixed and multistation, realizes the effect of one-machine-multi-function,
It solves the problems, such as that unmanned plane energy supplement is difficult and it is big to expend, improves the cruise duration of unmanned plane, improve unmanned plane work
The ability of industry.
(2) damping device of the invention uses Stewart parallel institutions and damping, has dual shock absorption effect, and
Stewart parallel institutions have many advantages, such as that compact-sized, bearing capacity is strong and damping performance is good, and it is flat that three can be carried out in space
The movement in the total six-freedom degree direction of three rotations is moved, and further improves subtracting for Stewart parallel institutions by limit spring
Shock stability, it is ensured that unmanned plane is dropping to stability when stopping pedestal, and jitter is small, and vibration is to nobody when reducing landing
The damage of machine fuselage.
(3) charging unit of the invention can highly be adjusted on the vertical plane, and lateral position and longitudinal direction in the horizontal plane
Position can be adjusted, and can be adapted for the charging of different type of machines unmanned plane, when charging align it is convenient and efficient, and using more chargings
Contact head charges, and charge efficiency is high.
Description of the drawings
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is the dimensional structure diagram of the present invention；
Fig. 2 is the dimensional structure diagram of damping device of the present invention；
Dimensional structure diagram when Fig. 3 is charging unit of the present invention and stop pedestal cooperation；
Fig. 4 is the dimensional structure diagram of Stewart parallel institutions of the present invention；
The dimensional structure diagram of Fig. 5 adjustable recharging bases of the invention.
Specific implementation mode
In order to make the technical means, the creative features, the aims and the efficiencies achieved by the present invention be easy to understand, tie below
Conjunction is specifically illustrating, and the present invention is further explained.
As shown in Figures 1 to 5, a kind of multidimensional damping type unmanned plane charging station, including damping device 1, stop and pedestal 3 and fill
Electric installation 4；The stop pedestal 3 is located at right over damping device 1, and stops and be connected between pedestal 3 and damping device 1, fills
Electric installation 4, which is located at, stops 3 top of pedestal.
As shown in Fig. 2, the damping device 1 includes lower fixed seat 11, upper fixed seat 12, Stewart parallel institutions 13
With damping 14；The Stewart parallel institutions 13 are between lower fixed seat 11 and upper fixed seat 12, and Stewart
13 lower end of parallel institution is connected with lower fixed seat 11, and 13 upper end of Stewart parallel institutions is connected with upper fixed seat 12, damping
14 quantity of mechanism is eight, and damping 14 is located at 13 outside of Stewart parallel institutions, and damping 14 is along Stewart
The central axis of parallel institution 13 is uniformly arranged circumferentially about.
As shown in figure 4, the Stewart parallel institutions 13 include fixed platform 131, moving platform 132, trigonid 133,
Upper Triangulum 134, spherical hinge 135, sleeve 136, telescopic rod 137 and limit spring 138, trigonid 133 and upper Triangulum 134
Quantity be three, the quantity of spherical hinge 135, sleeve 136 and limit spring 138 is 12, and the quantity of telescopic rod 137 is six；Institute
Fixed platform 131 and moving platform 132 structure in rounded shape stated, trigonid 133 are mounted on the upper surface of fixed platform 131,
And trigonid 133 is in equilateral triangle location arrangements on fixed platform 131, upper Triangulum 134 is mounted on 132 lower face of moving platform
On, and the installation site between upper Triangulum 134 and trigonid 133 is interlocked two-by-two, trigonid 133 is in equilateral triangle cylinder
Structure, trigonid 133 have been symmetrically arranged inclined surface along its vertical center line, are offered on inclined surface and spherical hinge 135
The matched installation threaded hole of lower end external screw thread, and the structure of upper Triangulum 134 is identical as the structure of trigonid 133；It is described
Spherical hinge 135 be separately mounted to 134 on trigonid 133 and upper Triangulum, 136 one end of sleeve is connected with spherical hinge 135,
136 other end of sleeve is connected with telescopic rod 137, and limit spring 138 is around being sleeved on telescopic rod 137；Stewart parallel institutions 13
Have many advantages, such as that compact-sized, bearing capacity is strong and damping performance is good, three translations three rotation totally six can be carried out in space
The movement of freedom degree direction, and the damping performance of Stewart parallel institutions 13 is further improved by limit spring 138, really
It has protected unmanned plane and has dropped to stability when stopping pedestal 3, jitter is small, and vibration is to unmanned aerial vehicle body when reducing landing
Damage.
As shown in Fig. 2, the damping 14 includes upper mounting post 141, lower mounting post 142 and damping compression spring 143；Institute
The 142 T-shaped structure of upper mounting post 141 and lower mounting post stated, 141 upper end of upper mounting post and lower 142 lower end of mounting post are divided equally
It is not provided with external screw thread, 141 lower end of upper mounting post and lower 142 upper end of mounting post are respectively provided with lock sleeve, upper mounting post 141
Be attached by the way of screw-thread fit between upper end and upper fixed seat 12, lower 142 lower end of mounting post and lower fixed seat 11 it
Between be attached also by the mode of screw-thread fit, 143 both ends of damping compression spring are separately mounted to 141 lower end of mounting post and lower peace
Fill 142 upper end of column；Damping 14 plays damping device the effect of secondary shock-absorbing so that damping device 1 has dual subtract
The effect of shake, damping performance are greatly improved.
As shown in figure 5,3 bottom end of stop pedestal is in octagon slab construction, and stop a left side for 3 upper surface of pedestal
Right both sides respectively symmetrically offer semicircle screens slot, can be to dropping to the nothing stopped on pedestal 3 by semicircle screens slot
Man-machine carry out position is fixed, and the center position for stopping 3 upper surface of pedestal offers circular hole, and the outside for stopping pedestal 3 is provided with
Surrounding edge, surrounding edge outside are evenly arranged with signal lamp successively, and signal lamp plays the role of at night to position indicating of the present invention.
As shown in Figure 3 and Figure 5, the charging unit 4 includes battery case 41, lithium battery 42, conduit 43, connecting line 44
With adjustable recharging base 45；The lithium battery 42 is mounted in battery case 41, and 43 one end of conduit is fixed on lithium battery 42
Side, 43 other end of conduit pass through the circular hole for stopping 45 center position of pedestal, conduit 43 to use rubber hose, connecting line 44
It is two with 45 quantity of adjustable recharging base, adjustable recharging base 45 is respectively symmetrically mounted on 43 front and rear sides of conduit, connection
44 lower end of line is connected with lithium battery 42, and 44 upper end of connecting line is connected with adjustable recharging base 45.
As shown in Figure 3 and Figure 5, the adjustable recharging base 45 is pushed away including bottom plate 451, lock-screw 452, longitudinal electric
Bar 453, lifter plate 454, vertical guide rail 455, sliding block 456, transverse electric push rod 457 and charging contact 458, longitudinal electric pushes away
Bar 453, sliding block 456, transverse electric push rod 457 and charging contact 458 quantity be two；The bottom plate 451 passes through lock
Tight screw 452, which is fixed on, to be stopped on pedestal 3, and longitudinal center axis of the longitudinal electric push rod 453 respectively along bottom plate 451 is arranged symmetrically
In 452 left and right sides of lock-screw, and 453 bottom end of longitudinal electric push rod is connected with bottom plate 451,453 top of longitudinal electric push rod
It is connected with lifter plate 454, vertical guide rail 455 is fixed on 454 upper surface of lifter plate, and sliding block 456 is mounted on vertical guide rail 455
Front, 457 one end of transverse electric push rod are connected with sliding block 456,457 other end of transverse electric push rod and charging contact 458
It is connected；Height can be adjusted adjustable recharging base 45 on the vertical plane, and lateral position and lengthwise position are equal in the horizontal plane
It can adjust, can be adapted for the charging of different type of machines unmanned plane, when charging aligns convenient and efficient, and uses more charging contacts
Charging, charge efficiency are high.
The basic principles, main features and advantages of the invention have been shown and described above.The technical staff of the industry should
Understand, the present invention is not limited to the above embodiments, and the description in above embodiments and description only illustrates the present invention
Principle, without departing from the spirit and scope of the present invention, various changes and improvements may be made to the invention, these change and change
Into all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its equivalent
It defines.
Claims (1)
1. a kind of multidimensional damping type unmanned plane charging station, it is characterised in that：Including damping device, stop pedestal and charging unit；
The stop pedestal is located at right over damping device, and stops and be connected between pedestal and damping device, and charging unit, which is located at, to stop
Above pedestal；Wherein：
The damping device includes lower fixed seat, upper fixed seat, Stewart parallel institutions and damping；Described
Stewart parallel institutions are between lower fixed seat and upper fixed seat, and Stewart parallel institutions lower end is connected with lower fixed seat
It connects, Stewart parallel institutions upper end is connected with upper fixed seat, and damping quantity is eight, and damping is located at
On the outside of Stewart parallel institutions, and damping is uniformly arranged circumferentially about along the central axis of Stewart parallel institutions；
The Stewart parallel institutions include fixed platform, moving platform, trigonid, upper Triangulum, spherical hinge, sleeve, stretch
Bar and limit spring, trigonid and upper Trianguli quantity are three, and the quantity of spherical hinge, sleeve and limit spring is 12,
The quantity of telescopic rod is six；The fixed platform and moving platform structure in rounded shape, trigonid are mounted on the upper of fixed platform
On end face, and trigonid is in equilateral triangle location arrangements on fixed platform, and upper Triangulum is mounted on moving platform lower face, and
Installation site between upper Triangulum and trigonid is interlocked two-by-two, and trigonid is in equilateral triangle column structure, trigonid
It has been symmetrically arranged inclined surface along its vertical center line, has been offered on inclined surface and the matched peace of spherical hinge lower end external screw thread
Threaded hole is filled, and upper Trianguli structure is identical as the structure of trigonid；The spherical hinge is separately mounted to trigonid
On upper Triangulum, sleeve one end is connected with spherical hinge, and the sleeve other end is connected with telescopic rod, and limit spring is stretched around being sleeved on
On contracting bar；
The charging unit includes battery case, lithium battery, conduit, connecting line and adjustable recharging base；The lithium battery
In battery case, conduit one end is fixed on above lithium battery, and the conduit other end, which passes through, to be stopped at base central position
Circular hole, connecting line and adjustable recharging base quantity are two, adjustable recharging base respectively symmetrically be mounted on conduit before and after two
Side, connecting line lower end are connected with lithium battery, and connecting line upper end is connected with adjustable recharging base；
The adjustable recharging base includes bottom plate, lock-screw, longitudinal electric push rod, lifter plate, vertical guide rail, sliding block, cross
To electric pushrod and charging contact, longitudinal electric push rod, sliding block, transverse electric push rod and charging contact quantity be
Two；The bottom plate is fixed on by lock-screw and is stopped on pedestal, and longitudinal electric push rod is respectively along the vertical central axis of bottom plate
Line is arranged symmetrically at left and right sides of lock-screw, and longitudinal electric push rod bottom end is connected with bottom plate, longitudinal electric push rod top with
Lifter plate is connected, and vertical guide rail is fixed on lifter plate upper surface, and sliding block is mounted in front of vertical guide rail, transverse electric push rod
One end is connected with sliding block, and the transverse electric push rod other end is connected with charging contact；
The damping includes upper mounting post, lower mounting post and damping compression spring；The upper mounting post and lower mounting post are equal
T-shaped structure, upper mounting post upper end and lower mounting post lower end are respectively provided with external screw thread, upper mounting post lower end and lower mounting post
Upper end is respectively provided with lock sleeve, is attached by the way of screw-thread fit between upper mounting post upper end and upper fixed seat,
It is attached also by the mode of screw-thread fit between lower mounting post lower end and lower fixed seat, damping compression spring both ends are separately mounted to
Upper mounting post lower end and lower mounting post upper end；
The stop base bottom is in octagon slab construction, and the left and right sides for stopping pedestal upper surface is respectively symmetrically opened
Equipped with semicircle screens slot, the center position for stopping pedestal upper surface offers circular hole, stops to be provided on the outside of pedestal and enclose
Side, surrounding edge outside are evenly arranged with signal lamp successively.
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 |
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| 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 CN105914844A (en) | 2016-08-31 |
| CN105914844B true CN105914844B (en) | 2018-08-24 |
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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 |
| CN201610491286.7A Active 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 |
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| CN201810359828.4A Active CN108336798B (en) | 2016-06-28 | 2016-06-28 | Charging station |
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Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106426107B (en) * | 2016-11-15 | 2019-01-25 | 常州大学 | A kind of tensioning integral vibration isolation mechanism |
| CN106737571B (en) * | 2016-11-15 | 2019-02-12 | 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 |
| CN110254737B (en) * | 2019-06-21 | 2021-02-05 | 燕山大学 | Multifunctional unmanned aerial vehicle comprehensive management platform and control method thereof |
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| CN202271897U (en) * | 2011-07-06 | 2012-06-13 | 珠海银通新能源有限公司 | Service guarantee vehicle for field operation of electric unmanned helicopter |
| 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 |
| CN104029711A (en) * | 2014-06-25 | 2014-09-10 | 王松豪 | Multi-dimensional shock-absorbing baby carriage |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204776052U (en) * | 2015-06-26 | 2015-11-18 | 哈瓦国际航空技术（深圳）有限公司 | Damping structure of cloud platform |
| CN106712160B (en) * | 2015-07-30 | 2019-05-21 | 安徽啄木鸟无人机科技有限公司 | A kind of charging method of unmanned plane quick charging system |
| CN205168939U (en) * | 2015-10-12 | 2016-04-20 | 西北农林科技大学 | Stationary vane VTOL unmanned aerial vehicle automated inspection platform that takes off and land |
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- 2016-06-28 CN CN201810359828.4A patent/CN108336798B/en active Active
- 2016-06-28 CN CN201610491286.7A patent/CN105914844B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202271897U (en) * | 2011-07-06 | 2012-06-13 | 珠海银通新能源有限公司 | Service guarantee vehicle for field operation of electric unmanned helicopter |
| 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 |
| CN104029711A (en) * | 2014-06-25 | 2014-09-10 | 王松豪 | Multi-dimensional shock-absorbing baby carriage |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105914844A (en) | 2016-08-31 |
| CN108336798B (en) | 2021-09-07 |
| CN108336798A (en) | 2018-07-27 |
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Effective date of registration: 20180720 Address after: 150000 Lake Jingpo, Heilongjiang Province, Harbin, Dalian Road North Applicant after: Hakda robotics group (Guangzhou) intellectual property Klc Holdings Ltd, Harbin branch Address before: 246001 third floor, 3 building complex, Xinzhou Town, Yingjiang District, Anqing, Anhui Applicant before: Anqing Baisite Electronic Technology Co., Ltd. |
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