CN108336798B - Charging station - Google Patents
Charging station Download PDFInfo
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- CN108336798B CN108336798B CN201810359828.4A CN201810359828A CN108336798B CN 108336798 B CN108336798 B CN 108336798B CN 201810359828 A CN201810359828 A CN 201810359828A CN 108336798 B CN108336798 B CN 108336798B
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- 238000013016 damping Methods 0.000 claims abstract description 56
- 238000003032 molecular docking Methods 0.000 claims abstract description 21
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 15
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 15
- 230000035939 shock Effects 0.000 claims abstract description 9
- 238000010521 absorption reaction Methods 0.000 claims abstract description 8
- 230000007246 mechanism Effects 0.000 claims description 47
- 230000000694 effects Effects 0.000 abstract description 8
- 238000012544 monitoring process Methods 0.000 description 8
- 230000008901 benefit Effects 0.000 description 6
- 239000013589 supplement Substances 0.000 description 3
- 238000013519 translation Methods 0.000 description 3
- 241000282414 Homo sapiens Species 0.000 description 2
- 230000009977 dual effect Effects 0.000 description 2
- 238000011835 investigation Methods 0.000 description 2
- 230000033001 locomotion Effects 0.000 description 2
- 230000014616 translation Effects 0.000 description 2
- 241001465754 Metazoa Species 0.000 description 1
- 241000607479 Yersinia pestis Species 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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Classifications
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- 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 invention relates to a charging station, which comprises a damping device, a parking base and a charging device, wherein the damping device is arranged on the parking base; the utility model discloses a charging device, including docking base, storage battery, conduit, connecting wire, base, damping device, charging device, lead pipe, connecting wire, adjustable charging base, the base is located directly over damping device, and dock between base and the damping device and link firmly, charging device is located the base top of docking, charging device lithium cell, conduit, connecting wire and adjustable charging base, conduit one end is fixed in the lithium cell top, the conduit other end passes the up end of docking the base, adjustable charging base is symmetrical respectively and installs both sides around the conduit, the connecting wire lower extreme is connected with the lithium cell, the connecting wire upper end is connected with adjustable charging base. The invention integrates double shock absorption, stop fixing and multi-station charging, realizes the effect of one machine with multiple functions, solves the problems of difficult energy supply and large consumption of the unmanned aerial vehicle, improves the endurance time of the unmanned aerial vehicle and improves the operation capability of the unmanned aerial vehicle.
Description
The application is a divisional application of a patent with the application number of 2016104912867 and the application date of 2016, 06 and 28, and the invention creates a multi-dimensional damping type unmanned aerial vehicle charging station.
Technical Field
The invention relates to the field of aircrafts, in particular to a multi-dimensional damping type unmanned aerial vehicle charging station.
Background
The aircraft is an apparatus flyer which is manufactured by human beings, can fly off the ground, flies in space and is controlled by the human beings to fly in the atmosphere or in the space (outer space), and the aircraft is divided into an aircraft, a spacecraft, a rocket, a missile and a guided weapon; the unmanned aerial vehicle is also one of aircrafts, is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, and can be divided into an unmanned helicopter, an unmanned fixed wing aircraft, an unmanned multi-rotor aircraft, an unmanned airship, an unmanned parachute wing aircraft and the like from the technical perspective; the unmanned aerial vehicle can be divided into military and civil according to the application field, and the unmanned aerial vehicle can be divided into a reconnaissance plane and a target drone in the aspect of military; at present, unmanned aerial vehicles can be widely applied to the fields of national ecological environment protection, aerial photography, mapping, mineral resource exploration, disaster monitoring, traffic patrol, power line patrol, public security monitoring, emergency disaster reduction, emergency command, artificial rainfall, national defense safety, national soil resource exploration, town planning, earthquake investigation, environmental monitoring, forest fire prevention, crop assessment, wild animal monitoring in protected areas, atmospheric sampling, maritime reconnaissance, border patrol, poison-forbidden reconnaissance, fire reconnaissance, ecological environment protection, marine environment monitoring, land utilization investigation, water resource development, crop growth monitoring and assessment, agricultural operation, natural disaster monitoring and assessment, urban planning and municipal management, forest pest protection and monitoring, digital cities and the like.
The unmanned aerial vehicle belongs to one type of aircrafts, and has the advantages of compact structure, small size, strong popularization, flexible movement, stable flight and the like, is widely applied to civilian use and military use, and is popular with the public; however, the present unmanned aerial vehicle is faced with the problem to be solved most urgently, namely, endurance, which determines flight time and stability of the unmanned aerial vehicle, indirectly determines operation efficiency and quality of the unmanned aerial vehicle, and for energy supplement of the unmanned aerial vehicle, military unmanned aerial vehicles mostly adopt aerial refueling to solve the problem, because the energy supplement mode is too expensive, the unmanned aerial vehicle is not applied to civil unmanned aerial vehicles, the civil unmanned aerial vehicles still have no good solution at present, and generally a charging base station is added to supplement energy for the unmanned aerial vehicle operating along the way.
Disclosure of Invention
In order to make up for the defects of the prior art, the invention provides a multi-dimensional damping type unmanned aerial vehicle charging station. The technical problem to be solved by the invention is realized by adopting the following technical scheme.
A multi-dimensional damping type unmanned aerial vehicle charging station comprises a damping device, a parking base and a charging device; the parking base is located right above the damping device and fixedly connected with the damping device, and the charging device is located above the parking base.
Further, the damping device comprises a lower fixed seat, an upper fixed seat, a Stewart parallel mechanism and a damping mechanism; the Stewart parallel mechanism is located between the lower fixing seat and the upper fixing seat, the lower end of the Stewart parallel mechanism is connected with the lower fixing seat, the upper end of the Stewart parallel mechanism is connected with the upper fixing seat, the number of the damping mechanisms is eight, the damping mechanisms are respectively located on the outer sides of the Stewart parallel mechanism, and the damping mechanisms are uniformly arranged in a circumferential mode along the central axis of the Stewart parallel mechanism.
Further, the Stewart parallel mechanism comprises a fixed platform, a movable platform, a lower triangular seat, an upper triangular seat, a spherical hinge, a sleeve, a telescopic rod and a limiting spring, wherein the number of the lower triangular seat and the upper triangular seat is three, the number of the spherical hinge, the sleeve and the limiting spring is twelve, and the number of the telescopic rod is six; the lower triangular seats are arranged on the upper end surface of the fixed platform and are arranged in regular triangle positions on the fixed platform, the upper triangular seats are arranged on the lower end surface of the movable platform, the mounting positions between the upper triangular seats and the lower triangular seats are staggered in pairs, the lower triangular seats are in regular triangle cylinder structures, the lower triangular seats are respectively and symmetrically provided with inclined planes along the vertical center line of the lower triangular seats, mounting threaded holes matched with external threads at the lower ends of the ball hinges are formed in the inclined planes, and the structures of the upper triangular seats are the same as those of the lower triangular seats; the ball hinge is respectively arranged on the lower triangular seat and the upper triangular seat, one end of the sleeve is connected with the ball hinge, the other end of the sleeve is connected with the telescopic rod, and the limiting spring is wound on the telescopic rod; the Stewart parallel mechanism has the advantages of compact structure, strong bearing capacity, good damping performance and the like, can move in the space in six degrees of freedom in three-translation and three-rotation directions, further improves the damping performance of the Stewart parallel mechanism through the limiting spring, ensures the stability of the unmanned aerial vehicle when the unmanned aerial vehicle descends to a parking base, has small jitter, and reduces the damage of the vibration to the unmanned aerial vehicle body when the unmanned aerial vehicle descends.
Furthermore, the damping mechanism comprises an upper mounting column, a lower mounting column and a damping pressure spring; the upper mounting column and the lower mounting column are both of T-shaped structures, the upper end of the upper mounting column and the lower end of the lower mounting column are respectively provided with external threads, the lower end of the upper mounting column and the upper end of the lower mounting column are respectively provided with a locking sleeve, the upper end of the upper mounting column is connected with the upper fixing seat in a thread fit mode, the lower end of the lower mounting column is connected with the lower fixing seat in a thread fit mode, and two ends of a damping pressure spring are respectively mounted at the lower end of the upper mounting column and the upper end of the lower mounting column; the damping mechanism has a secondary damping effect on the damping device, so that the damping device has a dual damping effect, and the damping performance is greatly improved.
Further, the bottom end of the docking base is of a regular octagonal flat plate structure, the left side and the right side of the upper end face of the docking base are symmetrically provided with semicircular clamping grooves respectively, the unmanned aerial vehicle landing on the docking base can be fixed in position through the semicircular clamping grooves, the center of the upper end face of the docking base is provided with a round hole, the outer side of the docking base is provided with a surrounding edge, signal lamps are uniformly arranged on the outer side of the surrounding edge in sequence, and the signal lamps play a role in prompting the position of the unmanned aerial vehicle at night.
Furthermore, the charging device comprises a battery box, a lithium battery, a wire conduit, a connecting wire and an adjustable charging base; the lithium cell install in the battery box, conduit one end is fixed in the lithium cell top, the conduit other end passes the round hole of berthhing base central point department of putting, the conduit adopts flexible rubber hose, connecting wire and adjustable charging base quantity are two, adjustable charging base symmetry respectively installs both sides around the conduit, the connecting wire lower extreme is connected with the lithium cell, the connecting wire upper end is connected with adjustable charging base.
Furthermore, the adjustable charging base comprises a bottom plate, a locking screw, a longitudinal electric push rod, a lifting plate, a vertical guide rail, a sliding block, a transverse electric push rod and charging contact heads, wherein the number of the longitudinal electric push rod, the number of the sliding block, the number of the transverse electric push rod and the number of the charging contact heads are two; the bottom plate is fixed on the parking base through a locking screw, the longitudinal electric push rods are symmetrically arranged on the left side and the right side of the locking screw along the longitudinal central axis of the bottom plate respectively, the bottom ends of the longitudinal electric push rods are fixedly connected with the bottom plate, the top ends of the longitudinal electric push rods are connected with the lifting plate, the vertical guide rail is fixed on the upper end surface of the lifting plate, the sliding block is installed in front of the vertical guide rail, one end of the transverse electric push rod is connected with the sliding block, and the other end of the transverse electric push; the adjustable base that charges highly can be adjusted on the perpendicular, and horizontal position and vertical position all can be adjusted on the horizontal plane, can be applicable to charging of different model unmanned aerial vehicle, and counterpoint convenient and fast when charging, and adopt many charging contact to charge, and charging efficiency is high.
Compared with the prior art, the invention has the following advantages:
(1) the invention integrates double shock absorption, stop fixing and multi-station charging, realizes the effect of one machine with multiple functions, solves the problems of difficult energy supply and large consumption of the unmanned aerial vehicle, improves the endurance time of the unmanned aerial vehicle and improves the operation capability of the unmanned aerial vehicle.
(2) The shock absorption device provided by the invention adopts the Stewart parallel mechanism and the shock absorption mechanism, has double shock absorption effects, and the Stewart parallel mechanism has the advantages of compact structure, strong bearing capacity, good shock absorption performance and the like, can move in six freedom directions of three translation and three rotation in space, further improves the shock absorption performance of the Stewart parallel mechanism through the limiting spring, ensures the stability of the unmanned aerial vehicle when the unmanned aerial vehicle lands on a parking base, has small jitter, and reduces the damage of the vibration to the unmanned aerial vehicle body when the unmanned aerial vehicle lands.
(3) The height of the charging device on the vertical plane can be adjusted, the horizontal position and the longitudinal position on the horizontal plane can be adjusted, the charging device can be suitable for charging unmanned aerial vehicles of different types, the alignment is convenient and quick during charging, multiple charging contacts are adopted for charging, and the charging efficiency is high.
Drawings
The invention is further illustrated with reference to the following figures and examples.
FIG. 1 is a schematic perspective view of the present invention;
FIG. 2 is a schematic perspective view of the shock absorbing device of the present invention;
FIG. 3 is a schematic perspective view of the charging device of the present invention mated with a docking station;
fig. 4 is a schematic perspective view of the Stewart parallel mechanism of the present invention;
fig. 5 is a schematic perspective view of an adjustable charging base according to the present invention.
Detailed Description
In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further explained below by combining the specific drawings.
As shown in fig. 1 to 5, a multi-dimensional damping type unmanned aerial vehicle charging station comprises a damping device 1, a parking base 3 and a charging device 4; the parking base 3 is located right above the damping device 1, the parking base 3 and the damping device 1 are fixedly connected, and the charging device 4 is located above the parking base 3.
As shown in fig. 2, the damping device 1 includes a lower fixing seat 11, an upper fixing seat 12, a Stewart parallel mechanism 13 and a damping mechanism 14; the Stewart parallel mechanism 13 is located between the lower fixed seat 11 and the upper fixed seat 12, the lower end of the Stewart parallel mechanism 13 is connected with the lower fixed seat 11, the upper end of the Stewart parallel mechanism 13 is connected with the upper fixed seat 12, the number of the damping mechanisms 14 is eight, the damping mechanisms 14 are respectively located on the outer sides of the Stewart parallel mechanism 13, and the damping mechanisms 14 are uniformly and circumferentially arranged along the central axis of the Stewart parallel mechanism 13.
As shown in fig. 4, the Stewart parallel mechanism 13 includes a fixed platform 131, a movable platform 132, a lower triangular seat 133, an upper triangular seat 134, a ball hinge 135, a sleeve 136, a telescopic rod 137 and a limit spring 138, the number of the lower triangular seat 133 and the upper triangular seat 134 is three, the number of the ball hinge 135, the number of the sleeve 136 and the number of the limit spring 138 are twelve, and the number of the telescopic rod 137 is six; the fixed platform 131 and the movable platform 132 are both circular structures, the lower triangular seats 133 are arranged on the upper end face of the fixed platform 131, the lower triangular seats 133 are arranged on the fixed platform 131 in regular triangle positions, the upper triangular seats 134 are arranged on the lower end face of the movable platform 132, the mounting positions between the upper triangular seats 134 and the lower triangular seats 133 are staggered in pairs, the lower triangular seats 133 are in regular triangle cylinder structures, inclined planes are symmetrically arranged on the lower triangular seats 133 along the vertical center line of the lower triangular seats 133 respectively, mounting threaded holes matched with the external threads at the lower ends of the ball hinges 135 are formed in the inclined planes, and the structures of the upper triangular seats 134 and the lower triangular seats 133 are the same; the ball hinge 135 is respectively arranged on the lower triangular seat 133 and the upper triangular seat 134, one end of the sleeve 136 is connected with the ball hinge 135, the other end of the sleeve 136 is connected with the telescopic rod 137, and the limiting spring 138 is wound on the telescopic rod 137; stewart parallel mechanism 13 has compact structure, bearing capacity is strong and shock-absorbing performance advantage such as good, can carry out three translations and three rotations in the motion of six degrees of freedom directions altogether in the space, and has further promoted Stewart parallel mechanism 13's shock-absorbing performance through spacing spring 138, has ensured unmanned aerial vehicle stability when descending to berth base 3, and the jitter is little, has reduced the damage of vibration to the unmanned aerial vehicle fuselage when descending.
As shown in fig. 2, the damping mechanism 14 includes an upper mounting column 141, a lower mounting column 142 and a damping pressure spring 143; the upper mounting column 141 and the lower mounting column 142 are both of a T-shaped structure, the upper end of the upper mounting column 141 and the lower end of the lower mounting column 142 are respectively provided with an external thread, the lower end of the upper mounting column 141 and the upper end of the lower mounting column 142 are respectively provided with a locking sleeve, the upper end of the upper mounting column 141 and the upper fixing seat 12 are connected in a thread fit manner, the lower end of the lower mounting column 142 and the lower fixing seat 11 are also connected in a thread fit manner, and two ends of a damping pressure spring 143 are respectively mounted at the lower end of the upper mounting column 141 and the upper end of the lower mounting column 142; the damping mechanism 14 has a secondary damping effect on the damping device, so that the damping device 1 has a dual damping effect, and the damping performance is greatly improved.
As shown in fig. 5, the bottom end of the docking base 3 is of a regular octagonal flat plate structure, the left side and the right side of the upper end face of the docking base 3 are symmetrically provided with semicircular clamping grooves respectively, the unmanned aerial vehicle landing on the docking base 3 can be fixed in position through the semicircular clamping grooves, a circular hole is formed in the center of the upper end face of the docking base 3, the outer side of the docking base 3 is provided with a surrounding edge, signal lamps are uniformly arranged on the outer side of the surrounding edge in sequence, and the signal lamps play a role of prompting the position of the invention at night.
As shown in fig. 3 and 5, the charging device 4 includes a battery box 41, a lithium battery 42, a conduit 43, a connecting wire 44 and an adjustable charging base 45; lithium cell 42 install in battery case 41, conduit 43 one end is fixed in lithium cell 42 top, the round hole of berthhing 45 central point department is passed to the conduit 43 other end, conduit 43 adopts rubber hose, connecting wire 44 and adjustable charging base 45 quantity are two, adjustable charging base 45 is respectively symmetrical installation in both sides around conduit 43, connecting wire 44 lower extreme is connected with lithium cell 42, connecting wire 44 upper end is connected with adjustable charging base 45.
As shown in fig. 3 and 5, the adjustable charging base 45 includes a bottom plate 451, a locking screw 452, a longitudinal electric push rod 453, a lifting plate 454, a vertical rail 455, a sliding block 456, a transverse electric push rod 457 and a charging contact 458, wherein the number of the longitudinal electric push rod 453, the sliding block 456, the transverse electric push rod 457 and the charging contact 458 is two; the bottom plate 451 is fixed on the docking base 3 through a locking screw 452, the longitudinal electric push rods 453 are respectively symmetrically arranged on the left side and the right side of the locking screw 452 along the longitudinal central axis of the bottom plate 451, the bottom end of the longitudinal electric push rod 453 is fixedly connected with the bottom plate 451, the top end of the longitudinal electric push rod 453 is connected with the lifting plate 454, the vertical guide rail 455 is fixed on the upper end surface of the lifting plate 454, the slide block 456 is installed in front of the vertical guide rail 455, one end of the transverse electric push rod 457 is connected with the slide block 456, and the other end of the transverse electric push rod 457 is connected with the charging contact 458; adjustable charging base 45 highly can adjust on the perpendicular, and horizontal position and vertical position all can be adjusted on the horizontal plane, can be applicable to charging of different model unmanned aerial vehicle, and counterpoint convenient and fast during charging, and adopt many charging contact to charge, and charging efficiency is high.
The foregoing illustrates and describes the principles, general features, and advantages of the present invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are given by way of illustration of the principles of the present invention, and that various changes and modifications may be made without departing from the spirit and scope of the invention as defined by the appended claims. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (8)
1. A charging station, characterized by: the device comprises a damping device, a docking base and a charging device; the parking base is positioned right above the damping device and fixedly connected with the damping device, and the charging device is positioned above the parking base; wherein:
the damping device comprises a lower fixed seat, an upper fixed seat, a Stewart parallel mechanism and at least one damping mechanism; the Stewart parallel mechanism is positioned between the lower fixed seat and the upper fixed seat, and the damping mechanisms are respectively positioned at the outer sides of the Stewart parallel mechanism;
the Stewart parallel mechanism comprises a fixed platform, a movable platform, a lower triangular seat, an upper triangular seat, a ball hinge, a sleeve, a telescopic rod and a limiting spring, wherein the lower triangular seat is arranged on the upper end surface of the fixed platform, the upper triangular seat is arranged on the lower end surface of the movable platform, the ball hinge is respectively arranged on the lower triangular seat and the upper triangular seat, one end of the sleeve is connected with the ball hinge, the other end of the sleeve is connected with the telescopic rod, and the limiting spring is wound on the telescopic rod;
the charging device comprises a lithium battery, a conduit, a connecting wire and at least one adjustable charging base; one end of the conduit is fixed above the lithium battery, the other end of the conduit penetrates through the upper end face of the parking base, the adjustable charging bases are symmetrically arranged on the front side and the rear side of the conduit respectively, the lower end of the connecting wire is connected with the lithium battery, and the upper end of the connecting wire is connected with the adjustable charging bases;
the adjustable charging base comprises a bottom plate, at least one longitudinal electric push rod, a lifting plate, a vertical guide rail, a sliding block, a transverse electric push rod and a charging contact head, wherein the bottom plate is fixed on the parking base;
the damping mechanism comprises an upper mounting column, a lower mounting column and a damping pressure spring; the upper end of the upper mounting column is connected with the upper fixing seat, the lower end of the lower mounting column is connected with the lower fixing seat, and two ends of the damping pressure spring are respectively mounted at the lower end of the upper mounting column and the upper end of the lower mounting column;
the lower end of the Stewart parallel mechanism is connected with the lower fixed seat, the upper end of the Stewart parallel mechanism is connected with the upper fixed seat, and the damping mechanisms are uniformly and circumferentially arranged along the central axis of the Stewart parallel mechanism; decide the platform and all be circular column structure with moving the platform, the triangle base is regular triangle position down and arranges on deciding the platform, and the triangle base is regular triangle cylinder structure down, and two liang of crisscross mounting position between triangle base and the last triangle base down, the triangle base is provided with the inclined plane along its perpendicular center line symmetry respectively down, offers on the inclined plane with ball hinge lower extreme external screw thread matched with mounting screw hole, and the structure of going up the triangle base is the same with the structure of triangle base down.
2. A charging station as claimed in claim 1, wherein: the number of the shock absorption mechanisms is eight.
3. A charging station as claimed in claim 1, wherein: the number of the lower triangular seats and the upper triangular seats is three, the number of the ball hinges, the sleeves and the limiting springs is twelve, and the number of the telescopic rods is six.
4. A charging station as claimed in claim 1, wherein: the charging device also comprises a battery box, and the lithium battery is arranged in the battery box.
5. A charging station as claimed in claim 1, wherein: the number of the connecting wires and the number of the adjustable charging bases are two.
6. A charging station as claimed in claim 1, wherein: the adjustable charging base further comprises locking screws, the longitudinal electric push rods are symmetrically arranged on the left side and the right side of the locking screws, and the bottom plate is fixed on the parking base through the locking screws.
7. A charging station as claimed in claim 1, wherein: go up the erection column and all be T type structure with erection column down, go up the erection column upper end and equally divide with the erection column lower extreme down and do not be provided with the external screw thread, go up the erection column lower extreme and equally divide with the erection column upper end down and do not be provided with the lock sleeve, go up the erection column upper end through screw-thread fit's mode with go up the fixing base and connect, the erection column lower extreme passes through screw-thread fit's mode down and is connected with lower fixing base down.
8. A charging station as claimed in claim 1, wherein: the utility model discloses a docking base, wire conduit, docking base bottom be regular octagon flat plate structure, and the left and right sides of docking base up end symmetry respectively has seted up semi-circular screens groove, the central point department of putting of docking base up end has seted up the round hole, the wire conduit other end passes this round hole, the outside of docking the base is provided with the surrounding edge, the surrounding edge outside evenly is provided with the signal lamp in proper order.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810359828.4A CN108336798B (en) | 2016-06-28 | 2016-06-28 | Charging station |
Applications Claiming Priority (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 | Title | Priority Date | Filing Date |
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| CN201610491286.7A Division CN105914844B (en) | 2016-06-28 | 2016-06-28 | A kind of multidimensional damping type unmanned plane charging station |
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| CN108336798A CN108336798A (en) | 2018-07-27 |
| CN108336798B true CN108336798B (en) | 2021-09-07 |
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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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| Publication number | Priority date | Publication date | Assignee | Title |
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| 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 |
| US11891192B2 (en) * | 2018-07-23 | 2024-02-06 | Shanghai Autoflight Co., Ltd. | Landing platform for unmanned aerial vehicle |
| 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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| Publication number | Priority date | Publication date | Assignee | Title |
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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 |
| CN103511549B (en) * | 2013-08-19 | 2016-03-02 | 燕山大学 | A kind of irrotational displacement parallel-connection vibration reduction 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 |
| CN104029711B (en) * | 2014-06-25 | 2017-06-06 | 玄春花 | A kind of multidimensional shock absorption babies ' barrow |
| 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 |
| CN104979882B (en) * | 2015-07-30 | 2017-03-01 | 安徽啄木鸟无人机科技有限公司 | A kind of unmanned plane quick charging system and its charging method |
| 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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Also Published As
| Publication number | Publication date |
|---|---|
| CN105914844B (en) | 2018-08-24 |
| CN105914844A (en) | 2016-08-31 |
| CN108336798A (en) | 2018-07-27 |
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