CN106026271B - A kind of self-stabilising photovoltaic charged formula unmanned plane charging base station - Google Patents

A kind of self-stabilising photovoltaic charged formula unmanned plane charging base station Download PDF

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Publication number
CN106026271B
CN106026271B CN201610491230.1A CN201610491230A CN106026271B CN 106026271 B CN106026271 B CN 106026271B CN 201610491230 A CN201610491230 A CN 201610491230A CN 106026271 B CN106026271 B CN 106026271B
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China
Prior art keywords
mounting post
damping
pedestal
damping device
electric push
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CN201610491230.1A
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CN106026271A (en
Inventor
吴燕
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Guangdong Tongjian Industrial Development Co.,Ltd.
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Quanzhou Taiwan Investment Zone Ben Sheng Machinery Technology Co Ltd
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    • H02J7/0003
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F16F15/04Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
    • F16F15/06Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means with metal springs
    • F16F15/067Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means with metal springs using only wound springs
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02SGENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S20/00Supporting structures for PV modules
    • H02S20/30Supporting structures being movable or adjustable, e.g. for angle adjustment
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02SGENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S30/00Structural details of PV modules other than those related to light conversion
    • H02S30/10Frame structures
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02SGENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S40/00Components or accessories in combination with PV modules, not provided for in groups H02S10/00 - H02S30/00
    • H02S40/30Electrical components
    • H02S40/38Energy storage means, e.g. batteries, structurally associated with PV modules
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/50Photovoltaic [PV] energy
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E70/00Other energy conversion or management systems reducing GHG emissions
    • Y02E70/30Systems combining energy storage with energy generation of non-fossil origin

Abstract

The present invention relates to a kind of self-stabilising photovoltaic charged formula unmanned plane charging base stations, including damping device, support device, stop pedestal and charging unit;The support device quantity is eight, support device is located at damping device outboard end along the central axis of damping device, and it is attached by bolt between support device and damping device, pedestal is stopped to be located at right over damping device, and stop and be connected between pedestal and damping device, charging unit, which is located at, to be stopped above pedestal.The present invention integrates photovoltaic energy storage, damping, 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

A kind of self-stabilising photovoltaic charged formula unmanned plane charging base station
Technical field
The present invention relates to aircraft field, specifically a kind of photovoltaic charged formula unmanned plane of self-stabilising charges base 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, energy source is single, stop is inconvenient, charging needs manual operation The problems such as, in consideration of it, the present invention provides a kind of self-stabilising photovoltaic charged formula unmanned plane charging base stations.
Invention content
In order to make up for the deficiencies of the prior art, the present invention provides a kind of photovoltaic charged formula unmanned plane charging bases of self-stabilising It stands.
The present invention to be solved its technical problem and be realized using following technical scheme.
A kind of photovoltaic charged formula unmanned plane of self-stabilising charges base station, including damping device, support device, stops pedestal and fill Electric installation;The support device quantity is eight, and support device is located at along the central axis of damping device outside damping device Side, and be attached by bolt between support device and damping device, it stops pedestal and is located at right over damping device, and stop It is connected between pedestal and damping device, charging unit, which is located at, to be stopped above pedestal.
Further, the damping device includes lower fixed seat, upper fixed seat and damping;The damping Quantity is eight, and damping is between lower fixed seat and upper fixed seat, and damping is equal along the central axis of lower fixed seat It is even to be arranged circumferentially about;The damping includes upper mounting post, lower mounting post and damping compression spring;The upper mounting post is under The 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 and Lower mounting post upper end is respectively provided with lock sleeve, between upper mounting post upper end and upper fixed seat by the way of screw-thread fit into Row connection, is attached between lower mounting post lower end and lower fixed seat also by the mode of screw-thread fit, damping compression spring both ends point It An Zhuan not upper mounting post lower end and lower mounting post upper end;Damping device has good damping effect.
Further, the support device include connecting seat, sleeve, adjusting screw rod, movable plate, Rotational Cylindrical, bidirectional tension rod, Support base, photovoltaic battery panel and clamping screw;The connecting seat is in crescent shape structure, and sleeve and adjusting screw rod quantity are Two, sleeve bottom end is respectively symmetrically fixed on connecting seat along the central transverse axis of connecting seat, and sleeve top end is provided with and adjusts The matched internal thread hole of screw rod is saved, adjusting screw rod one end is mounted on inside the internal thread hole of sleeve top end, and adjusting screw rod is another One end is connected with movable plate, and vertical duction hole is provided at movable plate upper end center position, and Rotational Cylindrical lower end is mounted on movement In vertical duction hole at plate upper end center position, Rotational Cylindrical upper end, which is provided with, is horizontally diverted hole, is mounted in the middle part of bidirectional tension rod Rotational Cylindrical upper end is horizontally diverted in hole, and bidirectional tension rod both ends length is adjustable, and support base quantity is two, and support base is fixed on double To pull rod outboard end, rectangular card slot is offered on support base, offers limit hole, photovoltaic on support base front/rear end at equal intervals Solar panel assigns into the rectangular card slot of support base, and is attached using clamping screw between photovoltaic battery panel and support base; It can change the distance that support device stretches outward by adjusting screw rod, be suitable for the use in different places, and support dress Set in the horizontal plane with can be rotated in vertical plane, in the horizontal plane and vertical plane so as to adjusting supporting device Interior angle, and then the angle of photovoltaic battery panel control sunlight can be changed, effectively raise the absorption of photovoltaic battery panel In addition to this sunlight ability can adjust the spacing between two support bases by bidirectional tension rod, be easily installed different model The photovoltaic battery panel of size, applicability is wider, and support device uses the form of cascaded structure, can carry out a translation two rotation totally three Movement in a freedom degree direction, can be adjusted at any time angular, improve the efficiency that solar energy is converted to electric energy, and can fit Photovoltaic battery panel for different model size.
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 photovoltaic energy storage, damping, stops the charging of fixed and multistation, realizes one-machine-multi-function Effect 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 nobody The ability of machine operation.
(2) damping device bearing capacity of the invention is strong and damping performance is good, it is ensured that unmanned plane is dropping to stop base Stability when seat, jitter is small, damage of the vibration to unmanned aerial vehicle body when reducing landing.
(3) support device of the invention uses the form of cascaded structure, can carry out a translation two rotation three degree of freedom altogether Movement on direction, can be adjusted at any time angular, improves solar energy and is converted to the efficiency of electric energy, and is applicable to difference The photovoltaic battery panel of gauge size.
(4) 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;
Fig. 3 is the dimensional structure diagram (seeing from front to back) of support device of the present invention;
Fig. 4 is the dimensional structure diagram (seeing from back to front) of support device of the present invention;
Dimensional structure diagram when Fig. 5 is charging unit of the present invention and stop pedestal cooperation;
The dimensional structure diagram of Fig. 6 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 6, a kind of self-stabilising photovoltaic charged formula unmanned plane charging base station, including damping device 1, support Device 2 stops pedestal 3 and charging unit 4;2 quantity of support device is eight, and support device 2 is along the center of damping device 1 Axis is located at 1 outboard end of damping device, and is attached by bolt between support device 2 and damping device 1, stops base Seat 3 is located at right over damping device 1, and stops and be connected between pedestal 3 and damping device 1, and charging unit 4, which is located at, stops pedestal 3 Top.
As shown in Fig. 2, the damping device 1 includes lower fixed seat 11, upper fixed seat 12 and damping 14;Described The quantity of damping 14 is eight, and damping 14 is between lower fixed seat 11 and upper fixed seat 12, and 14 edge of damping The central axis of lower fixed seat 11 is uniformly arranged circumferentially about;The damping 14 includes upper mounting post 141, lower mounting post 142 and damping compression spring 143;The 142 T-shaped structure of upper mounting post 141 and lower mounting post, 141 upper end of upper mounting post and Lower 142 lower end of mounting post is respectively provided with external screw thread, and 141 lower end of upper mounting post and lower 142 upper end of mounting post are respectively arranged There is lock sleeve, is attached by the way of screw-thread fit between 141 upper end of upper mounting post and upper fixed seat 12, lower mounting post It is attached also by the mode of screw-thread fit between 142 lower ends and lower fixed seat 11,143 both ends of damping compression spring are separately mounted to 141 lower end of upper mounting post and lower 142 upper end of mounting post;Damping device 1 has good damping effect.
As shown in Figure 3 and Figure 4, the support device 2 includes connecting seat 21, sleeve 22, adjusting screw rod 23, movable plate 24, Rotational Cylindrical 25, bidirectional tension rod 26, support base 27, photovoltaic battery panel 28 and clamping screw 29;The connecting seat 21 is in crescent moon Shape structure, sleeve 22 and 23 quantity of adjusting screw rod are two, and 22 bottom end of sleeve is right respectively along the central transverse axis of connecting seat 21 Title is fixed on connecting seat 21, and 22 top end of sleeve is provided with and 23 matched internal thread hole of adjusting screw rod, adjusting screw rod 23 One end is mounted on inside the internal thread hole of 22 top end of sleeve, and 23 other end of adjusting screw rod is connected with movable plate 24, movable plate Vertical duction hole is provided at 24 upper end center positions, 25 lower end of Rotational Cylindrical is mounted on hanging down at 24 upper end center position of movable plate In straight crossover port, 25 upper end of Rotational Cylindrical, which is provided with, is horizontally diverted hole, and 26 middle part of bidirectional tension rod is mounted on the water of 25 upper end of Rotational Cylindrical In flat crossover port, and 26 both ends length of bidirectional tension rod is adjustable, and 27 quantity of support base is two, and support base 27 is fixed on bidirectional tension rod 26 Outboard end offers rectangular card slot on support base 27, limit hole, photovoltaic electric is offered at equal intervals on 27 front/rear end of support base Pond plate 28 assigns into the rectangular card slot of support base 27, and between photovoltaic battery panel 28 and support base 27 using clamping screw 29 into Row connection;It can change the distance that support device 2 stretches outward by adjusting screw rod 23, be suitable for the use in different places, And support device 2 in the horizontal plane with can be rotated in vertical plane, so as to adjusting supporting device 2 in level Angle in face and in vertical plane, and then the angle that photovoltaic battery panel 28 compares sunlight can be changed, effectively raise light The power that absorbs solar energy of solar panel 28 is lied prostrate, in addition to this, can be adjusted between two support bases 27 by bidirectional tension rod 26 Spacing is easily installed the photovoltaic battery panel 28 of different model size, and applicability is wider, and support device 2 uses the shape of cascaded structure Formula can carry out the movement on the total three degree of freedom direction of a translation two rotation, can be adjusted at any time to angular, improve solar energy It is converted to the efficiency of electric energy, and is applicable to the photovoltaic battery panel 28 of different model size.
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 5 and Figure 6, 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 3 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 5 and Figure 6, 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 (3)

  1. The base station 1. a kind of photovoltaic charged formula unmanned plane of self-stabilising charges, it is characterised in that:Including damping device, support device, stop By pedestal and charging unit;The support device quantity is eight, and support device is located at along the central axis of damping device Damping device outboard end, and be attached by bolt between support device and damping device, it stops pedestal and is located at damping device Surface, and stop and be connected between pedestal and damping device, charging unit, which is located at, to be stopped above pedestal;Wherein:
    The damping device includes lower fixed seat, upper fixed seat and damping;The quantity of the damping is eight, is subtracted Mechanism is shaken between lower fixed seat and upper fixed seat, and damping is along the uniform circumferentially cloth of central axis of lower fixed seat It sets;The damping includes upper mounting post, lower mounting post and damping compression spring;The upper mounting post and lower mounting post are in T-type structure, upper mounting post upper end and lower mounting post lower end are respectively provided with external screw thread, on upper mounting post lower end and lower mounting post 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, under It is attached also by the mode of screw-thread fit between mounting post lower end and lower fixed seat, damping compression spring both ends are separately mounted to Mounting post lower end and lower mounting post upper end;
    The support device includes connecting seat, sleeve, adjusting screw rod, movable plate, Rotational Cylindrical, bidirectional tension rod, support base, photovoltaic Solar panel and clamping screw;The connecting seat is in crescent shape structure, and sleeve and adjusting screw rod quantity are two, sleeve bottom end edge The central transverse axis of connecting seat is respectively symmetrically fixed on connecting seat, and sleeve top end is provided with matched with adjusting screw rod Internal thread hole, adjusting screw rod one end are mounted on inside the internal thread hole of sleeve top end, the adjusting screw rod other end and movable plate phase It connects, vertical duction hole is provided at movable plate upper end center position, Rotational Cylindrical lower end is mounted on movable plate upper end center position In the vertical duction hole at place, Rotational Cylindrical upper end, which is provided with, is horizontally diverted hole, and the water of Rotational Cylindrical upper end is mounted in the middle part of bidirectional tension rod In flat crossover port, and bidirectional tension rod both ends length is adjustable, and support base quantity is two, and support base is fixed on bidirectional tension rod outboard end, Rectangular card slot is offered on support base, offers limit hole on support base front/rear end at equal intervals, and photovoltaic battery panel assigns into In the rectangular card slot of support base, and it is attached using clamping screw between photovoltaic battery panel and support base;
    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.
  2. The base station 2. the photovoltaic charged formula unmanned plane of a kind of self-stabilising according to claim 1 charges, it is characterised in that:Described It is in octagon slab construction to stop base bottom, and the left and right sides for stopping pedestal upper surface respectively symmetrically offers semicircle Screens slot, the center position for stopping pedestal upper surface offer circular hole, stop and be provided with surrounding edge on the outside of pedestal, on the outside of surrounding edge It is evenly arranged with signal lamp successively.
  3. The base station 3. the photovoltaic charged formula unmanned plane of a kind of self-stabilising according to claim 1 charges, it is characterised in that:Described Adjustable recharging base includes bottom plate, lock-screw, longitudinal electric push rod, lifter plate, vertical guide rail, sliding block, transverse electric push rod With 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 arranged symmetrically in along the longitudinal center axis of bottom plate respectively At left and right sides of lock-screw, and longitudinal electric push rod bottom end is connected with bottom plate, and longitudinal electric push rod top is connected with lifter plate, 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 and sliding block phase Connection, the transverse electric push rod other end are connected with charging contact.
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CN108820237A (en) * 2018-05-31 2018-11-16 智飞智能装备科技东台有限公司 A kind of photovoltaic charged base station for unmanned plane
CN109606723A (en) * 2019-01-25 2019-04-12 岩石矿业投资有限公司 A kind of vehicle-mounted unmanned aerial vehicle concave surface type landing platform
CN110380501B (en) * 2019-08-15 2022-05-31 国网冀北电力有限公司承德供电公司 Platform for receiving, releasing and charging express unmanned aerial vehicle based on wind-solar hybrid
CN112135202A (en) * 2020-08-11 2020-12-25 杭州炸裂科技有限公司 Adjustable base station equipment

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