CN106114884B - A kind of unmanned plane based on Stewart parallel institutions stops charging station - Google Patents
A kind of unmanned plane based on Stewart parallel institutions stops charging station Download PDFInfo
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- CN106114884B CN106114884B CN201610490997.2A CN201610490997A CN106114884B CN 106114884 B CN106114884 B CN 106114884B CN 201610490997 A CN201610490997 A CN 201610490997A CN 106114884 B CN106114884 B CN 106114884B
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- pedestal
- damping
- mounting post
- parallel institutions
- stewart parallel
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- 238000007600 charging Methods 0.000 title claims abstract description 50
- 238000013016 damping Methods 0.000 claims abstract description 63
- 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
- 230000002457 bidirectional effect Effects 0.000 claims description 13
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 12
- 229910052744 lithium Inorganic materials 0.000 claims description 12
- 230000006835 compression Effects 0.000 claims description 6
- 238000007906 compression Methods 0.000 claims description 6
- 238000009434 installation Methods 0.000 claims description 5
- 238000010276 construction Methods 0.000 claims description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 7
- 238000010521 absorption reaction Methods 0.000 abstract description 5
- 230000009977 dual effect Effects 0.000 abstract description 5
- 230000035939 shock Effects 0.000 abstract description 5
- 239000013589 supplement Substances 0.000 abstract description 4
- 238000004146 energy storage Methods 0.000 abstract description 2
- 238000012544 monitoring process Methods 0.000 description 8
- 238000010586 diagram Methods 0.000 description 7
- 238000013519 translation Methods 0.000 description 5
- 230000014616 translation Effects 0.000 description 5
- 230000007613 environmental effect Effects 0.000 description 4
- 230000008859 change Effects 0.000 description 2
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 1
- 241000607479 Yersinia pestis Species 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 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
- 238000013507 mapping Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/007—Helicopter portable landing pads
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression 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
- F16F15/04—Suppression 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
- F16F15/06—Suppression 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
-
- 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
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Power Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Photovoltaic Devices (AREA)
Abstract
The present invention relates to a kind of unmanned planes based on Stewart parallel institutions to stop charging station, including damping device, support device, stops pedestal and charging unit；The support device quantity is eight, support device is located at damping device outboard end respectively along the central axis of damping device, and it is attached between support device and damping device by bolt, 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, dual shock absorption, stops the charging of fixed and multistation, realize 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 the ability of unmanned machine operation.
Description
Technical field
The present invention relates to aircraft fields, and specifically a kind of unmanned plane based on Stewart parallel institutions, which is stopped, charges
It stands.
Background technology
Aircraft is to be manufactured by the mankind, can fly away from ground, controlled in space flight and by people in endoatmosphere or big
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.；It can be divided by application field military with civilian, military aspect unmanned plane is divided into reconnaissance plane and target drone；
At present, 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
The fields such as the protection of woods pest and disease damage and monitoring, digital city.
Unmanned plane belongs to one kind of aircraft, and unmanned plane has that 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 of unmanned machine operation, for the energy supplementary question of unmanned plane, military unmanned air vehicle mostly using air refuelling come
It solves, since such supplement energy mode cost is too big, there is no applying on civilian unmanned plane, civilian unmanned plane is current
Still also generally also have and charging base station is added to carry out energy supplement to the unmanned plane of operation on the way without good settling mode, but
It is that there are damping performance is poor, energy source is single, stop is inconvenient, charging needs manual operation for current unmanned plane charging base station
The problems such as, in consideration of it, the present invention provides a kind of unmanned planes based on Stewart parallel institutions to stop charging station.
Invention content
In order to make up for the deficiencies of the prior art, the present invention provides a kind of unmanned planes based on Stewart parallel institutions to stop
By charging station.
The present invention to be solved its technical problem and be realized using following technical scheme.
A kind of unmanned plane based on Stewart parallel institutions stops charging station, including damping device, support device, stop
Pedestal and charging unit；The support device quantity is eight, and the central axis of support device along damping device is located at respectively to be subtracted
Device outboard end is shaken, and is attached between support device and damping device by bolt, pedestal is stopped and is being located at damping device just
Top, and stop and be 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, 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, damping difference 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 mounted on moving platform on fixed platform in equilateral triangle location arrangements, upper Triangulum
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 with 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, limiting
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 common 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 during 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
Lock sleeve is respectively provided with lower mounting post upper end, between upper mounting post upper end and upper fixed seat by the way of thread fitting
It is attached, is attached between lower mounting post lower end and lower fixed seat also by the mode of thread fitting, 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 dual shock absorption, damping performance is greatly improved.
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 is assigned into the rectangular card slot of support base, and is attached between photovoltaic battery panel and support base using clamping screw；
The distance that support device stretches outward can be changed by adjusting screw rod, suitable for the use in different places, and support dress
Put in the horizontal plane with can be rotated in vertical plane, so as to adjusting supporting device in the horizontal plane and vertical plane
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 and rotate totally three
Movement on a degree of freedom direction, can adjust angular at any time, improve the efficiency that solar energy is converted to electric energy, and can fit
For the photovoltaic battery panel of 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 puts fixation, and the center position for stopping pedestal upper surface offers circular hole, stops and surrounding edge is provided 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 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, and lateral position and lengthwise position can be adjusted in the horizontal plane, can be adapted for difference on vertical plane
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, dual shock absorption, stops the charging of fixed and multistation, and it is more to realize a machine
The effect of energy 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.
(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 common six-freedom degree direction of three rotations is moved, and subtracting for Stewart parallel institutions is further improved 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) 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 adjust angular at any time, 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, and lateral position and longitudinal direction in the horizontal plane on the vertical 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
The present invention is further described with reference to the accompanying 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 stops pedestal cooperation；
Fig. 6 is the dimensional structure diagram of Stewart parallel institutions of the present invention；
The dimensional structure diagram of Fig. 7 adjustable recharging bases of the invention.
Specific embodiment
In order to be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, tie below
Conjunction is specifically illustrating, and the present invention is further explained.
As shown in Figures 1 to 7, a kind of unmanned plane based on Stewart parallel institutions stops charging station, including damping device
1st, support device 2, stop pedestal 3 and charging unit 4；2 quantity of support device is eight, and support device 2 is along damping device 1
Central axis be located at 1 outboard end of damping device respectively, and be attached between support device 2 and damping device 1 by bolt,
It stops pedestal 3 to be located at right over damping device 1, and stops and be connected between pedestal 3 and damping device 1, charging unit 4, which is located at, to be stopped
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 the outside of Stewart parallel institutions 13 respectively, and damping 14 is along Stewart
The central axis of parallel institution 13 is uniformly arranged circumferentially about.
As shown in fig. 6, 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 for 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 mounted on 132 lower face of moving platform on fixed platform 131 in equilateral triangle location arrangements, upper Triangulum 134
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 with 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 can be carried out in space and rotate totally six
The movement in degree of freedom 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 upper mounting post 141 and the T-shaped structure of lower mounting post 142 stated, upper 141 upper end of mounting post and lower 142 lower end of mounting post are divided equally
It is not provided with external screw thread, upper 141 lower end of 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 thread fitting 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 thread fitting, 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 3 and Figure 4, the support device 2 includes connecting seat 21, sleeve 22, adjusting screw rod 23, movable plate
24th, 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 is assigned 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；The distance that support device 2 stretches outward can be changed by adjusting screw rod 23, 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 common three degree of freedom direction of a translation two rotation, angular can be adjusted at any time, improve solar energy
The efficiency of electric energy is converted to, 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 7, 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, and conduit 43 uses rubber hose, connecting line 44
It is two with adjustable 45 quantity of 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 7, 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 electric push rod 453 is arranged symmetrically respectively along the longitudinal center axis of bottom plate 451
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, and lateral position and lengthwise position are equal in the horizontal plane adjustable recharging base 45 on the vertical 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 (4)
1. a kind of unmanned plane based on Stewart parallel institutions stops charging station, it is characterised in that：Including damping device, support
Device stops pedestal and charging unit；The support device quantity is eight, central axis point of the support device along damping device
Not Wei Yu damping device outboard end, and be attached between support device and damping device by bolt, stop pedestal and be located at and subtracts
It shakes right over device, and stops 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, 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 respectively
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 mounted in equilateral triangle location arrangements, upper Triangulum on moving platform lower face on fixed platform, and
Installation site between upper Triangulum and trigonid is interlocked two-by-two, and trigonid is in equilateral triangle column structure, trigonid
Inclined surface has been symmetrically arranged 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 with 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 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, photovoltaic battery panel assigns into
In the rectangular card slot of support base, and it is attached between photovoltaic battery panel and support base using clamping screw；
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. a kind of unmanned plane based on Stewart parallel institutions according to claim 1 stops charging station, feature exists
In：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 thread fitting between upper mounting post upper end and upper fixed seat, under
It is attached between mounting post lower end and lower fixed seat also by the mode of thread fitting, damping compression spring both ends are separately mounted to
Mounting post lower end and lower mounting post upper end.
3. a kind of unmanned plane based on Stewart parallel institutions according to claim 1 stops charging station, feature exists
In：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.
4. a kind of unmanned plane based on Stewart parallel institutions according to claim 1 stops charging station, feature exists
In：The adjustable recharging base includes bottom plate, lock-screw, longitudinal electric push rod, lifter plate, vertical guide rail, sliding block, transverse direction
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 stopped on pedestal, and longitudinal electric push rod is respectively along the longitudinal center axis pair of bottom plate
Title is arranged 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 and lifting
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
It is connected with sliding block, the transverse electric push rod other end is connected with charging contact.
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| CN201610490997.2A CN106114884B (en) | 2016-06-28 | 2016-06-28 | A kind of unmanned plane based on Stewart parallel institutions stops charging station |
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| CN201610490997.2A CN106114884B (en) | 2016-06-28 | 2016-06-28 | A kind of unmanned plane based on Stewart parallel institutions stops charging station |
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| CN106114884B true CN106114884B (en) | 2018-07-10 |
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| CN107010240A (en) * | 2017-05-12 | 2017-08-04 | 河南省酷农航空植保科技有限公司 | A kind of solar recharging landing platform of unmanned plane |
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| CN108674683A (en) * | 2018-05-25 | 2018-10-19 | 芜湖万户航空航天科技有限公司 | Unmanned vehicle landing adjusts platform |
| CN108466701A (en) * | 2018-05-25 | 2018-08-31 | 芜湖万户航空航天科技有限公司 | Unmanned plane landing adjusts platform |
| CN108791930A (en) * | 2018-05-25 | 2018-11-13 | 芜湖万户航空航天科技有限公司 | Safe unmanned plane landing platform |
| CN108797399A (en) * | 2018-05-25 | 2018-11-13 | 芜湖万户航空航天科技有限公司 | Ight unmanned plane landing adjusts platform |
| CN109552658B (en) * | 2018-11-28 | 2023-07-25 | 宁波上航测绘有限公司 | Unmanned aerial vehicle platform of taking off and land to sea water sample |
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| CN109898909A (en) * | 2019-04-03 | 2019-06-18 | 南昌汇达知识产权有限公司 | A kind of building earthquake isolating equipment |
| CN110667870B (en) * | 2019-10-12 | 2023-01-20 | 内蒙古工业大学 | Unmanned aerial vehicle is energy autonomous base station of independently taking off and land trading battery based on solar energy power supply |
| CN113685488A (en) * | 2021-09-13 | 2021-11-23 | 湖南工学院 | Electromagnetic shock absorber capable of achieving multi-direction shock absorption |
| CN113815443A (en) * | 2021-09-16 | 2021-12-21 | 星逻人工智能技术(上海)有限公司 | Automatic charging device of unmanned aerial vehicle |
| CN113738818B (en) * | 2021-11-03 | 2022-02-08 | 溧阳常大技术转移中心有限公司 | Two-dimensional vibration isolator capable of exciting and isolating any displacement in opposite surface |
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