CN106005464A - Energy-saving type energy supplement equipment for unmanned aerial vehicle - Google Patents
Energy-saving type energy supplement equipment for unmanned aerial vehicle Download PDFInfo
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- CN106005464A CN106005464A CN201610491227.XA CN201610491227A CN106005464A CN 106005464 A CN106005464 A CN 106005464A CN 201610491227 A CN201610491227 A CN 201610491227A CN 106005464 A CN106005464 A CN 106005464A
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- damping
- energy
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- 239000013589 supplement Substances 0.000 title abstract description 9
- 238000013016 damping Methods 0.000 claims abstract description 72
- 238000007600 charging Methods 0.000 claims abstract description 35
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 33
- 230000007246 mechanism Effects 0.000 claims description 30
- 230000002457 bidirectional effect Effects 0.000 claims description 14
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 12
- 229910052744 lithium Inorganic materials 0.000 claims description 12
- 238000009434 installation Methods 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 4
- 238000010276 construction Methods 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims description 2
- 238000004146 energy storage Methods 0.000 abstract description 2
- 230000002035 prolonged effect Effects 0.000 abstract 1
- 230000033001 locomotion Effects 0.000 description 20
- 230000000694 effects Effects 0.000 description 14
- 238000012544 monitoring process Methods 0.000 description 7
- 230000008859 change Effects 0.000 description 5
- 230000009977 dual effect Effects 0.000 description 4
- 230000007613 environmental effect Effects 0.000 description 4
- 230000001105 regulatory effect Effects 0.000 description 4
- 238000010521 absorption reaction Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- 238000006073 displacement reaction Methods 0.000 description 3
- 230000008030 elimination Effects 0.000 description 3
- 238000003379 elimination reaction Methods 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 238000013519 translation Methods 0.000 description 3
- 238000007689 inspection Methods 0.000 description 2
- 241000607479 Yersinia pestis Species 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 201000010099 disease Diseases 0.000 description 1
- 208000037265 diseases, disorders, signs and symptoms Diseases 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 230000001502 supplementing effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- 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
- B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
-
- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention relates to energy-saving type energy supplement equipment for an unmanned aerial vehicle. The energy-saving type energy supplement equipment comprises a damping device, eight supporting devices, a stopping base and charging devices; the supporting devices are located at the outer side end of the damping device along the central axis of the damping device, the supporting devices are connected with the damping device through bolts, the stopping base is located on the damping device and fixedly connected with the damping device, and the charging devices are located above the stopping base. According to the energy-saving type energy supplement equipment for the unmanned aerial vehicle, photovoltaic energy storage, double damping, stopping fixing and multi-station charging are integrated into a whole, one machine is used for multiple functions, the problems that for the unmanned aerial vehicle, energy supplement is difficult, and consumption is large are solved, the duration time of the unmanned aerial vehicle is prolonged, and the operation capability of the unmanned aerial vehicle is improved.
Description
Technical field
The present invention relates to aircraft field, a kind of energy-saving unmanned plane energy ancillary equipment.
Background technology
Aircraft be by the mankind manufacture, can fly away from ground, space flight and by people control in endoatmosphere or exoatmosphere
The apparatus flying object flown in space (space), aircraft is divided into airborne vehicle, spacecraft, rocket, guided missile and guided weapon；Nothing
Man-machine is also the one of aircraft, and unmanned plane is utilize that radio robot and the presetting apparatus provided for oneself handle the most manned
Aircraft, can be divided into depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship from technical standpoint definition
With unmanned parasol etc.；Can be divided into military and civilian by application, military aspect unmanned plane is divided into reconnaissance plane and target drone；At present,
Unmanned plane can be widely applied to country's ecological environmental protection, aeroplane photography, mapping, mineral resources exploration, the condition of a disaster supervision, traffic
Patrol, power-line patrolling, security monitoring, emergent mitigation, emergency command, rain making, national defense safety, land resources exploration,
Town planning, seismic survey, environmental monitoring, forest fire protection, Crop Estimation, protection zone wild animal monitoring, air sampling,
Maritime affairs scout, border make an inspection tour, the prohibition of drug scouting, fire inspection, ecological environmental protection, marine environmental monitoring, land use survey,
Water resources development, crop growth monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, urban planning and municipal administration pipe
The fields such as the protection of reason, forest disease and pest and monitoring, digital city.
Unmanned plane belongs to the one of aircraft, unmanned plane have relatively strong, the motion less than normal, popular of compact conformation, build flexibly and
The advantages such as flight stability are widely used in civil and military, and the most popular；But unmanned plane faces maximum at present
Problem demanding prompt solution is continued a journey exactly, and continuation of the journey decides time and the stability of the flight of unmanned plane, indirectly decides unmanned plane
The efficiency of operation and quality, for the energy supplementary question of unmanned plane, military unmanned air vehicle many employings air refuelling solves, due to
This kind of supplementary energy mode spends too big, therefore not application on civilian unmanned plane, and civilian unmanned plane is the most also without very well
Settling mode, the most also have and set up charging base station the unmanned plane of operation on the way is carried out energy supplement, but current unmanned
Machine charging base station exists that damping performance is poor, energy source is single, energy resource consumption is big, stop is inconvenient, charging needs manual operation
Etc. problem, in consideration of it, the invention provides a kind of energy-saving unmanned plane energy ancillary equipment.
Summary of the invention
In order to make up the deficiencies in the prior art, the invention provides a kind of energy-saving unmanned plane energy ancillary equipment.
The present invention to solve its technical problem and realize by the following technical solutions.
A kind of energy-saving unmanned plane energy ancillary equipment, including damping device, support means, stop pedestal and charging device；Institute
The support means quantity stated is eight, and support means lays respectively at damping device outboard end along the central axis of damping device, and supports
It is attached by bolt between device and damping device, stops pedestal and be positioned at directly over damping device, and stop pedestal and damping
Being connected between device, charging device is positioned at above stop pedestal.
Further, described damping device includes lower fixed seat, upper fixed seat, redundancy parallel mechanism and damping；Described
Redundancy parallel mechanism is between lower fixed seat and upper fixed seat, and redundancy parallel mechanism lower end is connected with lower fixed seat, redundancy
Parallel institution upper end is connected with upper fixed seat, and damping quantity is eight, and damping lays respectively at outside redundancy parallel mechanism,
And damping is uniformly arranged circumferentially about along the central axis of redundancy parallel mechanism.
Further, described redundancy parallel mechanism includes fixed platform, moving platform, the first side chain and the second side chain；Described allocates
Platform and moving platform are disc-shaped structure, and moving platform is positioned at directly over fixed platform；The first described side chain and the number of the second side chain
Amount is two, and the first side chain and the second side chain are respectively positioned between fixed platform and moving platform, and the two ends of the first side chain and the second side chain are equal
It is connected with fixed platform and moving platform respectively, and the horizontal installation angle of the first side chain and the second side chain is 90 degree；Described first
Side chain includes the first ear mount, Hooke's hinge, the first electric pushrod, the first spherical hinge, the first connection post and the first vibrating spring；Institute
The first ear mount stated is fixed on fixed platform upper surface, uses Hooke's hinge to carry out even between the first ear mount and the first electric pushrod lower end
Connecing, the first electric pushrod upper end is connected with the first spherical hinge, and the first spherical hinge connects post by first and is fixed under moving platform
On end face, the first vibrating spring is around being enclosed within the first electric pushrod；The rotation of both direction can be carried out, by by Hooke's hinge
One spherical hinge can carry out the rotation in three directions, can be moved up and down by the first electric pushrod, and the first side chain uses 2-UPS
The form of parallel institution, and the damping performance of the first side chain is added by the first vibrating spring, improve the damping effect of the present invention
Really；The second described side chain includes the second ear mount, rotational pin, the second electric pushrod, the second spherical hinge, second connects post and the
Two vibrating springs；The second described ear mount is fixed on fixed platform upper surface, adopts between the second ear mount and the second electric pushrod lower end
Being attached with rotational pin, the second electric pushrod upper end is connected with the second spherical hinge, and the second spherical hinge is solid by the second connection post
Being scheduled on the lower surface of moving platform, the second vibrating spring is around being enclosed within the second electric pushrod；A direction can be carried out by rotational pin
Rotation, the rotation in three directions can be carried out by the second spherical hinge, can be moved up and down by the second electric pushrod, second
Side chain uses the form of 2-RPS parallel institution, and when adding second chain movement by the second vibrating spring damping performance,
Improve the damping effect of the present invention；Four-degree-of-freedom is constituted symmetrical by fixed platform, moving platform, the first side chain and the second side chain
Redundancy parallel mechanism, and it uses the parallel institution form of 2-UPS-2-RPS, its can realize moving along X-axis and Z axis and around
X-axis and the motion in rotation totally four the degree of freedom directions around Y-axis, and four degree of freedom are all independent, also may be used by four degree of freedom
With co-ordination, the moving platform track made is along the curvilinear motion of predetermined space, stable movement, and motion is flexible, when unmanned plane lands
During stop, though UAV Attitude unstable or skewed time, redundancy parallel mechanism pass through the first side chain and the sky of the second side chain
Between move, reach the elimination of displacement difference during unmanned plane landing and supplement, thus serving the good result of damping, it is ensured that be unmanned
The machine stability when dropping to stop pedestal, jitter is little, the vibration damage to unmanned aerial vehicle body when reducing landing.
Further, described damping includes mounting post, lower mounting post and damping stage clip；Described upper mounting post and lower peace
The dress the most T-shaped structure of post, upper mounting post upper end and lower mounting post lower end be provided with external screw thread respectively, upper mounting post lower end and under
Mounting post upper end is provided with lock sleeve respectively, uses the mode of threaded engagement to carry out even between upper mounting post upper end and upper fixed seat
Connecing, between lower mounting post lower end and lower fixed seat, the mode also by threaded engagement is attached, and damping stage clip two ends are respectively mounted
In upper mounting post lower end and lower mounting post upper end；Damping serves the effect of secondary shock-absorbing to damping device so that damping fills
Putting the effect with dual shock absorption, damping performance is greatly improved.
Further, described support means include connect seat, sleeve, adjusting screw rod, movable plate, Rotational Cylindrical, bidirectional tension rod,
Support seat, photovoltaic battery panel and clamping screw；Described connection seat is crescent shape structure, and sleeve and adjusting screw rod quantity are two,
Sleeve bottom end is respectively symmetrically along the central transverse axis connecting seat and is fixed on connection seat, and sleeve top end is provided with and adjusting screw rod
The internal thread hole matched, adjusting screw rod one end is arranged on inside the internal thread hole of sleeve top end, the adjusting screw rod other end and shifting
Dynamic plate is connected, and movable plate upper end center position is provided with vertical duction hole, and Rotational Cylindrical lower end is arranged on movable plate upper end center
In the vertical duction hole of position, Rotational Cylindrical upper end is provided with and is horizontally diverted hole, is arranged on Rotational Cylindrical upper end in the middle part of bidirectional tension rod
It is horizontally diverted in hole, and bidirectional tension rod two ends adjustable length, supporting seat quantity is two, supports seat and is fixed on bidirectional tension rod outboard end,
Supporting and offer square draw-in groove on seat, support the equally spaced spacing hole that offers on seat front/rear end, photovoltaic battery panel assigns into and props up
In the square draw-in groove of support seat, and clamping screw between photovoltaic battery panel and support seat, is used to be attached；Permissible by adjusting screw rod
Change the distance that stretches laterally of support means, it is adaptable to the use in different places, and support means in horizontal plane and hang down
Face directly and interior all can rotate, such that it is able to the angle that adjusting supporting device is in horizontal plane and in vertical, and then can change
Become the angle of photovoltaic battery panel comparison sunlight, effectively raise the power that absorbs solar energy of photovoltaic battery panel, in addition,
Two spacing supported between seat can be regulated by bidirectional tension rod, it is simple to the photovoltaic battery panel of different model size is installed, be suitable for
Property wider, support means uses the form of cascaded structure, can carry out a translation two and rotate the motion on three degree of freedom direction altogether,
Angular can be regulated at any time, improve solar energy and change into the efficiency of electric energy, and be applicable to the photovoltaic of different model size
Cell panel.
Further, described stop base bottom is octagon slab construction, and stops the left and right sides of pedestal upper surface respectively
Symmetry offers semicircle screens groove, the unmanned plane dropped on stop pedestal can be carried out position by semicircle screens groove solid
Fixed, the center position stopping pedestal upper surface offers circular hole, and the outside stopping pedestal is provided with surrounding edge, outside surrounding edge successively
Being evenly arranged with signal lights, signal lights serves the effect at night to position indicating of the present invention.
Further, described charging device includes battery case, lithium battery, conduit, connecting line and adjustable recharging base；Described
Lithium battery be arranged in battery case, conduit one end is fixed on above lithium battery, the conduit other end through stop base central
The circular hole of position, conduit uses rubber hose, and connecting line and adjustable recharging base quantity are two, and adjustable recharging base divides
Not being symmetrically mounted on both sides before and after conduit, connecting line lower end is connected with lithium battery, connecting line upper end and adjustable recharging base phase
Connect.
Further, described adjustable recharging base include base plate, lock-screw, longitudinal electric push rod, lifter plate, vertical guide rail,
Slide block, transverse electric push rod and charging contact, longitudinal electric push rod, slide block, transverse electric push rod and the number of charging contact
Amount is two；Described base plate is fixed on stop pedestal by lock-screw, and longitudinal electric push rod is respectively along the longitudinal direction of base plate
Mandrel line is arranged symmetrically in the lock-screw left and right sides, and longitudinal electric push rod bottom is connected with base plate, longitudinal electric push rod top
Being connected with lifter plate, vertical guide rail is fixed on lifter plate upper surface, and slide block is arranged on vertical guide rail front, and transverse electric pushes away
Bar one end is connected with slide block, and the transverse electric push rod other end is connected with charging contact；Adjustable recharging base is on the vertical plane
Highly can regulate, and lateral attitude and lengthwise position all can regulate in the horizontal plane, go for different type of machines unmanned plane
Charging, during charging, para-position is convenient and swift, and uses many chargings contact to charge, and charge efficiency is high.
Compared with prior art, the invention have the advantages that
(1) present invention integrates photovoltaic energy storage, dual shock absorption, stop fixes and multistation charges, it is achieved that one-machine-multi-function
Effect, solves the unmanned plane energy and supplements difficulty and expend big problem, improve the cruising time of unmanned plane, improve unmanned
The ability of machine operation.
(2) damping device of the present invention uses redundancy parallel mechanism and damping, has dual shock absorption effect, and redundant parallel
Mechanism uses the parallel institution form of 2-UPS-2-RPS, and it can realize moving along X-axis and Z axis and around X-axis with around Y-axis
Rotate the motion in totally four degree of freedom directions, and four degree of freedom be all independent, by four degree of freedom can also co-ordination, make
Moving platform track along the curvilinear motion of predetermined space, stable movement, motion flexibly, when unmanned plane landing is stopped, though nothing
Man-machine attitude unstable or skewed time, redundancy parallel mechanism pass through the first side chain and the space motion of the second side chain, reach nothing
The elimination of displacement difference and supplementing during man-machine landing, thus serves the good result of damping, it is ensured that unmanned plane is stopped dropping to
Stability during pedestal, jitter is little, the vibration damage to unmanned aerial vehicle body when reducing landing.
(3) support means of the present invention uses the form of cascaded structure, can carry out on a translation two rotation three degree of freedom direction altogether
Motion, angular can be regulated at any time, improves solar energy and change into the efficiency of electric energy, and be applicable to different model chi
Very little photovoltaic battery panel.
(4) charging device of the present invention the most highly can regulate, and lateral attitude and lengthwise position are equal in the horizontal plane
Can regulate, go for the charging of different type of machines unmanned plane, during charging, para-position is convenient and swift, and uses many chargings contact
Charging, charge efficiency is high.
Accompanying drawing explanation
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the perspective view of the present invention；
Fig. 2 is the perspective view of damping device of the present invention；
Fig. 3 is the perspective view (seeing from front to back) of support means of the present invention；
Fig. 4 is the perspective view (seeing from back to front) of support means of the present invention；
Fig. 5 is charging device of the present invention and stops perspective view when pedestal coordinates；
Fig. 6 is the perspective view of redundancy parallel mechanism of the present invention；
The perspective view of Fig. 7 present invention is adjustable recharging base.
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and be easy to understand with effect, below in conjunction with tool
Body illustrates, and the present invention is expanded on further.
As shown in Figures 1 to 7, a kind of energy-saving unmanned plane energy ancillary equipment, including damping device 1, support means 2, stops
By pedestal 3 and charging device 4；Described support means 2 quantity is eight, and support means 2 is along the central axis of damping device 1
Lay respectively at damping device 1 outboard end, and be attached by bolt between support means 2 and damping device 1, stop pedestal
3 are positioned at directly over damping device 1, and stop between pedestal 3 and damping device 1 connected, and charging device 4 is positioned at stop pedestal 3
Top.
As in figure 2 it is shown, described damping device 1 includes lower fixed seat 11, upper fixed seat 12, redundancy parallel mechanism 13 and subtracts
Shake mechanism 14；Described redundancy parallel mechanism 13 is between lower fixed seat 11 and upper fixed seat 12, and redundancy parallel mechanism
13 lower ends are connected with lower fixed seat 11, and redundancy parallel mechanism 13 upper end is connected with upper fixed seat 12, damping 14 number
Amount is eight, and damping 14 lays respectively at outside redundancy parallel mechanism 13, and damping 14 is along redundancy parallel mechanism 13
Central axis is uniformly arranged circumferentially about.
As shown in Figure 6, the redundancy parallel mechanism 13 stated includes fixed platform 131, moving platform the 132, first side chain 133 and second
Side chain 134；Described fixed platform 131 and moving platform 132 are disc-shaped structure, and moving platform 132 is positioned at fixed platform 131
Surface；The first described side chain 133 and the quantity of the second side chain 134 are two, the first side chain 133 and the second side chain 134
Be respectively positioned between fixed platform 131 and moving platform 132, the two ends of the first side chain 133 and the second side chain 134 respectively with fixed platform
131 are connected with moving platform 132, and the horizontal installation angle of the first side chain 133 and the second side chain 134 is 90 degree；Described
First side chain 133 include the first ear mount 1331, Hooke's hinge the 1332, first electric pushrod the 1333, first spherical hinge 1334,
One connects post 1335 and the first vibrating spring 1336；The first described ear mount 1331 is fixed on fixed platform 131 upper surface, the
Hooke's hinge 1332 is used to be attached between one ear mount 1331 and the first electric pushrod 1333 lower end, the first electric pushrod 1333
Upper end is connected with the first spherical hinge 1334, and the first spherical hinge 1334 is fixed on moving platform 132 by the first connection post 1335
On lower surface, the first vibrating spring 1336 is around being enclosed within the first electric pushrod 1333；Two sides can be carried out by Hooke's hinge 1332
To rotation, the rotation in three directions can be carried out by the first spherical hinge 1334, can be carried out by the first electric pushrod 1333 on
Lower movement, the first side chain 133 uses the form of 2-UPS parallel institution, and adds first by the first vibrating spring 1336
The damping performance of chain 133, improves the damping effect of the present invention；The second described side chain 134 includes the second ear mount 1341, turns
Untie-sell the 1342, second electric pushrod the 1343, second spherical hinge 1344, second connects post 1345 and the second vibrating spring 1346；
The second described ear mount 1341 is fixed on fixed platform 131 upper surface, the second ear mount 1341 and the second electric pushrod 1343 lower end
Between use rotational pin 1342 be attached, the second electric pushrod 1343 upper end is connected with the second spherical hinge 1344, the second ball
Hinge 1344 is fixed on the lower surface of moving platform 132 by the second connection post 1345, and the second vibrating spring 1346 is around being enclosed within the
On two electric pushrods 1343；The rotation in a direction can be carried out by rotational pin 1342, can be carried out by the second spherical hinge 1344
The rotation in three directions, can be moved up and down by the second electric pushrod 1343, and the second side chain 134 uses 2-RPS parallel machine
The form of structure, and by the second vibrating spring 1346 add when the second side chain 134 moves damping performance, improve this
Bright damping effect；Four-degree-of-freedom is constituted by fixed platform 131, moving platform the 132, first side chain 133 and the second side chain 134
Symmetrical redundancy parallel mechanism 13, and it uses the parallel institution form of 2-UPS-2-RPS, it can realize moving along X-axis and Z axis
And around X-axis and the motion in rotation totally four the degree of freedom directions around Y-axis, and four degree of freedom are all independent, by four freedom
Degree can also co-ordination, the moving platform track made along the curvilinear motion of predetermined space, stable movement, motion flexibly, when unmanned
When machine landing is stopped, though UAV Attitude unstable or skewed time, redundancy parallel mechanism 13 is by the first side chain 133 He
The space motion of the second side chain 134, reaches the elimination of displacement difference during unmanned plane landing and supplements, thus serving the good of damping
Effect, it is ensured that the unmanned plane stability when dropping to stop pedestal 3, jitter is little, and when reducing landing, vibration is to unmanned
The damage of machine fuselage.
As in figure 2 it is shown, described damping 14 includes mounting post 141, lower mounting post 142 and damping stage clip 143；Institute
The upper mounting post 141 stated and the lower the most T-shaped structure of mounting post 142, upper mounting post 141 upper end and lower mounting post 142 lower end are equal
It is respectively arranged with external screw thread, upper mounting post 141 lower end and lower mounting post 142 upper end and is provided with lock sleeve, upper mounting post respectively
The mode using threaded engagement between 141 upper ends and upper fixed seat 12 is attached, lower mounting post 142 lower end and lower fixed seat 11
Between be attached also by the mode of threaded engagement, damping stage clip 143 two ends be separately mounted to mounting post 141 lower end and under
Mounting post 142 upper end；Damping 14 serves the effect of secondary shock-absorbing to damping device so that damping device 1 has dual
The effect of damping, damping performance is greatly improved.
As shown in Figure 3 and Figure 4, described support means 2 includes connecting seat 21, sleeve 22, adjusting screw rod 23, movable plate
24, Rotational Cylindrical 25, bidirectional tension rod 26, support seat 27, photovoltaic battery panel 28 and clamping screw 29；Described connection seat 21
In crescent shape structure, sleeve 22 and adjusting screw rod 23 quantity are two, and sleeve 22 bottom is along the transverse central axis connecting seat 21
Line is respectively symmetrically and is fixed on connection seat 21, and sleeve 22 top end is provided with the internal thread hole matched with adjusting screw rod 23, adjusts
Joint screw rod 23 one end is arranged on inside the internal thread hole of sleeve 22 top end, and adjusting screw rod 23 other end is connected with movable plate 24
Connecing, movable plate 24 upper end center position is provided with vertical duction hole, and Rotational Cylindrical 25 lower end is arranged on movable plate 24 upper end center
In the vertical duction hole of position, Rotational Cylindrical 25 upper end is provided with and is horizontally diverted hole, is arranged on Rotational Cylindrical in the middle part of bidirectional tension rod 26
Being horizontally diverted in hole of 25 upper ends, and bidirectional tension rod 26 two ends adjustable length, supporting seat 27 quantity is two, supports seat 27 solid
It is scheduled on bidirectional tension rod 26 outboard end, supports and on seat 27, offer square draw-in groove, support equally spaced on seat 27 front/rear end offering
Limited location hole, photovoltaic battery panel 28 assigns in the square draw-in groove supporting seat 27, and photovoltaic battery panel 28 with support seat 27 it
Between use clamping screw 29 be attached；The distance that support means 2 stretches laterally can be changed by adjusting screw rod 23, suitable
For the use in different places, and and all can the rotating in vertical in horizontal plane of support means 2, such that it is able to
The adjusting supporting device 2 angle in horizontal plane and in vertical, and then photovoltaic battery panel 28 can be changed compare the angle of sunlight
Degree, is effectively raised the power that absorbs solar energy of photovoltaic battery panel 28, in addition, can be regulated by bidirectional tension rod 26
Two spacing supported between seat 27, it is simple to install the photovoltaic battery panel 28 of different model size, the suitability is wider, supports dress
Put the form of 2 employing cascaded structures, a translation two can be carried out and rotate the motion on altogether three degree of freedom direction, can be with to angular
Time regulation, improve solar energy and change into the efficiency of electric energy, and be applicable to the photovoltaic battery panel 28 of different model size.
As it is shown in figure 5, described stop pedestal 3 bottom is octagon slab construction, and stop the left and right of pedestal 3 upper surface
Both sides are respectively symmetrically and offer semicircle screens groove, can be to dropping to stop the unmanned plane on pedestal 3 by semicircle screens groove
Carrying out position to fix, the center position stopping pedestal 3 upper surface offers circular hole, and the outside stopping pedestal 3 is provided with surrounding edge,
Being evenly arranged with signal lights outside surrounding edge successively, signal lights serves the effect at night to position indicating of the present invention.
As shown in figure 5 and figure 7, described charging device 4 includes battery case 41, lithium battery 42, conduit 43, connecting line
44 and adjustable recharging base 45；Described lithium battery 42 is arranged in battery case 41, and conduit 43 one end is fixed on lithium battery
Above in the of 42, conduit 43 other end is through the circular hole of stop pedestal 45 center position, and conduit 43 uses rubber hose,
Connecting line 44 and adjustable recharging base 45 quantity are two, and adjustable recharging base 45 is respectively symmetrically before and after being arranged on conduit 43
Both sides, connecting line 44 lower end is connected with lithium battery 42, and connecting line 44 upper end is connected with adjustable recharging base 45.
As shown in Figure 5 and Figure 6, described adjustable recharging base 45 includes that base plate 451, lock-screw 452, longitudinal electric push away
Bar 453, lifter plate 454, vertical guide rail 455, slide block 456, transverse electric push rod 457 and charging contact 458, longitudinally
The quantity of electric pushrod 453, slide block 456, transverse electric push rod 457 and charging contact 458 is two；Described base plate
451 are fixed on stop pedestal 3 by lock-screw 452, and longitudinal electric push rod 453 is respectively along the longitudinal center of base plate 451
Axisymmetrical is arranged in lock-screw 452 left and right sides, and longitudinal electric push rod 453 bottom is connected with base plate 451, longitudinally electricity
Dynamic push rod 453 top is connected with lifter plate 454, and vertical guide rail 455 is fixed on lifter plate 454 upper surface, slide block 456
Being arranged on vertical guide rail 455 front, transverse electric push rod 457 one end is connected with slide block 456, and transverse electric push rod 457 is another
One end is connected with charging contact 458；Adjustable recharging base 45 the most highly can regulate, and horizontal in the horizontal plane
All can regulate to position and lengthwise position, go for the charging of different type of machines unmanned plane, during charging, para-position is convenient and swift,
And using many chargings contact to charge, charge efficiency is high.
The ultimate principle of the present invention, principal character and advantage have more than been shown and described.Skilled person will appreciate that of the industry,
The present invention is not restricted to the described embodiments, the principle that the present invention is simply described of the description in above-described embodiment and description,
Without departing from the spirit and scope, the present invention also has various changes and modifications, and these changes and improvements both fall within
In scope of the claimed invention.Claimed scope is defined by appending claims and equivalent thereof.
Claims (5)
1. an energy-saving unmanned plane energy ancillary equipment, it is characterised in that: include damping device, support means, stop pedestal
And charging device；Described support means quantity is eight, and support means lays respectively at damping device along the central axis of damping device
It is attached by bolt between outboard end, and support means and damping device, stops pedestal and be positioned at directly over damping device, and
Stopping and be connected between pedestal and damping device, charging device is positioned at above stop pedestal；Wherein:
Described damping device includes lower fixed seat, upper fixed seat, redundancy parallel mechanism and damping；Described redundant parallel
Mechanism is between lower fixed seat and upper fixed seat, and redundancy parallel mechanism lower end is connected with lower fixed seat, redundancy parallel mechanism
Upper end is connected with upper fixed seat, and damping quantity is eight, and damping lays respectively at outside redundancy parallel mechanism, and damping
Mechanism is uniformly arranged circumferentially about along the central axis of redundancy parallel mechanism；
Described redundancy parallel mechanism includes fixed platform, moving platform, the first side chain and the second side chain；Described fixed platform is flat with dynamic
Platform is disc-shaped structure, and moving platform is positioned at directly over fixed platform；The first described side chain and the quantity of the second side chain are two,
First side chain and the second side chain are respectively positioned between fixed platform and moving platform, the two ends of the first side chain and the second side chain respectively with allocate
Platform is connected with moving platform, and the horizontal installation angle of the first side chain and the second side chain is 90 degree；
The first described side chain includes the first ear mount, Hooke's hinge, the first electric pushrod, the first spherical hinge, first connects post and the
One vibrating spring；The first described ear mount is fixed on fixed platform upper surface, adopts between the first ear mount and the first electric pushrod lower end
Being attached with Hooke's hinge, the first electric pushrod upper end is connected with the first spherical hinge, and the first spherical hinge is solid by the first connection post
Being scheduled on the lower surface of moving platform, the first vibrating spring is around being enclosed within the first electric pushrod；
Described support means include connect seat, sleeve, adjusting screw rod, movable plate, Rotational Cylindrical, bidirectional tension rod, support seat,
Photovoltaic battery panel and clamping screw；Described connection seat is crescent shape structure, and sleeve and adjusting screw rod quantity are two, at the bottom of sleeve
End is respectively symmetrically along the central transverse axis connecting seat and is fixed on connection seat, and sleeve top end is provided with and matches with adjusting screw rod
Internal thread hole, adjusting screw rod one end is arranged on inside the internal thread hole of sleeve top end, the adjusting screw rod other end and movable plate phase
Connecting, movable plate upper end center position is provided with vertical duction hole, and Rotational Cylindrical lower end is arranged on movable plate upper end center position
Vertical duction hole in, Rotational Cylindrical upper end is provided with and is horizontally diverted hole, and the level being arranged on Rotational Cylindrical upper end in the middle part of bidirectional tension rod turns
In hole, and bidirectional tension rod two ends adjustable length, supporting seat quantity is two, supports seat and is fixed on bidirectional tension rod outboard end, supports
Offering square draw-in groove on Zuo, support the equally spaced spacing hole that offers on seat front/rear end, photovoltaic battery panel assigns into support seat
Square draw-in groove in, and between photovoltaic battery panel and support seat use clamping screw be attached；
Described charging device includes battery case, lithium battery, conduit, connecting line and adjustable recharging base；Described lithium battery
Being arranged in battery case, conduit one end is fixed on above lithium battery, and the conduit other end is through stopping base central position
Circular hole, connecting line and adjustable recharging base quantity are two, and adjustable recharging base is respectively symmetrically and is arranged on both sides before and after conduit,
Connecting line lower end is connected with lithium battery, and connecting line upper end is connected with adjustable recharging base.
One the most according to claim 1 energy-saving unmanned plane energy ancillary equipment, it is characterised in that: described damping machine
Structure includes mounting post, lower mounting post and damping stage clip；Described upper mounting post and the lower the most T-shaped structure of mounting post, upper installation
Post upper end and lower mounting post lower end are provided with external screw thread, upper mounting post lower end and lower mounting post upper end respectively and are provided with lock respectively
Tight set, uses the mode of threaded engagement to be attached between upper mounting post upper end and upper fixed seat, and lower mounting post lower end is fixing with lower
Between Zuo, the mode also by threaded engagement is attached, and damping stage clip two ends are separately mounted to mounting post lower end and lower mounting post
Upper end.
One the most according to claim 1 energy-saving unmanned plane energy ancillary equipment, it is characterised in that: described stop base
Seat bottom end is octagon slab construction, and the left and right sides stopping pedestal upper surface is respectively symmetrically and offers semicircle screens groove,
The center position stopping pedestal upper surface offers circular hole, and the outside stopping pedestal is provided with surrounding edge, the most uniform outside surrounding edge
It is provided with signal lights.
One the most according to claim 1 energy-saving unmanned plane energy ancillary equipment, it is characterised in that: described adjustable fill
Electricity pedestal includes base plate, lock-screw, longitudinal electric push rod, lifter plate, vertical guide rail, slide block, transverse electric push rod and fills
Electrical contact head, the quantity of longitudinal electric push rod, slide block, transverse electric push rod and charging contact is two；Described base plate leads to
Crossing lock-screw to be fixed on stop pedestal, longitudinal electric push rod is arranged symmetrically in locking screw along longitudinal center's axis of base plate respectively
The nail left and right sides, and longitudinal electric push rod bottom is connected with base plate, longitudinal electric push rod top is connected with lifter plate, vertically leads
Rail is fixed on lifter plate upper surface, and slide block is arranged on vertical guide rail front, and transverse electric push rod one end is connected with slide block, horizontal
It is connected with charging contact to the electric pushrod other end.
One the most according to claim 1 energy-saving unmanned plane energy ancillary equipment, it is characterised in that: described second
Chain includes the second ear mount, rotational pin, the second electric pushrod, the second spherical hinge, the second connection post and the second vibrating spring；Described
The second ear mount be fixed on fixed platform upper surface, between the second ear mount and the second electric pushrod lower end use rotational pin be attached,
Second electric pushrod upper end is connected with the second spherical hinge, and the second spherical hinge connects post by second and is fixed on the lower surface of moving platform
On, the second vibrating spring is around being enclosed within the second electric pushrod.
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| CN201610491227.XA CN106005464B (en) | 2016-06-28 | 2016-06-28 | A kind of energy-saving unmanned plane energy ancillary equipment |
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| CN106005464B (en) | 2017-12-19 |
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Inventor after: Shi Guanghong Inventor before: Wu Yan |
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Effective date of registration: 20171115 Address after: 221400 Xuzhou, Jiangsu City, Xinyi province Xinyi Economic Development Zone, latitude five road north, seven Road East Applicant after: Jiangsu Hong Han Biological Technology Co., Ltd. Address before: 246001 Xinzhou in Anhui province Anqing City Yingjiang District Town Comprehensive Building 3 floor Applicant before: Anqing Baisite Electronic Technology Co., Ltd. |
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