CN110406668A - A kind of easy to maintain solar energy unmanned plane with pooling feature - Google Patents
A kind of easy to maintain solar energy unmanned plane with pooling feature Download PDFInfo
- Publication number
- CN110406668A CN110406668A CN201910625182.4A CN201910625182A CN110406668A CN 110406668 A CN110406668 A CN 110406668A CN 201910625182 A CN201910625182 A CN 201910625182A CN 110406668 A CN110406668 A CN 110406668A
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- China
- Prior art keywords
- connecting rod
- unmanned plane
- main body
- solar panels
- block
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
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- 238000011176 pooling Methods 0.000 title claims abstract description 22
- 230000007246 mechanism Effects 0.000 claims abstract description 38
- 238000009434 installation Methods 0.000 claims description 11
- 239000011248 coating agent Substances 0.000 claims description 4
- 238000000576 coating method Methods 0.000 claims description 4
- 230000007797 corrosion Effects 0.000 claims description 4
- 238000005260 corrosion Methods 0.000 claims description 4
- 239000004519 grease Substances 0.000 claims description 4
- 230000002401 inhibitory effect Effects 0.000 claims description 4
- 230000001050 lubricating effect Effects 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 3
- 230000003139 buffering effect Effects 0.000 abstract description 4
- 238000012423 maintenance Methods 0.000 abstract description 4
- 230000000694 effects Effects 0.000 description 5
- 230000006870 function Effects 0.000 description 5
- 230000009471 action Effects 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000010297 mechanical methods and process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B64D27/40—
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24S—SOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
- F24S25/00—Arrangement of stationary mountings or supports for solar heat collector modules
- F24S25/60—Fixation means, e.g. fasteners, specially adapted for supporting solar heat collector modules
- F24S25/63—Fixation means, e.g. fasteners, specially adapted for supporting solar heat collector modules for fixing modules or their peripheral frames to supporting elements
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S20/00—Supporting structures for PV modules
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/40—Solar thermal energy, e.g. solar towers
- Y02E10/47—Mountings or tracking
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
Abstract
The present invention relates to a kind of easy to maintain solar energy unmanned plane with pooling feature, including main body, solar panels and four flight instruments, it further include installing mechanism and four supporting mechanisms, the installing mechanism includes cylindrical recess, friction block, drive rod, guide rail, drive block, driving assembly and two fixation kits, the supporting mechanism includes hinge assembly, slide bar, sliding block, first connecting rod, second connecting rod, third connecting rod and two springs, the fixation kit includes fixed strip, connection strap and strip groove, the hinge assembly includes connecting shaft, connecting sleeve and two fixed blocks, in the easy to maintain solar energy unmanned plane with pooling feature, the convenient degree of solar panels dismounting is improved by installing mechanism, improve the convenient degree of unmanned plane maintenance, improve the practicability of unmanned plane, made by the buffering of supporting mechanism With the impact force being subject to when reducing UAV Landing reduces the probability that unmanned plane is damaged.
Description
Technical field
The present invention relates to photovoltaic apparatus field, in particular to a kind of easy to maintain solar energy with pooling feature
Unmanned plane.
Background technique
UAV is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself,
Or fully or intermittently automatically operated by car-mounted computer, compared with manned aircraft, unmanned plane is often more suitable for
Those dirty or dangerous tasks, unmanned plane press application field, can be divided into military with civilian, military aspect, and unmanned plane, which is divided into, to be detectd
Machine and target drone, civilian aspect are examined, unmanned plane industrial application is that unmanned plane has really just needed, currently in order to extending the continuous of unmanned plane
ETS estimated time of sailing usually installs solar panels on unmanned plane.
The solar energy unmanned plane of the prior art is hit, due to nobody in the moment of landing between unmanned plane and ground
Machine does not have effective buffer unit, and unmanned plane is caused to be easy to happen damage, moreover, the solar energy unmanned plane of the prior art
Solar panels are fixedly mounted on unmanned plane, and after solar panels are damaged, solar panels replacement is more difficult, are reduced
The practicability of unmanned plane.
Summary of the invention
The technical problem to be solved by the present invention is for overcome the deficiencies in the prior art, providing a kind of with pooling feature
Easy to maintain solar energy unmanned plane.
The technical solution adopted by the present invention to solve the technical problems is: a kind of easy to maintain sun with pooling feature
Energy unmanned plane, including main body, solar panels and four flight instruments, four flight instruments are circumferentially uniformly arranged on the top of main body
Surrounding, further include installing mechanism and four supporting mechanisms, the close of main body is arranged in by installing mechanism in the solar panels
The side of flight instruments, four supporting mechanisms are circumferentially uniformly arranged on the surrounding of the bottom end of main body；
The installing mechanism includes cylindrical recess, friction block, drive rod, guide rail, drive block, driving assembly and two fixations
Component, two connection components are separately positioned on the two sides of the face of solar panels, and the solar panels pass through connection component and master
Body connection, the axis of the cylindrical recess is vertical with solar panels, and the close solar panels of main body are arranged in the cylindrical recess
Side, the friction block is arranged in the inside of the opening of cylindrical recess, and the inner wall of the friction block and cylindrical recess, which slides, to be connected
It connects, the friction block and solar panels are against the guide rail is vertical with the axis of cylindrical recess and intersects, the both ends of the guide rail
It is fixedly connected with the inner wall of cylindrical recess, the inside of the drive block is equipped with through-hole, and the guide rail passes through drive block, the drive
Motion block is slidably connected with guide rail, and one end of the drive rod and drive block are hinged, the other end of the drive rod and friction block
One end far from solar panels is hinged, and the side of guide rail is arranged in the driving component, and the driving component is connect with drive block；
The supporting mechanism include hinge assembly, slide bar, sliding block, first connecting rod, the second connecting rod, third connecting rod and
Two springs, the slide bar is vertical with solar panels, and the both ends of the slide bar are fixedly connected with main body, the inside of the sliding block
Equipped with through hole, the slide bar passes through sliding block, and the sliding block is connect with sliding bar, and two springs are set on slide bar, institute
The both ends for stating slide bar are fixedly connected with a slide block by spring, and second connecting rod is vertical with slide bar, second connecting rod
One end connect with main body by hinge assembly, the third connecting rod is vertical with the second connecting rod, and the third connecting rod is set
It sets in the side of the separate slide bar of the second connecting rod, the fixed company of the other end of second connecting rod and one end of third connecting rod
It connects, the other end of second connecting rod and one end of first connecting rod are hinged, the other end and sliding block of the first connecting rod
Hingedly, the first connecting rod, the second connecting rod, third connecting rod and slide bar are in same plane.
Preferably, in order to improve the degree of automation of unmanned plane, the inside of the main body is equipped with wireless signal folding and unfolding mould
Block and PLC, the wireless signal transceiver module are electrically connected with PLC.
Preferably, the driving component includes motor and screw rod in order to give drive block to provide power, the screw rod with lead
Rail is parallel, and the both ends of the screw rod are equipped with installation bearing, and the both ends of the screw rod pass through installation bearing and connect with guide rail, institute
Screw rod is stated across drive block, the screw rod is threadedly coupled with drive block, and the motor is fixedly connected with guide rail, the motor and silk
Bar transmission connection.
Preferably, in order to improve solar panels dismounting convenient degree, the fixation kit include fixed strip, connection strap and
The side of solar panels is arranged in strip groove, the fixed strip, and the fixed strip is fixedly connected with main body, the strip groove setting
In the side of the close solar panels of fixed strip, the side of the close fixed strip of solar panels is arranged in the connection strap, described
Connection strap is matched with strip groove, and the inside of strip groove is arranged in the connection strap.
Preferably, in order to improve solar panels installation firmness, the side of the separate main body of the strip groove it is interior
Wall is equipped with tread plate.
Preferably, in order to increase the coefficient of friction of friction block, the making material of the friction block is rubber.
Preferably, in order to improve the stability of the second connecting rod, the hinge assembly include connecting shaft, connecting sleeve and
Two fixed blocks, the connecting shaft and first connecting rod and the second connecting rod are vertical, and the both ends of the connecting shaft pass through solid
Determine block to be fixedly connected with one end of the close slide bar of the side of the separate solar panels of main body, the connecting sleeve and connecting shaft are same
Axis setting, the connecting shaft pass through connecting sleeve, the fixed company in one end of the connecting sleeve and the close main body of the second connecting rod
It connects.
Preferably, being coated with lubricating grease on the slide bar to improve sliding block mobile smooth degree.
Preferably, in order to improve the buffering effect to unmanned plane, one end of the separate main body of the third connecting rod is set
There is air bag.
Preferably, being coated with corrosion-inhibiting coating in the main body to extend the service life of unmanned plane.
The invention has the advantages that this has in the easy to maintain solar energy unmanned plane of pooling feature, pass through fitting machine
Structure improves the convenient degree of solar panels dismounting, improves the convenient degree of unmanned plane maintenance, improves the practicability of unmanned plane, with
Existing installing mechanism is compared, and the installing mechanism structure is simple, is reduced the quantity of the mechanism-trouble point, is reduced the event of the mechanism
Barrier rate, moreover, by the buffer function of supporting mechanism, the impact force being subject to when reducing UAV Landing reduces nothing
The man-machine probability being damaged, compared with existing supporting mechanism, which is made by the mutual redundancy between two springs
When one of spring failure, another spring can support unmanned plane to continue to run, and improve the reality of unmanned plane
The property used.
Detailed description of the invention
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is the structural schematic diagram of the easy to maintain solar energy unmanned plane with pooling feature of the invention；
Fig. 2 is the structural representation of the supporting mechanism of the easy to maintain solar energy unmanned plane with pooling feature of the invention
Figure；
Fig. 3 is the portion the A enlarged drawing of Fig. 1；
Fig. 4 is the portion the B enlarged drawing of Fig. 1；
In figure: 1. flight instruments, 2. solar panels, 3. main bodys, 4. first connecting rods, 5. second connecting rods, 6. thirds connect
Extension bar, 7. sliding blocks, 8. slide bars, 9. springs, 10. connecting sleeves, 11. connecting shafts, 12. fixed blocks, 13. fixed strips, 14. bar shapeds
Slot, 15. connection straps, 16. friction blocks, 17. drive rods, 18. guide rails, 19. screw rods, 20. drive blocks, 21. cylindrical recess, 22. electricity
Machine.
Specific embodiment
In conjunction with the accompanying drawings, the present invention is further explained in detail.These attached drawings are simplified schematic diagram, only with
Illustration illustrates basic structure of the invention, therefore it only shows the composition relevant to the invention.
As shown in Figure 1, a kind of easy to maintain solar energy unmanned plane with pooling feature, including main body 3, solar panels 2
With four flight instruments 1, the surrounding on the circumferential top for being uniformly arranged on main body 3 of four flight instruments 1, further include installing mechanism and
The side of the close flight instruments 1 of main body 3, four branch are arranged in by installing mechanism for four supporting mechanisms, the solar panels 2
Support mechanism is circumferentially uniformly arranged on the surrounding of the bottom end of main body 3；
The convenient degree that the dismounting of solar panels 2 is improved by installing mechanism improves the convenient degree of unmanned plane maintenance, improves
The practicability of unmanned plane, moreover, by the buffer function of supporting mechanism, the impact being subject to when reducing UAV Landing
Power reduces the probability that unmanned plane is damaged；
As shown in Figure 3-4, the installing mechanism includes cylindrical recess 21, friction block 16, drive rod 17, guide rail 18, driving
Block 20, driving assembly and two fixation kits, two connection components are separately positioned on the two sides of the face of solar panels 2, described
Solar panels 2 are connect by connection component with main body 3, and the axis of the cylindrical recess 21 is vertical with solar panels 2, the cylindricality
The side of the close solar panels 2 of main body 3 is arranged in recess 21, and the friction block 16 is arranged in the opening of cylindrical recess 21
The inner wall in portion, the friction block 16 and cylindrical recess 21 is slidably connected, and the friction block 16 is with solar panels 2 against described to lead
Rail 18 is vertical with the axis of cylindrical recess 21 and intersects, and the both ends of the guide rail 18, which are fixed with the inner wall of cylindrical recess 21, to be connected
It connects, the inside of the drive block 20 is equipped with through-hole, and the guide rail 18 passes through drive block 20, and the drive block 20 is slided with guide rail 18
Connection, one end of the drive rod 17 and drive block 20 are hinged, and the other end of the drive rod 17 is with friction block 16 far from too
One end of positive energy plate 2 is hinged, and the side of guide rail 18 is arranged in the driving component, and the driving component is connect with drive block 20；
After solar panels 2 are installed between two fixation kits, power is provided by driving assembly, makes drive block 20
It is moved along guide rail 18, then under the transmission effect of drive rod 17, drives friction block 16 along cylindrical recess by drive block 20
21 is mobile, after friction block 16 is resisted against on solar panels 2, the work of the frictional force between friction block 16 and solar panels 2
Under, solar panels 2 are reduced from the probability being detached between two fixation kits, improve the firmness of the installation of solar panels 2,
After friction block 16 is separated with solar panels 2, then operator can take solar panels 2 between two fixation kits
Under, improve the convenient degree of the disassembly of solar panels 2；
As shown in Fig. 2, the supporting mechanism includes hinge assembly, slide bar 8, sliding block 7, first connecting rod 4, the second connecting rod
5, third connecting rod 6 and two springs 9, the slide bar 8 is vertical with solar panels 2, and the both ends of the slide bar 8 are solid with main body 3
Fixed connection, the inside of the sliding block 7 are equipped with through hole, and the slide bar 8 passes through sliding block 7, and the sliding block 7 is slidably connected with slide bar 8,
Two springs 9 are set on slide bar 8, and the both ends of the slide bar 8 pass through spring 9 and are fixedly connected with sliding block 7, and described second connects
Extension bar 5 is vertical with slide bar 8, and one end of second connecting rod 5 is connect by hinge assembly with main body 3, the third connecting rod 6
Vertical with the second connecting rod 5, the third connecting rod 6 is arranged in the side of the separate slide bar 8 of the second connecting rod 5, and described second
The other end of connecting rod 5 is fixedly connected with one end of third connecting rod 6, and the other end of second connecting rod 5 is connect with first
One end of bar 4 is hinged, and the other end of the first connecting rod 4 and sliding block 7 are hinged, the first connecting rod 4, the second connecting rod 5,
Third connecting rod 6 and slide bar 8 are in same plane；
When UAV Landing, third connecting rod 6 and ground face contact push the second connection by third connecting rod 6
Bar 5 is rotated around hinge assembly, under the transmission effect of first connecting rod 4, drives sliding block 7 along cunning by the second connecting rod 5
Bar 8 is mobile, by spring 9 to the buffer function of sliding block 7, reduces the impact force that main body 3 is transmitted by ground, reduces nobody
The probability that machine is damaged.
Preferably, in order to improve the degree of automation of unmanned plane, the inside of the main body 3 is equipped with wireless signal folding and unfolding mould
Block and PLC, the wireless signal transceiver module are electrically connected with PLC；
PLC, that is, programmable logic controller (PLC), it is used for its internally stored program, is held using a kind of programmable memory
The user oriented instruction such as row logical operation, sequential control, timing, counting and arithmetical operation, and by digital or analog defeated
Enter/export the various types of mechanical or production processes of control, its essence is a kind of computer for being exclusively used in Industry Control, hardware
Structure is substantially identical as microcomputer, the reception and output of processing and the instruction of data is generally used for, for realizing in
Centre control is established PLC and mobile device by wireless signal transceiver module and is communicated, and operator can be remote by mobile device
Journey sends control signal to PLC, then controls unmanned plane operation by PLC, then improve the degree of automation of unmanned plane.
As shown in figure 4, the driving component includes motor 22 and screw rod 19, the screw rod 19 is parallel with guide rail 18, described
The both ends of screw rod 19 are equipped with installation bearing, and the both ends of the screw rod 19 pass through installation bearing and connect with guide rail 18, the silk
Bar 19 passes through drive block 20, and the screw rod 19 is threadedly coupled with drive block 20, and the motor 22 is fixedly connected with guide rail 18, described
Motor 22 and screw rod 19 are sequentially connected；
It drives screw rod 19 to rotate by motor 22, then drives drive block 20 to move along guide rail 18 by screw rod 19.
As shown in figure 3, the fixation kit includes fixed strip 13, connection strap 15 and strip groove 14, the fixed strip 13 is set
It sets in the side of solar panels 2, the fixed strip 13 is fixedly connected with main body 3, and fixed strip 13 is arranged in the strip groove 14
Close to the side of solar panels 2, the side of the close fixed strip 13 of solar panels 2, the connection is arranged in the connection strap 15
Item 15 is matched with strip groove 14, and the inside of strip groove 14 is arranged in the connection strap 15；
Fixed strip 13 is fixedly mounted in main body 3, by being inserted into two connection straps 15 in two strip grooves 14 respectively
Solar panels 2 can be then mounted between two fixed strips 13 by portion in strip groove 15 under the position-limiting action of connection strap 15,
Solar panels 2 are fixed by friction block 16, solar panels 2 is reduced from the probability slid between two fixed strips 13, improves
The firmness that solar panels 2 are installed.
Preferably, in order to improve the firmness of the installation of solar panels 2, the side of the separate main body 3 of the strip groove 14
Inner wall be equipped with tread plate；
After friction block 16 is resisted against on solar panels 2, the side of the separate main body 3 of connection strap 15 and strip groove 14
Inner wall is against increasing the frictional force between the inner wall of strip groove 14 and connection strap 15, reduce then under the action of tread plate
The probability that connection strap 15 slides inside strip groove 14 improves the firmness of the installation of solar panels 2.
Preferably, in order to increase the coefficient of friction of friction block 16, the making material of the friction block 16 is rubber；
Since rubber has biggish coefficient of friction, then increase the frictional force between friction block 16 and solar panels 2, improves
The stability of solar panels 2.
As shown in Fig. 2, the hinge assembly includes connecting shaft 11, connecting sleeve 10 and two fixed blocks 12, the connection
Axis 11 and first connecting rod 4 and the second connecting rod 5 are vertical, and the both ends of the connecting shaft 11 pass through fixed block 12 and main body 3
One end of close slide bar 8 of side of separate solar panels 2 be fixedly connected, the connecting sleeve 10 is coaxially set with connecting shaft 11
It sets, the connecting shaft 11 passes through connecting sleeve 10, and one end of the close main body 3 of the connecting sleeve 10 and the second connecting rod 5 is consolidated
Fixed connection；
Under the action of fixed block 12, the stability of connecting shaft 11 is improved, by connecting sleeve 10 around connecting shaft 11
Rotation rotates the second connecting rod 5 around connecting shaft 11.
Preferably, being coated with lubricating grease on the slide bar 8 to improve the mobile smooth degree of sliding block 7；
The frictional force between sliding block 7 and slide bar 8 is reduced by lubricating grease, then improves the mobile smooth degree of sliding block 7.
Preferably, in order to improve the buffering effect to unmanned plane, one end of the separate main body 3 of the third connecting rod 6
Equipped with air bag；
By the buffer function of air bag, the impact force that main body 3 is subject to is further reduced, then improves and unmanned plane is delayed
Rush effect.
Preferably, being coated with corrosion-inhibiting coating in the main body 3 to extend the service life of unmanned plane；
The speed that main body 3 is corroded is slowed down by corrosion-inhibiting coating, then extends the service life of unmanned plane.
After solar panels 2 are installed between two fixation kits, power is provided by driving assembly, makes friction block 16
Be resisted against on solar panels 2, under the action of frictional force between friction block 16 and solar panels 2, reduce solar panels 2 from
The probability being detached between two fixation kits improves the firmness of the installation of solar panels 2, when UAV Landing, the
Three connecting rods 6 and ground face contact, push the second connecting rod 5 to rotate around hinge assembly, in the first connection by third connecting rod 6
Under the transmission effect of bar 4, sliding block 7 is driven to move along slide bar 8 by the second connecting rod 5, by spring 9 to the buffering of sliding block 7
Effect, reduces the impact force that main body 3 is transmitted by ground, reduces the probability that unmanned plane is damaged.
Compared with prior art, this has in the easy to maintain solar energy unmanned plane of pooling feature, is mentioned by installing mechanism
The convenient degree that high solar panels 2 dismount, improves the convenient degree of unmanned plane maintenance, improves the practicability of unmanned plane, and existing
There is installing mechanism to compare, the installing mechanism structure is simple, reduces the quantity of the mechanism-trouble point, reduces the failure of the mechanism
Rate, moreover, by the buffer function of supporting mechanism, the impact force being subject to when reducing UAV Landing reduces nobody
The probability that machine is damaged, compared with existing supporting mechanism, which is made by the mutual redundancy between two springs 9
When one of spring 9 breaks down, another spring 9 can support unmanned plane to continue to run, and improve unmanned plane
Practicability.
Taking the above-mentioned ideal embodiment according to the present invention as inspiration, through the above description, relevant staff is complete
Various changes and amendments can be carried out without departing from the scope of the technological thought of the present invention' entirely.The technology of this invention
Property range is not limited to the contents of the specification, it is necessary to which the technical scope thereof is determined according to the scope of the claim.
Claims (10)
1. a kind of easy to maintain solar energy unmanned plane with pooling feature, including main body (3), solar panels (2) and four fly
Luggage is set (1), and four flight instruments (1) are circumferentially uniformly arranged on the surrounding on the top of main body (3), which is characterized in that further include
The close flight instruments in main body (3) are arranged by installing mechanism for installing mechanism and four supporting mechanisms, the solar panels (2)
(1) side, four supporting mechanisms are circumferentially uniformly arranged on the surrounding of the bottom end of main body (3)；
The installing mechanism includes cylindrical recess (21), friction block (16), drive rod (17), guide rail (18), drive block (20), drives
Dynamic component and two fixation kits, two connection components are separately positioned on the two sides of the face of solar panels (2), the solar energy
Plate (2) is connect by connection component with main body (3), and the axis of the cylindrical recess (21) is vertical with solar panels (2), the column
Shape recess (21) is arranged in the side of the close solar panels (2) of main body (3), and the friction block (16) is arranged in cylindrical recess
(21) inside of opening, the friction block (16) and the inner wall of cylindrical recess (21) are slidably connected, the friction block (16) with
Solar panels (2) are against the guide rail (18) is vertical with the axis of cylindrical recess (21) and intersects, the both ends of the guide rail (18)
It is fixedly connected with the inner wall of cylindrical recess (21), the inside of the drive block (20) is equipped with through-hole, and the guide rail (18) passes through
Drive block (20), the drive block (20) are slidably connected with guide rail (18), one end and drive block (20) of the drive rod (17)
Hingedly, one end of the separate solar panels (2) of the other end and friction block (16) of the drive rod (17) is hinged, the driving group
Part is arranged in the side of guide rail (18), and the driving component is connect with drive block (20)；
The supporting mechanism includes hinge assembly, slide bar (8), sliding block (7), first connecting rod (4), the second connecting rod (5), third
Connecting rod (6) and two springs (9), the slide bar (8) is vertical with solar panels (2), and the both ends of the slide bar (8) are and main body
(3) be fixedly connected, the inside of the sliding block (7) is equipped with through hole, and the slide bar (8) passes through sliding block (7), the sliding block (7) with
Slide bar (8) is slidably connected, and two springs (9) are set on slide bar (8), the both ends of the slide bar (8) pass through spring (9) with
Sliding block (7) is fixedly connected, and second connecting rod (5) is vertical with slide bar (8), and one end of second connecting rod (5) passes through hinge
Connected components are connect with main body (3), and the third connecting rod (6) is vertical with the second connecting rod (5), and the third connecting rod (6) sets
It sets in the side of the separate slide bar (8) of the second connecting rod (5), the other end of second connecting rod (5) and third connecting rod (6)
One end be fixedly connected, one end of the other end and first connecting rod (4) of second connecting rod (5) is hinged, it is described first connect
The other end of extension bar (4) and sliding block (7) hingedly, the first connecting rod (4), the second connecting rod (5), third connecting rod (6) with
Slide bar (8) is in same plane.
2. as described in claim 1 with the easy to maintain solar energy unmanned plane of pooling feature, which is characterized in that the main body
(3) inside is equipped with wireless signal folding and unfolding module and PLC, and the wireless signal transceiver module is electrically connected with PLC.
3. as described in claim 1 with the easy to maintain solar energy unmanned plane of pooling feature, which is characterized in that the driving
Component includes motor (22) and screw rod (19), and the screw rod (19) is parallel with guide rail (18), and the both ends of the screw rod (19) are all provided with
There is installation bearing, the both ends of the screw rod (19) pass through installation bearing and connect with guide rail (18), and the screw rod (19), which passes through, drives
Motion block (20), the screw rod (19) are threadedly coupled with drive block (20), and the motor (22) is fixedly connected with guide rail (18), described
Motor (22) and screw rod (19) are sequentially connected.
4. as described in claim 1 with the easy to maintain solar energy unmanned plane of pooling feature, which is characterized in that the fixation
Component includes fixed strip (13), connection strap (15) and strip groove (14), and the fixed strip (13) is arranged the one of solar panels (2)
Side, the fixed strip (13) are fixedly connected with main body (3), close solar energy of strip groove (14) setting in fixed strip (13)
The side of plate (2), the connection strap (15) are arranged in the side of the close fixed strip (13) of solar panels (2), the connection strap
(15) it is matched with strip groove (14), inside of connection strap (15) setting in strip groove (14).
5. as claimed in claim 4 with the easy to maintain solar energy unmanned plane of pooling feature, which is characterized in that the bar shaped
The inner wall of the side of the separate main body (3) of slot (14) is equipped with tread plate.
6. as described in claim 1 with the easy to maintain solar energy unmanned plane of pooling feature, which is characterized in that the friction
The making material of block (16) is rubber.
7. as described in claim 1 with the easy to maintain solar energy unmanned plane of pooling feature, which is characterized in that described hinged
Component includes connecting shaft (11), connecting sleeve (10) and two fixed blocks (12), the connecting shaft (11) and first connecting rod (4)
Vertical with the second connecting rod (5), the both ends of the connecting shaft (11) pass through the separate sun of fixed block (12) Yu main body (3)
Can one end of close slide bar (8) of side of plate (2) be fixedly connected, the connecting sleeve (10) with connecting shaft (11) is coaxial sets
It sets, the connecting shaft (11) passes through connecting sleeve (10), the close main body of the connecting sleeve (10) and the second connecting rod (5)
(3) one end is fixedly connected.
8. as described in claim 1 with the easy to maintain solar energy unmanned plane of pooling feature, which is characterized in that the slide bar
(8) lubricating grease is coated on.
9. as described in claim 1 with the easy to maintain solar energy unmanned plane of pooling feature, which is characterized in that the third
One end of the separate main body (3) of connecting rod (6) is equipped with air bag.
10. as described in claim 1 with the easy to maintain solar energy unmanned plane of pooling feature, which is characterized in that the master
Body is coated with corrosion-inhibiting coating on (3).
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| CN110406668B (en) | 2021-09-28 |
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