CN207496933U - It is a kind of that there is the intelligent unmanned machine of emergent charging for rainforest shooting - Google Patents
It is a kind of that there is the intelligent unmanned machine of emergent charging for rainforest shooting Download PDFInfo
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- CN207496933U CN207496933U CN201721223712.5U CN201721223712U CN207496933U CN 207496933 U CN207496933 U CN 207496933U CN 201721223712 U CN201721223712 U CN 201721223712U CN 207496933 U CN207496933 U CN 207496933U
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- unfolding
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Abstract
There is the intelligent unmanned machine of emergent charging for rainforest shooting the utility model is related to a kind of,Including fuselage,Propeller and stent,Fuselage further includes charging mechanism and two fixed mechanisms,Charging mechanism includes the hydraulic turbine and folding and unfolding component,Folding and unfolding component includes the first motor,First bevel gear,Folding and unfolding plate and two retractable units,Fixed mechanism includes the first support plate,Second support plate and fixation kit,Fixation kit includes fixed block,Sliding shoe,Expansion bracket,Hinged block,Folding and unfolding block and cylinder,This has the function of the intelligent unmanned machine of emergent charging for rainforest shooting,When unmanned plane out of power can not normal use when,Make full use of the water resource in rainforest,Unmanned plane is fixed on above flow by fixed mechanism,It is stretched into flow by charging mechanism again,It is generated electricity using the kinetic energy of water,Flight for unmanned plane provides electric energy,Substantially increase the practicability that unmanned plane works in rainforest.
Description
Technical field
The utility model is related to unmanned plane field, more particularly to a kind of emergent charging that has the function of for rainforest shooting
Intelligent unmanned machine.
Background technology
Unmanned plane is the not manned vehicle manipulated by radio robot or airborne computer stored program controlled.
Unmanned plane is simple in structure, use cost is low, can not only complete the task of manned aircraft execution, be more suitable for someone's aircraft not
Preferably performing for task.
At present, unmanned plane is gradually applied in the shooting work to rainforest, because unmanned plane can aloft to rainforest into
Some artificial pictures for being difficult to shoot of rainforest can be presented in face of spectators by row shooting, however photographer is using unmanned plane
During being taken photo by plane, the situation of unmanned plane out of power is often encountered, and at this point, when the electricity of portable mobile power
When being finished, unmanned plane just can not normal use, however existing unmanned plane does not have special emergent charging function, this is with regard to big
Reduce the practicability that unmanned plane works in rainforest greatly.
Utility model content
The technical problems to be solved in the utility model is：It is a kind of for rainforest in order to overcome the deficiencies of the prior art and provide
Shooting has the function of the intelligent unmanned machine of emergent charging.
Technical solution is used by the utility model solves its technical problem：It is a kind of emergent for having for rainforest shooting
The intelligent unmanned machine of charge function, including fuselage, propeller and stent, the fuselage further includes charging mechanism and two fixations
Mechanism, the charging mechanism and two fixed mechanisms are arranged in fuselage, and two fixed mechanisms are respectively positioned at charging mechanism
Both sides, two fixed mechanisms are separately positioned on the both sides of fuselage, and two fixed mechanisms are symmetrical arranged about charging mechanism；
The charging mechanism includes the hydraulic turbine and folding and unfolding component, and the hydraulic turbine is arranged on the lower section of folding and unfolding component, described
The hydraulic turbine is sequentially connected with folding and unfolding component；
The folding and unfolding component includes the first motor, first bevel gear, folding and unfolding plate and two retractable units, first motor
It vertically sets downward, first motor is sequentially connected with first bevel gear, and two retractable units are located at first bevel gear respectively
Both sides, two retractable units are symmetrical arranged about first bevel gear, and the folding and unfolding plate level is arranged on two retractable units
Lower section, two retractable units are symmetrical arranged about folding and unfolding plate；
The retractable unit includes screw, second bevel gear, sliding block and connecting rod, and the screw is horizontally disposed with, the screw
It is connected by the side of bearing and fuselage, the bearing and second bevel gear are separately positioned on the both ends of screw, second cone
Gear is set on screw, and the second bevel gear is engaged with first bevel gear, and the screw passes through sliding block and screw and sliding block
It is threadedly coupled, the top surface level of the fuselage is equipped with sliding slot, and the top of the sliding block is located in sliding slot, the sliding block and sliding slot
Match and be slidably connected, one end and the sliding block of the connecting rod are hinged, and the other end and the folding and unfolding plate of the connecting rod are hinged, the hydraulic turbine
It is arranged on the lower section of folding and unfolding plate, the bottom surface of the fuselage is equipped with the first opening, and the hydraulic turbine is located at the first opening and with the
One opening corresponds to；
The fixed mechanism includes the first support plate, the second support plate and fixation kit, and first support plate is horizontally set on machine
The side of body, second support plate are vertically provided at one end of the separate fuselage of the first support plate, and the fixation kit is arranged on
The side of two support plates, the fixation kit is between the second support plate and the side of fuselage；
The fixation kit include fixed block, sliding shoe, expansion bracket, hinged block, folding and unfolding block and cylinder, the fixed plate and
Sliding shoe is arranged at the side of the second support plate, and the fixed block is fixedly connected with the side of the second support plate, the sliding shoe with
The side of second support plate is slidably connected, and the expansion bracket is horizontally disposed with, the both ends of the side of the expansion bracket respectively with fixed block
It is hinged with sliding shoe, there are two the hinged blocks, and the both ends of the opposite side of the expansion bracket are hinged respectively with two hinged blocks, institute
The side that folding and unfolding block is arranged on the separate expansion bracket of hinged block is stated, two hinged blocks are slidably connected with folding and unfolding block, the cylinder
The vertical side for being arranged on the second support plate downward, the output shaft of the cylinder are fixedly connected with sliding shoe, the folding and unfolding block it is remote
Side level from hinged block is equipped with several first contact pins, and each first contact pin is uniformly arranged on the side of folding and unfolding block, the fuselage
Both sides be equipped with the second opening, two folding and unfolding blocks are located at two the second openings respectively, two folding and unfolding blocks respectively with two the
Two openings correspond to.
Preferably, in order to improve the stability of fuselage, firm organization, the firm organization packet are equipped in the folding and unfolding block
Include the second motor, driving wheel, drive rod, drive block, connecting rod, firm plate and pilot unit, second motor and driving wheel
It being sequentially connected, the drive block is located in pilot unit, and the drive block is slidably connected with pilot unit, and the one of the drive rod
End is hinged with driving wheel, and the other end and the drive block of the drive rod are hinged, and the hinged place of the drive rod and driving wheel is located at
The side in the center of circle of driving wheel, the driving wheel drive drive block to move up and down by drive rod, and the connecting rod is vertically arranged
In the lower section of drive block, the firm plate level is arranged on the lower section of connecting rod, and the lower section of the firm plate is vertically equipped with several
Second contact pin, each second contact pin are uniformly arranged on the lower section of firm plate, and the bottom surface of the folding and unfolding block is open equipped with third, described steady
Solid plate is located at third opening and corresponding with third opening.
Preferably, in order to avoid sundries enters fuselage, hermetyic window is equipped in first opening and the second opening, institute
It states hermetyic window to match with the first opening and the second opening respectively, the hermetyic window is hinged with fuselage.
Preferably, in order to improve the slip precision of drive block and the stability of sliding process, the pilot unit includes
Two guide rods being mutually parallel, the drive block are located between two guide rods, the drive block respectively with two guide rods
It is slidably connected.
Preferably, in order to improve the stability that sliding shoe and hinged block slide, it is all provided on the sliding shoe and hinged block
There is limited block, limiting slot is equipped on second support plate and folding and unfolding block, the limited block is located in limiting slot, the limited block
It matches and is slidably connected with limiting slot.
Preferably, in order to further improve the stability that sliding shoe and hinged block slide, the limiting slot is dovetail groove.
Preferably, in order to make hydraulic turbine quickly retracting, the surface of the screw is equipped with anticorrosion galvanizing layer.
Preferably, in order to extend the service life of the first contact pin and the second contact pin, first contact pin and the second contact pin
Making material be stainless steel.
Preferably, the working condition for Shi Ge mechanisms is intelligent, first motor and the second motor are servo
Motor.
Preferably, in order to make drive block quick sliding, the surface of the drive block and guide rod is equipped with teflon painting
Layer.
The beneficial effects of the utility model are, what this was used for rainforest shooting has the function of the intelligent unmanned of emergent charging
Machine, when unmanned plane out of power can not normal use when, make full use of the water resource in rainforest, consolidated unmanned plane by fixed mechanism
It stretches into flow, is generated electricity using the kinetic energy of water, the flight for unmanned plane provides above flow, then by charging mechanism
Electric energy substantially increases the practicability that unmanned plane works in rainforest.
Description of the drawings
The utility model is further illustrated with reference to the accompanying drawings and examples.
Fig. 1 is a kind of knot with the intelligent unmanned machine of emergent charging for rainforest shooting of the utility model
Structure schematic diagram.
Fig. 2 is that a kind of of the utility model has the function of filling for the intelligent unmanned machine of emergent charging for rainforest shooting
The structure diagram of motor structure.
Fig. 3 is that a kind of of the utility model has the function of consolidating for the intelligent unmanned machine of emergent charging for rainforest shooting
Determine the structure diagram of mechanism.
Fig. 4 is that a kind of of the utility model has the function of the steady of the intelligent unmanned machine of emergent charging for rainforest shooting
Gu the structure diagram of mechanism.
In figure：1. fuselage, 2. propellers, 3. stents, 4. charging mechanisms, 5. fixed mechanisms, 6. hydraulic turbines, 7.
First motor, 8. first bevel gears, 9. folding and unfolding plates, 10. screws, 11. second bevel gears, 12. sliding blocks, 13. connecting rods,
14. the first support plate, 15. second support plates, 16. fixed blocks, 17. sliding shoes, 18. expansion brackets, 19. hinged blocks, 20. receive
Put block, 21. cylinders, 22. first contact pins, 23. second motors, 24. driving wheels, 25. drive rods, 26. drive blocks, 27.
Connecting rod, 28. firm plates, 29. second contact pins, 30. guide rods.
Specific embodiment
The utility model is described in further detail presently in connection with attached drawing.These attached drawings are simplified schematic diagram,
Only illustrate the basic structure of the utility model in a schematic way, therefore it only shows the composition related with the utility model.
As shown in Figs 1-4, it is a kind of that there is the intelligent unmanned machine of emergent charging for rainforest shooting, including fuselage
1st, propeller 2 and stent 3, the fuselage 1 further include charging mechanism 4 and two fixed mechanisms 5, the charging mechanism 4 and two
Fixed mechanism 5 is arranged in fuselage 1, and two fixed mechanisms 5 are located at the both sides of charging mechanism 4 respectively, and two fixed mechanisms 5 divide
It is not arranged on the both sides of fuselage 1, two fixed mechanisms 5 are symmetrical arranged about charging mechanism 4；
When unmanned plane out of power can not normal use when, the water resource in rainforest is made full use of, by fixed mechanism 5 by nothing
It is man-machine to be fixed on above flow, then stretched into flow by charging mechanism 4, it is generated electricity using the kinetic energy of water, is unmanned plane
Flight provides electric energy, substantially increases the practicability that unmanned plane works in rainforest.
The charging mechanism 4 includes the hydraulic turbine 6 and folding and unfolding component, and the hydraulic turbine 6 is arranged on the lower section of folding and unfolding component, institute
The hydraulic turbine 6 is stated to be sequentially connected with folding and unfolding component；
The folding and unfolding component include the first motor 7, first bevel gear 8, folding and unfolding plate 9 and two retractable units, described first
Motor 7 is vertically set downward, and first motor 7 is sequentially connected with first bevel gear 8, and two retractable units are located at first respectively
The both sides of bevel gear 8, two retractable units are symmetrical arranged about first bevel gear 8, and the folding and unfolding plate 9 is horizontally set on two receipts
The lower section of unit is put, two retractable units are symmetrical arranged about folding and unfolding plate 9；
The retractable unit includes screw 10, second bevel gear 11, sliding block 12 and connecting rod 13, and 10 level of screw is set
It puts, the screw 10 is connect by bearing with the side of fuselage 1, and the bearing and second bevel gear 11 are separately positioned on screw 10
Both ends, the second bevel gear 11 is set on screw 10, and the second bevel gear 11 is engaged with first bevel gear 8, described
Screw 10 passes through sliding block 12 and screw 10 is threadedly coupled with sliding block 12, and the top surface level of the fuselage 1 is equipped with sliding slot, the sliding block
12 top is located in sliding slot, and the sliding block 12 is matched and is slidably connected with sliding slot, and one end and the sliding block 12 of the connecting rod 13 are cut with scissors
It connects, the other end of the connecting rod 13 is hinged with folding and unfolding plate 9, and the hydraulic turbine 6 is arranged on the lower section of folding and unfolding plate 9, the fuselage 1
Bottom surface is equipped with the first opening, and the hydraulic turbine 6 is located at the first opening and corresponding with the first opening；
The fixed mechanism 5 includes the first support plate 14, the second support plate 15 and fixation kit, and 14 level of the first support plate is set
It puts in the side of fuselage 1, second support plate 15 is vertically provided at one end of the separate fuselage 1 of the first support plate 14, the fixation
Component is arranged on the side of the second support plate 15, and the fixation kit is between the second support plate 15 and the side of fuselage 1；
The fixation kit includes fixed block 16, sliding shoe 17, expansion bracket 18, hinged block 19, folding and unfolding block 20 and cylinder 21,
The fixed plate and sliding shoe 17 are arranged at the side of the second support plate 15, and the side of the fixed block 16 and the second support plate 15 is consolidated
Fixed connection, the side of the sliding shoe 17 and the second support plate 15 are slidably connected, and the expansion bracket 18 is horizontally disposed, the expansion bracket
The both ends of 18 side are hinged with fixed block 16 and sliding shoe 17 respectively, and there are two the hinged blocks 19, the expansion bracket 18
The both ends of opposite side are hinged with two hinged blocks 19 respectively, and the folding and unfolding block 20 is arranged on the separate expansion bracket 18 of hinged block 19
Side, two hinged blocks 19 are slidably connected with folding and unfolding block 20, and the cylinder 21 is vertically arranged on the one of the second support plate 15 downward
Side, the output shaft of the cylinder 21 are fixedly connected with sliding shoe 17, and the side of the separate hinged block 19 of the folding and unfolding block 20 is horizontal
Equipped with several first contact pins 22, each first contact pin 22 is uniformly arranged on the side of folding and unfolding block 20, and the both sides of the fuselage 1 are equipped with
Second opening, two folding and unfolding blocks 20 respectively be located at two the second openings, two folding and unfolding blocks 20 respectively with two second opening pair
It should.
When unmanned plane out of power can not normal use when, make full use of the water resource in rainforest, first start cylinder 21, gas
Cylinder 21 drives sliding shoe 17 to be slided to fixed block 16 so that and expansion bracket 18 is elongated, and expansion bracket 18 drives folding and unfolding block 20 to move horizontally,
So that the first contact pin 22 moves horizontally, so as to which the first contact pin 22 be made to be inserted into respectively in the soil of flow both sides from the both sides of fuselage 1,
And then unmanned plane is fixed on above flow, restart the first motor 7, the first motor 7 driving first bevel gear 8 rotates, and first
Bevel gear 8 drives two screws 10 to rotate backward by two second bevel gears 11 respectively so that and two sliding blocks 12 move toward one another,
Two sliding blocks 12 drive folding and unfolding plate 9 to move downward by two connecting rods 13 respectively so that and the hydraulic turbine 6 is stretched out from the bottom of fuselage 1,
And stretch into flow, it is generated electricity using the kinetic energy of water, the flight for unmanned plane provides electric energy, substantially increases unmanned plane in rain
The practicability to work in woods.
Preferably, in order to improve the stability of fuselage 1, firm organization, the firm machine are equipped in the folding and unfolding block 20
Structure includes the second motor 23, driving wheel 24, drive rod 25, drive block 26, connecting rod 27, firm plate 28 and pilot unit, described
Second motor 23 is sequentially connected with driving wheel 24, and the drive block 26 is located in pilot unit, and the drive block 26 is single with being oriented to
Member is slidably connected, and one end of the drive rod 25 is hinged with driving wheel 24, and the other end and the drive block 26 of the drive rod 25 are cut with scissors
It connects, the hinged place of the drive rod 25 and driving wheel 24 is located at the side in the center of circle of driving wheel 24, and the driving wheel 24 passes through drive
Lever 25 drives drive block 26 to move up and down, and the connecting rod 27 is vertically provided at the lower section of drive block 26, the firm plate 28
The lower section of connecting rod 27 is horizontally set on, the lower section of the firm plate 28 is vertically equipped with several second contact pins 29, each second contact pin
29 are uniformly arranged on the lower section of firm plate 28, and the bottom surface of the folding and unfolding block 20 is open equipped with third, and the firm plate 28 is located at the
Three openings and corresponding with third opening, the second motor 23 driving driving wheel 24 rotate, and driving wheel 24 is driven by drive rod 25
Drive block 26 moves up and down so that connecting rod 27 drives the second contact pin 29 to be inserted into soil by firm plate 28, so as to improve fuselage 1
Stability.
Preferably, in order to avoid sundries enters fuselage 1, hermetyic window is equipped in first opening and the second opening,
The hermetyic window is open respectively with first and the second opening matches, and the hermetyic window is hinged with fuselage 1, when charging mechanism 4 and admittedly
When determining mechanism 5 and being accommodated in fuselage 1, the first opening and the second opening can keep sealing state, and sundries is avoided to enter fuselage 1, when
When charging mechanism 4 and fixed mechanism 5 work, it can be stretched out through the first opening and the second opening.
Preferably, in order to improve the slip precision of drive block 26 and the stability of sliding process, the pilot unit packet
Include two guide rods being mutually parallel 30, the drive block 26 is located between two guide rods 30, the drive block 26 respectively with
Two guide rods 30 are slidably connected, because the sliding trace of drive block 26 is limited to a certain range by the guide rod 30 being mutually parallel
It is interior, therefore realize the accuracy and stability of its sliding process.
Preferably, in order to improve the stability that sliding shoe 17 and hinged block 19 slide, the sliding shoe 17 and hinged block
Limited block is equipped on 19, limiting slot is equipped on second support plate 15 and folding and unfolding block 20, the limited block is located at limiting slot
Interior, the limited block is matched and is slidably connected with limiting slot, and limiting slot limits the movement locus of limited block in a certain range,
So as to improve the stability that sliding shoe 17 and hinged block 19 slide.
Preferably, in order to further improve the stability that sliding shoe 17 and hinged block 19 slide, the limiting slot is swallow
Stern notch.
Preferably, in order to make 6 quickly retracting of the hydraulic turbine, the surface of the screw 10 is equipped with anticorrosion galvanizing layer, due to zinc
The product of corrosion has zinc preferable protective effect, so corrosion rate is very slow, the service life is ungalvanized l5~30 times, therefore energy
Screw 10 is prevented to be corroded, avoids influencing the movement speed of sliding block 12, so as to make 6 quickly retracting of the hydraulic turbine.
Preferably, in order to extend the service life of the first contact pin 22 and the second contact pin 29, first contact pin 22 and
The making material of two contact pins 29 is stainless steel, and due to soil moisture in rainforest, and the first contact pin 22 and the second contact pin 29 need
Soil is inserted into, and stainless steel is not easy to be corroded, therefore the service life of the first contact pin 22 and the second contact pin 29 can be extended.
Preferably, the working condition for Shi Ge mechanisms is intelligent, 7 and second motor 23 of the first motor is to watch
Take motor.
Preferably, in order to make 26 quick sliding of drive block, the surface of the drive block 26 and guide rod 30 is equipped with spy
Fluon coating, since teflon coating has relatively low friction coefficient, lubricity, particularly self lubricity are very good, to it
He hardly adheres to substance, therefore can reduce the frictional force between drive block 26 and guide rod 30, so as to make 26 quick sliding of drive block.
Compared with prior art, this be used for rainforest shooting there is the intelligent unmanned machine of emergent charging, when nobody
Machine out of power can not normal use when, make full use of the water resource in rainforest, unmanned plane be fixed on by flow by fixed mechanism 5
Top, then stretched into flow by charging mechanism 4, it is generated electricity using the kinetic energy of water, the flight for unmanned plane provides electric energy, greatly
Improve the practicability that unmanned plane works in rainforest greatly.
Using the above-mentioned desirable embodiment according to the utility model as enlightenment, pass through above-mentioned description, related work people
Member can carry out various changes and amendments in the range of without departing from this item utility model technological thought completely.This item is real
The content being not limited to novel technical scope on specification, it is necessary to which its technology is determined according to right
Property range.
Claims (10)
1. a kind of have the function of the intelligent unmanned machine of emergent charging for rainforest shooting, which is characterized in that including fuselage, spiral shell
Rotation paddle and stent, the fuselage further include charging mechanism and two fixed mechanisms, and the charging mechanism and two fixed mechanisms are equal
It is arranged in fuselage, two fixed mechanisms are located at the both sides of charging mechanism respectively, and two fixed mechanisms are separately positioned on fuselage
Both sides, two fixed mechanisms are symmetrical arranged about charging mechanism；
The charging mechanism includes the hydraulic turbine and folding and unfolding component, and the hydraulic turbine is arranged on the lower section of folding and unfolding component, the water wheels
Machine is sequentially connected with folding and unfolding component；
The folding and unfolding component includes the first motor, first bevel gear, folding and unfolding plate and two retractable units, and first motor is vertical
It sets downward, first motor is sequentially connected with first bevel gear, and two retractable units are located at the two of first bevel gear respectively
Side, two retractable units are symmetrical arranged about first bevel gear, and the folding and unfolding plate level is arranged on the lower section of two retractable units,
Two retractable units are symmetrical arranged about folding and unfolding plate；
The retractable unit includes screw, second bevel gear, sliding block and connecting rod, and the screw is horizontally disposed with, and the screw passes through
The connection of the side of bearing and fuselage, the bearing and second bevel gear are separately positioned on the both ends of screw, the second bevel gear
It is set on screw, the second bevel gear is engaged with first bevel gear, and the screw passes through sliding block and screw and sliding block screw thread
Connection, the top surface level of the fuselage are equipped with sliding slot, and the top of the sliding block is located in sliding slot, the sliding block matched with sliding slot and
It is slidably connected, one end and the sliding block of the connecting rod are hinged, and the other end and the folding and unfolding plate of the connecting rod are hinged, the hydraulic turbine setting
In the lower section of folding and unfolding plate, the bottom surface of the fuselage is equipped with the first opening, and the hydraulic turbine is located at the first opening and is opened with first
Mouth is corresponding；
The fixed mechanism includes the first support plate, the second support plate and fixation kit, and first support plate is horizontally set on fuselage
Side, second support plate are vertically provided at one end of the separate fuselage of the first support plate, and the fixation kit is arranged on second
The side of plate, the fixation kit is between the second support plate and the side of fuselage；
The fixation kit includes fixed block, sliding shoe, expansion bracket, hinged block, folding and unfolding block and cylinder, the fixed plate and slip
Block is arranged at the side of the second support plate, and the fixed block is fixedly connected with the side of the second support plate, the sliding shoe and second
The side of support plate is slidably connected, and the expansion bracket is horizontally disposed with, the both ends of the side of the expansion bracket respectively with fixed block and cunning
Motion block is hinged, and there are two the hinged blocks, and the both ends of the opposite side of the expansion bracket are hinged respectively with two hinged blocks, the receipts
The side that block is arranged on the separate expansion bracket of hinged block is put, two hinged blocks are slidably connected with folding and unfolding block, and the cylinder is vertical
It is arranged on the side of the second support plate downward, the output shaft of the cylinder is fixedly connected with sliding shoe, the separate hinge of the folding and unfolding block
The side level for connecing block is equipped with several first contact pins, and each first contact pin is uniformly arranged on the side of folding and unfolding block, and the two of the fuselage
Side is equipped with the second opening, and two folding and unfolding blocks are located at two the second openings respectively, and two folding and unfolding blocks are opened respectively with two second
Mouth is corresponding.
2. having the function of the intelligent unmanned machine of emergent charging as described in claim 1 for rainforest shooting, feature exists
In the folding and unfolding block is interior to be equipped with firm organization, and the firm organization includes the second motor, driving wheel, drive rod, drive block, company
Extension bar, firm plate and pilot unit, second motor are sequentially connected with driving wheel, and the drive block is located in pilot unit,
The drive block is slidably connected with pilot unit, and one end and the driving wheel of the drive rod are hinged, the other end of the drive rod
It is hinged with drive block, the hinged place of the drive rod and driving wheel is located at the side in the center of circle of driving wheel, and the driving wheel passes through
Drive rod driving drive block moves up and down, and the connecting rod is vertically provided at the lower section of drive block, the firm plate level setting
In the lower section of connecting rod, the lower section of the firm plate is vertically equipped with several second contact pins, and each second contact pin is uniformly arranged on firm
The lower section of plate, the bottom surface of the folding and unfolding block are open equipped with third, and the firm plate is located at third opening and is open pair with third
It should.
3. having the function of the intelligent unmanned machine of emergent charging as described in claim 1 for rainforest shooting, feature exists
In described first is open and hermetyic window is equipped in the second opening, and the hermetyic window is open respectively with first and the second opening
Match, the hermetyic window is hinged with fuselage.
4. having the function of the intelligent unmanned machine of emergent charging as claimed in claim 2 for rainforest shooting, feature exists
In the pilot unit includes two guide rods being mutually parallel, and the drive block is located between two guide rods, the driving
Block is slidably connected respectively with two guide rods.
5. having the function of the intelligent unmanned machine of emergent charging as described in claim 1 for rainforest shooting, feature exists
In being equipped with limited block on the sliding shoe and hinged block, limiting slot, the limit be equipped on second support plate and folding and unfolding block
Position block is located in limiting slot, and the limited block is matched and is slidably connected with limiting slot.
6. having the function of the intelligent unmanned machine of emergent charging as claimed in claim 5 for rainforest shooting, feature exists
In the limiting slot is dovetail groove.
7. having the function of the intelligent unmanned machine of emergent charging as described in claim 1 for rainforest shooting, feature exists
In the surface of the screw is equipped with anticorrosion galvanizing layer.
8. having the function of the intelligent unmanned machine of emergent charging as claimed in claim 2 for rainforest shooting, feature exists
In the making material of first contact pin and the second contact pin is stainless steel.
9. having the function of the intelligent unmanned machine of emergent charging as claimed in claim 2 for rainforest shooting, feature exists
In first motor and the second motor are servo motor.
10. having the function of the intelligent unmanned machine of emergent charging as claimed in claim 4 for rainforest shooting, feature exists
In the surface of the drive block and guide rod is equipped with teflon coating.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721223712.5U CN207496933U (en) | 2017-09-22 | 2017-09-22 | It is a kind of that there is the intelligent unmanned machine of emergent charging for rainforest shooting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721223712.5U CN207496933U (en) | 2017-09-22 | 2017-09-22 | It is a kind of that there is the intelligent unmanned machine of emergent charging for rainforest shooting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207496933U true CN207496933U (en) | 2018-06-15 |
Family
ID=62498497
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721223712.5U Expired - Fee Related CN207496933U (en) | 2017-09-22 | 2017-09-22 | It is a kind of that there is the intelligent unmanned machine of emergent charging for rainforest shooting |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207496933U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109906796A (en) * | 2019-03-13 | 2019-06-21 | 河南科技学院 | A kind of crop topping machine based on plant protection drone |
| CN111232205A (en) * | 2020-03-18 | 2020-06-05 | 浦江光特通讯技术有限公司 | Aircraft is received with communication signal in field |
-
2017
- 2017-09-22 CN CN201721223712.5U patent/CN207496933U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109906796A (en) * | 2019-03-13 | 2019-06-21 | 河南科技学院 | A kind of crop topping machine based on plant protection drone |
| CN111232205A (en) * | 2020-03-18 | 2020-06-05 | 浦江光特通讯技术有限公司 | Aircraft is received with communication signal in field |
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