CN109533326A - A kind of intelligent unmanned machine with emergent charging function for rainforest shooting - Google Patents
A kind of intelligent unmanned machine with emergent charging function for rainforest shooting Download PDFInfo
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- CN109533326A CN109533326A CN201710866287.XA CN201710866287A CN109533326A CN 109533326 A CN109533326 A CN 109533326A CN 201710866287 A CN201710866287 A CN 201710866287A CN 109533326 A CN109533326 A CN 109533326A
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- unfolding
- rainforest
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- 230000007246 mechanism Effects 0.000 claims abstract description 52
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 23
- 230000008520 organization Effects 0.000 claims description 5
- 230000033001 locomotion Effects 0.000 claims description 4
- 229910001220 stainless steel Inorganic materials 0.000 claims description 4
- 239000010935 stainless steel Substances 0.000 claims description 4
- 239000004809 Teflon Substances 0.000 claims description 3
- 229920006362 Teflon® Polymers 0.000 claims description 3
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- 238000005246 galvanizing Methods 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- 230000005611 electricity Effects 0.000 abstract description 7
- 238000010586 diagram Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 239000002689 soil Substances 0.000 description 4
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 239000010410 layer Substances 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- 229920006358 Fluon Polymers 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000012791 sliding layer Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
The present invention relates to a kind of intelligent unmanned machines with emergent charging function for rainforest shooting, including fuselage, propeller and bracket, 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 first motor, first bevel gear, folding and unfolding plate and two retractable units, fixed mechanism includes the first supporting plate, second supporting plate and fixation kit, fixation kit includes fixed block, sliding shoe, expansion bracket, hinged block, folding and unfolding block and cylinder, this is used for the intelligent unmanned machine with emergent charging function of rainforest shooting, when unmanned plane it is out of power can not normal use when, make full use of the water resource in rainforest, unmanned plane is fixed on above water flow by fixed mechanism, it is protruded into water flow by charging mechanism again, it is generated electricity using the kinetic energy of water, electric energy is provided for the flight of unmanned plane , substantially increase the practicability that unmanned plane works in rainforest.
Description
Technical field
The present invention relates to unmanned plane field, in particular to a kind of intelligence with emergent charging function for rainforest shooting
Type unmanned plane.
Background technique
Unmanned plane is the not manned vehicle manipulated by radio robot or airborne computer stored program controlled.
Unmanned plane structure is simple, use cost is low, can not only complete the task of manned aircraft execution, be more suitable for someone's aircraft not
Preferably executing for task.
Currently, unmanned plane is gradually applied in the shooting work to rainforest, because unmanned plane can aloft to rainforest into
Some pictures for manually 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, unmanned plane situation out of power is often encountered, and at this point, working as the electricity of portable mobile power source
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
The practicability that unmanned plane works in rainforest is reduced greatly.
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 for rainforest shooting
The intelligent unmanned machine with emergent charging function.
The technical solution adopted by the present invention to solve the technical problems is: a kind of to have emergent charging for rainforest shooting
The intelligent unmanned machine of function, including fuselage, propeller and bracket, the fuselage further include charging mechanism and two fixed machines
Structure, the charging mechanism and two fixed mechanisms are arranged in fuselage, and two fixed mechanisms are located at the two of charging mechanism
Side, two fixed mechanisms are separately positioned on the two 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 lower section of folding and unfolding component, the water wheels are arranged in the hydraulic turbine
Machine and folding and unfolding component are sequentially connected；
The folding and unfolding component includes that first motor, first bevel gear, folding and unfolding plate and two retractable units, the first motor are vertical
It is arranged downward, the first motor and first bevel gear are sequentially connected, and two retractable units are located at the two of first bevel gear
Side, two retractable units are symmetrical arranged about first bevel gear, and the folding and unfolding plate is horizontally set on the lower section of two retractable units,
Two retractable units are symmetrical arranged about folding and unfolding plate；
The retractable unit includes screw rod, second bevel gear, sliding block and connecting rod, and the screw rod is horizontally disposed, and the screw rod 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 rod, the second bevel gear
It is set on screw rod, the second bevel gear is engaged with first bevel gear, and the screw rod is across sliding block and screw rod 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 of the connecting rod and sliding block are hinged, and the other end and 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 opens with first
Mouth is corresponding；
The fixed mechanism includes the first supporting plate, the second supporting plate and fixation kit, and first supporting plate is horizontally set on fuselage
Side, second supporting plate are vertically provided at one end of the separate fuselage of the first supporting plate, and the fixation kit is arranged at second
The side of plate, the fixation kit is between the second supporting 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 sliding
Block is arranged at the side of the second supporting plate, and the fixed block is fixedly connected with the side of the second supporting plate, the sliding shoe and second
The side of supporting plate is slidably connected, and the expansion bracket is horizontally disposed, 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 other side of the expansion bracket are hinged with two hinged blocks respectively, the receipts
The side that the separate expansion bracket of hinged block is arranged in block is put, two hinged blocks are slidably connected with folding and unfolding block, and the cylinder is vertical
The side of second supporting plate is set downward, and 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, and two folding and unfolding blocks are opened with two second respectively
Mouth is corresponding.
Preferably, being equipped with firm organization, the firm organization packet in the folding and unfolding block to improve the stability of fuselage
Include the second motor, driving wheel, drive rod, drive block, connecting rod, firm plate and pilot unit, second motor and driving wheel
Transmission connection, the drive block are 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 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 is horizontally set 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, being equipped with hermetyic window, institute in the first opening and the second opening in order to avoid sundries enters fuselage
It states hermetyic window to match with the first opening and the second opening respectively, the hermetyic window and fuselage are hinged.
Preferably, in order to improve the sliding precision of drive block and the stability of sliding process, the pilot unit includes
Two guide rods being parallel to each other, the drive block are located between two guide rods, the drive block respectively with two guide rods
It is slidably connected.
Preferably, being all provided on the sliding shoe and hinged block to improve the stability of sliding shoe and hinged block sliding
There is limited block, limiting slot is equipped on second supporting 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 increase the stability of sliding shoe and hinged block sliding, the limiting slot is dovetail groove.
Preferably, in order to make hydraulic turbine quickly retracting, the surface of the screw rod 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 mechanism is intelligent, the first motor and the second motor are servo
Motor.
Preferably, the surface of the drive block and guide rod is equipped with teflon painting in order to make drive block quick sliding
Layer.
The invention has the advantages that this is used for the intelligent unmanned machine with emergent charging function of rainforest shooting, when
Unmanned plane it is out of power can not normal use when, make full use of the water resource in rainforest, be fixed on unmanned plane by fixed mechanism
It above water flow, then is protruded into water flow by charging mechanism, is generated electricity using the kinetic energy of water, provide electricity for the flight of unmanned plane
Can, substantially increase the practicability that unmanned plane works in rainforest.
Detailed description of the invention
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is that a kind of structure of intelligent unmanned machine with emergent charging function for rainforest shooting of the invention is shown
It is intended to.
Fig. 2 is a kind of charger of intelligent unmanned machine with emergent charging function for rainforest shooting of the invention
The structural schematic diagram of structure.
Fig. 3 is a kind of fixation machine of intelligent unmanned machine with emergent charging function for rainforest shooting of the invention
The structural schematic diagram of structure.
Fig. 4 is a kind of firm machine of intelligent unmanned machine with emergent charging function for rainforest shooting of the invention
The structural schematic diagram of structure.
In figure: 1. fuselages, 2. propellers, 3. brackets, 4. charging mechanisms, 5. fixed mechanisms, 6. hydraulic turbines, 7.
First motor, 8. first bevel gears, 9. folding and unfolding plates, 10. screw rods, 11. second bevel gears, 12. sliding blocks, 13. connecting rods,
14. the first supporting plate, 15. second supporting 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
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 Figs 1-4, a kind of intelligent unmanned machine with emergent charging function for rainforest shooting, including fuselage
1, propeller 2 and bracket 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 two sides of charging mechanism 4, and two fixed mechanisms 5 divide
The two sides of fuselage 1 are not set, and two fixed mechanisms 5 are symmetrical arranged about charging mechanism 4；
When unmanned plane it is out of power can not normal use when, the water resource in rainforest is made full use of, by fixed mechanism 5 by unmanned plane
It is fixed on above water flow, then is protruded into water flow by charging mechanism 4, generated electricity using the kinetic energy of water, be the flight of unmanned plane
Electric energy is provided, the practicability that unmanned plane works in rainforest is substantially increased.
The charging mechanism 4 includes the hydraulic turbine 6 and folding and unfolding component, and the lower section of folding and unfolding component, institute is arranged in the hydraulic turbine 6
It states the hydraulic turbine 6 and folding and unfolding component is sequentially connected；
The folding and unfolding component includes first motor 7, first bevel gear 8, folding and unfolding plate 9 and two retractable units, the first motor 7
Vertically it is arranged downward, the first motor 7 is sequentially connected with first bevel gear 8, and two retractable units are located at the first cone tooth
The two sides of wheel 8, two retractable units are symmetrical arranged about first bevel gear 8, and the folding and unfolding plate 9 is horizontally set on two folding and unfolding lists
The lower section of member, two retractable units are symmetrical arranged about folding and unfolding plate 9；
The retractable unit includes screw rod 10, second bevel gear 11, sliding block 12 and connecting rod 13, and the screw rod 10 is horizontally disposed, institute
It states screw rod 10 to connect by bearing with the side of fuselage 1, the bearing and second bevel gear 11 are separately positioned on the two of screw rod 10
End, the second bevel gear 11 are set on screw rod 10, and the second bevel gear 11 is engaged with first bevel gear 8, the screw rod
10 across sliding block 12 and screw rod 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 of the connecting rod 13 and sliding block 12 are hinged, institute
The other end and the folding and unfolding plate 9 for stating connecting rod 13 are hinged, and the lower section of folding and unfolding plate 9, the bottom surface of the fuselage 1 is arranged in the hydraulic turbine 6
Equipped with the first opening, the hydraulic turbine 6 is located at the first opening and corresponding with the first opening；
The fixed mechanism 5 includes the first supporting plate 14, the second supporting plate 15 and fixation kit, and first supporting plate 14 is horizontally set on
The side of fuselage 1, second supporting plate 15 are vertically provided at one end of the separate fuselage 1 of the first supporting plate 14, the fixation kit
The side of second supporting plate 15 is set, and the fixation kit is between the second supporting 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, described
Fixed plate and sliding shoe 17 are arranged at the side of the second supporting plate 15, the fixed company in the side of the fixed block 16 and the second supporting plate 15
It connects, the side of the sliding shoe 17 and the second supporting plate 15 is slidably connected, and the expansion bracket 18 is horizontally disposed, the expansion bracket 18
The both ends of side are hinged with fixed block 16 and sliding shoe 17 respectively, and there are two the hinged blocks 19, the expansion bracket 18 it is another
The both ends of side are hinged with two hinged blocks 19 respectively, and the one of the separate expansion bracket 18 of hinged block 19 is arranged in the folding and unfolding block 20
Side, two hinged blocks 19 are slidably connected with folding and unfolding block 20, and the side of the second supporting plate 15 is vertically arranged in the cylinder 21 downward,
The output shaft of the cylinder 21 is fixedly connected with sliding shoe 17, and the side level of the separate hinged block 19 of the folding and unfolding block 20 is equipped with
Several first contact pins 22, each first contact pin 22 are uniformly arranged on the side of folding and unfolding block 20, and the two sides of the fuselage 1 are equipped with second
Opening, two folding and unfolding blocks 20 are located at two the second openings, and two folding and unfolding blocks 20 are corresponding with two second openings respectively.
When unmanned plane it is out of power can not normal use when, make full use of the water resource in rainforest, first starting cylinder 21, gas
Cylinder 21 drives sliding shoe 17 to slide to fixed block 16, so that expansion bracket 18 is elongated, expansion bracket 18 drives folding and unfolding block 20 to move horizontally,
So that the first contact pin 22 moves horizontally, thus make the first contact pin 22 from the soil that water flow two sides are inserted into the two sides of fuselage 1 respectively,
And then unmanned plane is fixed on above water flow, restart first motor 7, first motor 7 drives first bevel gear 8 to rotate, and first
Bevel gear 8 drives two screw rods 10 to rotate backward by two second bevel gears 11 respectively, so that 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 the hydraulic turbine 6 is stretched out from the bottom of fuselage 1,
And protrude into water flow, it is generated electricity using the kinetic energy of water, provides electric energy for the flight of unmanned plane, substantially increase unmanned plane in rain
The practicability to work in woods.
Preferably, being equipped with firm organization, the firm machine in the folding and unfolding block 20 to improve the stability of fuselage 1
Structure includes the second motor 23, driving wheel 24, drive rod 25, drive block 26, connecting rod 27, consolidates 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 and guiding are single
Member is slidably connected, and one end of the drive rod 25 and driving wheel 24 are hinged, and the other end and 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
It is horizontally set on the lower section of connecting rod 27, 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 drive driving wheel 24 to 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, to improve fuselage 1
Stability.
Preferably, it is equipped with hermetyic window in the first opening and the second opening in order to avoid sundries enters fuselage 1,
The hermetyic window is matched with the first opening and the second opening respectively, and the hermetyic window and fuselage 1 are hinged, 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 sliding precision of drive block 26 and the stability of sliding process, the pilot unit packet
Include two guide rods being parallel to each other 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 parallel to each other
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
It is equipped with limited block on 19, limiting slot is equipped on second supporting 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 motion profile of limited block in a certain range,
To improve the stability that sliding shoe 17 and hinged block 19 slide.
Preferably, in order to further increase the stability that sliding shoe 17 and hinged block 19 slide, the limiting slot is swallow
Stern notch.
Preferably, the surface of the screw rod 10 is equipped with anticorrosion galvanizing layer, due to zinc in order to make 6 quickly retracting of the hydraulic turbine
The product of corrosion has preferable protective effect to zinc, so corrosion rate is very slow, the service life is ungalvanized l5~30 times, therefore energy
It prevents screw rod 10 to be corroded, the movement speed for influencing sliding block 12 is avoided, 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
It is inserted into soil, 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 mechanism is intelligent, the first motor 7 and the second motor 23 are to watch
Take motor.
Preferably, the surface of the drive block 26 and guide rod 30 is equipped with spy in order to make 26 quick sliding of drive block
Fluon coating, since teflon coating has lower coefficient of friction, lubricity, especially self-lubrication are very good, to it
He hardly adheres to substance, therefore can reduce the frictional force between drive block 26 and guide rod 30, to make 26 quick sliding of drive block.
Compared with prior art, intelligent unmanned machine with emergent charging function for being used for rainforest shooting, when nobody
Machine it is out of power can not normal use when, make full use of the water resource in rainforest, unmanned plane be fixed on by water flow by fixed mechanism 5
Top, then protruded into water flow by charging mechanism 4, it is generated electricity using the kinetic energy of water, provides electric energy for the flight of unmanned plane, greatly
The practicability that unmanned plane works in rainforest is improved greatly.
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 intelligent unmanned machine with emergent charging function for rainforest shooting, which is characterized in that including fuselage, spiral shell
It revolves paddle and bracket, the fuselage further includes charging mechanism and two fixed mechanisms, the charging mechanism and two fixed mechanisms are equal
It is arranged in fuselage, two fixed mechanisms are located at the two sides of charging mechanism, and two fixed mechanisms are separately positioned on fuselage
Two sides, two fixed mechanisms are symmetrical arranged about charging mechanism；
The charging mechanism includes the hydraulic turbine and folding and unfolding component, and the lower section of folding and unfolding component, the water wheels are arranged in the hydraulic turbine
Machine and folding and unfolding component are sequentially connected；
The folding and unfolding component includes that first motor, first bevel gear, folding and unfolding plate and two retractable units, the first motor are vertical
It is arranged downward, the first motor and first bevel gear are sequentially connected, and two retractable units are located at the two of first bevel gear
Side, two retractable units are symmetrical arranged about first bevel gear, and the folding and unfolding plate is horizontally set on the lower section of two retractable units,
Two retractable units are symmetrical arranged about folding and unfolding plate；
The retractable unit includes screw rod, second bevel gear, sliding block and connecting rod, and the screw rod is horizontally disposed, and the screw rod 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 rod, the second bevel gear
It is set on screw rod, the second bevel gear is engaged with first bevel gear, and the screw rod is across sliding block and screw rod 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 of the connecting rod and sliding block are hinged, and the other end and 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 opens with first
Mouth is corresponding；
The fixed mechanism includes the first supporting plate, the second supporting plate and fixation kit, and first supporting plate is horizontally set on fuselage
Side, second supporting plate are vertically provided at one end of the separate fuselage of the first supporting plate, and the fixation kit is arranged at second
The side of plate, the fixation kit is between the second supporting 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 sliding
Block is arranged at the side of the second supporting plate, and the fixed block is fixedly connected with the side of the second supporting plate, the sliding shoe and second
The side of supporting plate is slidably connected, and the expansion bracket is horizontally disposed, 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 other side of the expansion bracket are hinged with two hinged blocks respectively, the receipts
The side that the separate expansion bracket of hinged block is arranged in block is put, two hinged blocks are slidably connected with folding and unfolding block, and the cylinder is vertical
The side of second supporting plate is set downward, and 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, and two folding and unfolding blocks are opened with two second respectively
Mouth is corresponding.
2. the intelligent unmanned machine with emergent charging function for rainforest shooting, feature exist as described in claim 1
In equipped with firm organization in the folding and unfolding block, the firm organization includes the second motor, driving wheel, drive rod, drive block, company
Extension bar, firm plate and pilot unit, second motor and driving wheel are sequentially connected, and the drive block is located in pilot unit,
The drive block is slidably connected with pilot unit, and one end of the drive rod and driving wheel are hinged, the other end of the drive rod
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, and the firm plate is horizontally disposed
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 answers.
3. the intelligent unmanned machine with emergent charging function for rainforest shooting, feature exist as described in claim 1
In, be equipped with hermetyic window in the first opening and the second opening, the hermetyic window respectively with the first opening and the second opening
Match, the hermetyic window and fuselage are hinged.
4. the intelligent unmanned machine with emergent charging function for rainforest shooting, feature exist as claimed in claim 2
In the pilot unit includes two guide rods being parallel to each other, and the drive block is located between two guide rods, the driving
Block is slidably connected with two guide rods respectively.
5. the intelligent unmanned machine with emergent charging function for rainforest shooting, feature exist as described in claim 1
In being equipped with limited block on the sliding shoe and hinged block, limiting slot, the limit be equipped on second supporting 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. the intelligent unmanned machine with emergent charging function for rainforest shooting, feature exist as claimed in claim 5
In the limiting slot is dovetail groove.
7. the intelligent unmanned machine with emergent charging function for rainforest shooting, feature exist as described in claim 1
In the surface of the screw rod is equipped with anticorrosion galvanizing layer.
8. the intelligent unmanned machine with emergent charging function for rainforest shooting, feature exist as claimed in claim 2
In the making material of first contact pin and the second contact pin is stainless steel.
9. the intelligent unmanned machine with emergent charging function for rainforest shooting, feature exist as claimed in claim 2
In the first motor and the second motor are servo motor.
10. the intelligent unmanned machine with emergent charging function for rainforest shooting, feature exist as claimed in claim 4
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 |
|---|---|---|---|
| CN201710866287.XA CN109533326A (en) | 2017-09-22 | 2017-09-22 | A kind of intelligent unmanned machine with emergent charging function for rainforest shooting |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201710866287.XA CN109533326A (en) | 2017-09-22 | 2017-09-22 | A kind of intelligent unmanned machine with emergent charging function for rainforest shooting |
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| Publication Number | Publication Date |
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| CN109533326A true CN109533326A (en) | 2019-03-29 |
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| CN201710866287.XA Pending CN109533326A (en) | 2017-09-22 | 2017-09-22 | A kind of intelligent unmanned machine with emergent charging function for rainforest shooting |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114148532A (en) * | 2021-12-06 | 2022-03-08 | 四川省建筑科学研究院有限公司 | Mounting bracket for monitoring devices based on unmanned aerial vehicle |
| CN116902244A (en) * | 2023-09-08 | 2023-10-20 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle airborne investigation nacelle |
-
2017
- 2017-09-22 CN CN201710866287.XA patent/CN109533326A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114148532A (en) * | 2021-12-06 | 2022-03-08 | 四川省建筑科学研究院有限公司 | Mounting bracket for monitoring devices based on unmanned aerial vehicle |
| CN114148532B (en) * | 2021-12-06 | 2024-04-26 | 四川省建筑科学研究院有限公司 | Monitoring device mounting frame based on unmanned aerial vehicle |
| CN116902244A (en) * | 2023-09-08 | 2023-10-20 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle airborne investigation nacelle |
| CN116902244B (en) * | 2023-09-08 | 2023-12-01 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle airborne investigation nacelle |
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Application publication date: 20190329 |