CN108341063A - A kind of anti-tampering unmanned plane - Google Patents
A kind of anti-tampering unmanned plane Download PDFInfo
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- CN108341063A CN108341063A CN201810147472.8A CN201810147472A CN108341063A CN 108341063 A CN108341063 A CN 108341063A CN 201810147472 A CN201810147472 A CN 201810147472A CN 108341063 A CN108341063 A CN 108341063A
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- 238000009434 installation Methods 0.000 claims abstract description 89
- 238000000926 separation method Methods 0.000 claims abstract description 37
- 230000005540 biological transmission Effects 0.000 claims description 60
- 229910003460 diamond Inorganic materials 0.000 claims description 22
- 239000010432 diamond Substances 0.000 claims description 22
- 238000006243 chemical reaction Methods 0.000 claims description 16
- 238000003825 pressing Methods 0.000 claims description 6
- 230000000694 effects Effects 0.000 claims description 3
- 230000008450 motivation Effects 0.000 claims 2
- 230000010354 integration Effects 0.000 claims 1
- 230000005611 electricity Effects 0.000 abstract description 5
- 230000007613 environmental effect Effects 0.000 abstract description 3
- 239000007788 liquid Substances 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 238000005096 rolling process Methods 0.000 description 3
- 238000012271 agricultural production Methods 0.000 description 2
- 239000003814 drug Substances 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 230000003321 amplification Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000003199 nucleic acid amplification method Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
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- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
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- 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
- H02S20/30—Supporting structures being movable or adjustable, e.g. for angle adjustment
-
- 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
-
- 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
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention discloses a kind of anti-tampering unmanned planes, its structure includes fuselage, separation for electric installation, engine base, wing, paddle, supporting rack, shower plate, medicine-chest, holder, camera, fuselage is connected with engine base and is set to top, separation is set to fuselage interior for electric installation and is electrically connected, engine base is that round connects fuselage in lower section, wing is equally spaced and is welded in base outer and is flexibly connected with paddle, and paddle is installed in wing top and is electrically connected with fuselage.The present invention can be by raising battery at a distance from controller, it is that electric energy is continuously battery powered that solar panel at the top of while avoidable controller is influenced by battery and put outside battery, which can absorb converting heat, sufficient electricity is provided for unmanned plane navigation, boosts environmental awareness and takes full advantage of natural resources.
Description
Technical field
The present invention is a kind of anti-tampering unmanned plane, belongs to anti-tampering unmanned plane field.
Background technology
Unmanned plane is the not manned aircraft manipulated using radio robot and the controller provided for oneself, to realize sprinkling
Operation can spray medicament, seed, pulvis etc..With land transformation, farm land production scale, to improve agricultural production
Efficiency is reduced agricultural production, the demand of generalization is had become using unmanned plane plant protection.Existing unmanned plane is generally comprised equipped with liquid
The liquid reserve tank of body and the jet pipe being connect with liquid reserve tank.When unmanned plane flight on farmland, the liquid in liquid reserve tank passes through jet pipe
It is sprayed onto on the crop in farmland, realizes plant protection.
Existing technology normal controller and battery are closely located, since magnetic field problem controller is easy the shadow by battery
Pilot causes control failure, it has not been convenient to use and operate.
Invention content
In view of the deficienciess of the prior art, it is an object of the present invention to provide a kind of anti-tampering unmanned plane, to solve general control
Device and battery processed are closely located, since magnetic field problem controller is easy to be influenced to cause to control failure by battery, it has not been convenient to make
The problem of with operation.
To achieve the goals above, the present invention is to realize by the following technical solutions：A kind of anti-tampering unmanned plane,
Structure includes fuselage, detaches for electric installation, engine base, wing, paddle, supporting rack, shower plate, medicine-chest, holder, camera, described
Fuselage is connected with engine base and is set to top, and the separation is set to fuselage interior for electric installation and is electrically connected, and the engine base is circle
Shape connects fuselage in lower section, and the wing is equally spaced and is welded in base outer and is flexibly connected with paddle, the paddle
It is installed in wing top and is electrically connected with fuselage, support frame as described above is installed in engine base bottom and is connected in shower plate, the spray
Plate is spilt as cuboid and is fixed on support frame bottom, the medicine-chest is set to base inner and is fixedly connected to form integral structure,
Holder connection engine base bottom is fixedly connected in camera and with camera, and the camera is set to by holder below engine base
And in the middle part of supporting rack, the separation includes power source transmission device, transmission mechanism, lifting gear, promotion machine for electric installation
Structure, limiting device, heat conversion device, for electric installation, the power source transmission device is set to separation for electric installation inside and and machine
Body pressing connection, the transmission mechanism are installed in for being flexibly connected below electric installation and with power source transmission device, the lifting
Device is set in the middle part of transmission mechanism and lifts connection with for electric installation by transmission mechanism, and the pushing mechanism is set to for electric installation
Both sides are simultaneously flexibly connected with transmission mechanism, and the limiting device connection pushing mechanism limits company in top and with heat conversion device
It connects, the heat conversion device is installed in for electric installation top and is connect with limiting device slot, described to be sheathed on liter for electric installation
Outside falling unit and lift connection.
Further, the power source transmission device includes triggering rod, fixed block, motor rack, motor, terminal box, motor
Axis, cone tooth, motor housing, the triggering rod are connected by notch and fuselage control connection and with motor pressing, the fixed block set
For bottom in electric installation outside triggering rod and set on separation, the motor rack is welded in motor bottom and in motor housing
Portion, the motor are installed on motor housing and are electrically connected with for electric installation, and the terminal box is installed on motor and is fixedly connected with shape
Integralization structure, the motor shaft are rotatablely connected and are set to transmission mechanism both ends with motor, and the cone tooth is welded in motor shaft
Outside is simultaneously connect with gear wheel, and the motor housing is fixed on separation for electric installation inside and is fixedly connected and top and confession
Electric installation is connected.
Further, the transmission mechanism includes gear connecting rod, tooth row, transmission gear, the first belt pulley, transmission skin
Band, the second belt pulley, the second connection tooth row, the gear connecting rod are set to transmission gear upper surface and are fixedly connected with tooth row,
The tooth row both ends are fixed with gear connecting rod and are threadedly coupled with lifting gear by gear connecting rod, and the transmission gear is logical
It crosses axis and is fixed on separation for being connect on electric installation inner wall and with bevel gear, first belt pulley is fixed on the outside of transmission gear
And rotate synchronously, the driving belt connects the first belt pulley on the second belt pulley and being rotatablely connected, second belt pulley
It is symmetrically distributed in lifting gear both sides and is fixed on motor housing and be sequentially connected with driving belt, the second connection tooth row connection
Second belt pulley is simultaneously rotated synchronously and is connect with pushing mechanism gear.
Further, the lifting gear includes threaded drive rod, lifting jacking block, the second fastening block, the screw-driven
Bar runs through for electric installation and is threadedly coupled with tooth row, and the lifting jacking block, which is sheathed on outside threaded drive rod and lifts, is connected to confession
Electric installation bottom, second fastening block are sheathed on outside threaded drive rod and are fixed on separation power supply bottom of device.
Further, the pushing mechanism includes fixed frame, scroll wheel, diamond shape motion bar, vertical tooth row, rectangle channel bar,
The fixed frame is welded in separation for being fixedly connected on electric installation inner wall and with diamond shape motion bar, and the scroll wheel is installed in diamond shape
Motion bar bottom simultaneously connect tooth row rolling connection with second, and the diamond shape motion bar passes through scroll wheel and limiting device activity connects
It connects, the vertical tooth row is welded on the outside of diamond shape motion bar and is connected with for electric installation, and the rectangle channel bar is fixed on diamond shape
It is connected at the top of motion bar and with limiting device.
Further, the limiting device includes limit round pin, connecting rod, wall bar, set block, limit inserted link, the limit
Round pin through connecting rod and on rectangle channel bar, weld with set block bottom and be connected with rectangle channel bar by the connecting rod top
It connects, is fixedly connected for electric installation inner wall on the left of the wall bar with detaching, the set block is sheathed on wall bar outside and passes through connecting rod
With wall bar mobile connection, the limit inserted link, which is fixed on set block top and is limited with heat conversion device, to be connected.
Further, the heat conversion device include slot, motion bar, connecting spring, solar panel, gag lever post,
Hinge axis, link, the slot are embedded at motion bar bottom and are fixedly connected to form integral structure, the motion bar connection
Solar panel is flexibly connected in rear portion and by limiting inserted link with solar panel, and the connecting spring is sheathed on limit
Outside bar and with for being connected at the top of electric installation, the solar panel is installed on for electric installation top and is led to by link
Gag lever post to be crossed to be mutually parallel with for electric installation, the gag lever post is welded in solar panel bottom and is connected with connecting spring,
The hinge axis be set on link and with solar panel hinge connection, the link is installed on for electric installation top.
Further, described for electric installation includes battery block, ball, limit buckle, accumulator, live wire, the battery block
It is fixed at the top of lifting jacking block and is connected with motor housing top, the ball is welded in battery block both ends and lives with vertical tooth row
Dynamic connection, the limit buckle are fixed on separation and are connected for limiting on electric installation inner wall and with live wire, and the accumulator is installed on
Simultaneously be electrically connected with live wire at the top of motor housing, the live wire connects battery block, accumulator on motor and being electrically connected.
Advantageous effect
A kind of anti-tampering unmanned plane of the present invention makes internal controller that controller be made to push and touches by remote control control fuselage
Bar drives motor shaft rotation with motor pressing connection starting switch, motor, and cone tooth is welded on the outside of motor shaft and and transmission gear
Gear connects, and transmission gear and the first belt pulley rotate synchronously, and separation is for electric installation inside in symmetrical structure and by being driven skin
Band is connected, and gear connecting rod is fixed on transmission gear and is connected to right side transmission gear, the gear when transmission gear rotates
Connecting rod drives tooth row to be threadedly coupled with threaded drive rod, so that threaded drive rod is rotated up and lifting jacking block is driven to be raised above
Battery block jack-up is made to detach at the top of battery block and motor housing, battery block is sent to separation for electric installation top and internal controller
Spacing out prevents controller from being operated failure by the influence of battery block, when driving belt is connect with the second pulley drive,
The second connection tooth row being fixed on the second belt pulley, which is moved synchronously and rolled with scroll wheel, to be connected, and scroll wheel passes through the second connection
Top drives connecting rod synchronizing moving and covers block when tooth row is moved left and right drives limit inserted link to be inserted with slot by connecting rod
Slot limit connection makes solar panel be mutually parallel with battery block, and outside is welded in when diamond shape motion bar is mobile to centre
Vertical tooth row rolls connection auxiliary with ball and rises, and can absorb nature heat when solar panel struts is converted into electric energy not
Break and power for battery block, keeps unmanned plane easy to use with flying for long time.
A kind of anti-tampering unmanned plane of the present invention can avoid controller by electricity by raising battery at a distance from controller
It is that electric energy is continuously battery powered that solar panel at the top of while pond influences and put outside battery, which can absorb converting heat, is
Unmanned plane navigation provides sufficient electricity, boosts environmental awareness and takes full advantage of natural resources.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention,
Objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural schematic diagram of anti-tampering unmanned plane of the present invention.
Fig. 2 is structural schematic diagram of the present invention separation for electric installation plane.
Fig. 3 is structural schematic diagram of the present invention separation for electric installation discrete state.
Fig. 4 is the structural schematic diagram of present invention separation power supply device feature amplification.
In figure：Fuselage -1, separation are for electric installation -2, engine base -3, wing -4, paddle -5, supporting rack -6, shower plate -7, medicine
Case -8, holder -9, camera -10, power source transmission device -20, transmission mechanism -21, lifting gear -22, pushing mechanism -23,
Limiting device -24, heat conversion device -25, for electric installation -26, triggering rod -2001, fixed block -2002, motor rack -2003, electricity
Machine -2004, terminal box -2005, motor shaft -2006, cone tooth -2007, motor housing -2008, gear connecting rod -2101, tooth row -
2102, transmission gear -2103, the first belt pulley -2104, driving belt -2105, the second belt pulley -2106, the second tooth connection
Row -2107, threaded drive rod -2201, lifting jacking block -2202, the second fastening block -2203, fixed frame -2301, scroll wheel -
2302, diamond shape motion bar -2303, vertical tooth row -2304, rectangle channel bar -2305, limit round pin -2401, connecting rod -2402, wall
Bar -2403, set block -2404, limit inserted link -2405, slot -2501, motion bar -2502, connecting spring -2503, solar-electricity
Pond plate -2504, gag lever post -2505, hinge axis -2506, link -2507, battery block -2601, ball -2602, limit buckle -
2603, accumulator -2604, live wire -2605.
Specific implementation mode
To make the technical means, the creative features, the aims and the efficiencies achieved by the present invention be easy to understand, with reference to
Specific implementation mode, the present invention is further explained.
Embodiment
- Fig. 4 is please referred to Fig.1, the present invention provides a kind of anti-tampering unmanned plane:Its structure includes fuselage 1, separation for electric installation
2, engine base 3, wing 4, paddle 5, supporting rack 6, shower plate 7, medicine-chest 8, holder 9, camera 10, the fuselage 1 are connected with engine base 3
Top is connect and is set to, the separation is set to 1 inside of fuselage for electric installation 2 and is electrically connected, and the engine base 3 is that round connects fuselage
1 in lower section, and the wing 4 is equally spaced and is welded in 3 outside of engine base and is flexibly connected with paddle 5, and the paddle 5 is installed in machine
4 top of the wing is simultaneously electrically connected with fuselage 1, and support frame as described above 6 is installed in 3 bottom of engine base and is connected in shower plate 7, the shower plate
7 are cuboid and are fixed on 6 bottom of supporting rack, and the medicine-chest 8 is set to 3 inside of engine base and is fixedly connected to form integral structure,
The holder 9 connects 3 bottom of engine base and is fixedly connected in camera 10 and with camera 10, and the camera 10 is set by holder 9
In 3 lower section of engine base and set on 6 middle part of supporting rack, the separation includes power source transmission device 20, transmission mechanism for electric installation 2
21, lifting gear 22, pushing mechanism 23, limiting device 24, heat conversion device 25, for electric installation 26, the power source transmission dress
It sets 20 to be set to separation for 2 inside of electric installation and connect with the pressing of fuselage 1, the transmission mechanism 21 is installed in for 26 lower section of electric installation
And be flexibly connected with power source transmission device 20, the lifting gear 22 is set to 21 middle part of transmission mechanism and passes through transmission mechanism 21
It being connected with being lifted for electric installation 26, the pushing mechanism 23 is set to for 26 both sides of electric installation and is flexibly connected with transmission mechanism 21,
The limiting device 24 connects pushing mechanism 23 and limits connection in top and with heat conversion device 25, and the heat conversion device 25 fills
It is connect set on for 26 top of electric installation and with 24 slot of limiting device, it is described to be sheathed on 22 outside of lifting gear simultaneously for electric installation 26
Lifting connection, the power source transmission device 20 include triggering rod 2001, fixed block 2002, motor rack 2003, motor 2004, connect
Wire box 2005, motor shaft 2006, cone tooth 2007, motor housing 2008, the triggering rod 2001 are connected by notch and the control of fuselage 1
And press and connect with motor 2004, the fixed block 2002 is sheathed on 2001 outside of triggering rod and set on separation in electric installation 2
Bottom, the motor rack 2003 are welded in 2004 bottom of motor and inside motor housings 2008, and the motor 2004 is installed on
Motor housing 2008 is simultaneously electrically connected with for electric installation 26, and the terminal box 2005 is installed on motor 2004 and is fixedly connected to form one
Body structure, the motor shaft 2006 are rotatablely connected with motor 2004 and are set to 21 both ends of transmission mechanism, and the cone tooth 2007 welds
It is connected to 2006 outside of motor shaft and is connect with 21 gear of transmission mechanism, the motor housing 2008 is fixed on separation in electric installation 2
Portion is simultaneously fixedly connected and top is connected with for electric installation 26, and the transmission mechanism 21 includes gear connecting rod 2101, tooth row
2102, transmission gear 2103, the first belt pulley 2104, driving belt 2105, the second belt pulley 2106, second connect tooth row
2107, the gear connecting rod 2101 is set to 2103 upper surface of transmission gear and is fixedly connected with tooth row 2102, the tooth row
2102 both ends are fixed with gear connecting rod 2101 and are threadedly coupled with lifting gear 22 by gear connecting rod 2101, the transmission
Gear 2103 is fixed on by axis to be detached for being connect on 2 inner wall of electric installation and with cone 2007 gear of tooth, first belt pulley
2104 are fixed on 2103 outside of transmission gear and rotate synchronously, and the driving belt 2105 connects the first belt pulley 2104 in second
It on belt pulley 2106 and is rotatablely connected, second belt pulley 2106 is symmetrically distributed in 22 both sides of lifting gear and is fixed on motor
It is sequentially connected with driving belt 2105 on case 2008, the second connection tooth row 2107 connects the second belt pulley 2106 and synchronous turn
It moves and is connect with 23 gear of pushing mechanism, the lifting gear 22 includes threaded drive rod 2201, lifts jacking block 2202, second tightly
Gu block 2203, the threaded drive rod 2201 runs through for electric installation 26 and is threadedly coupled with tooth row 2102, the lifting jacking block
2202 are sheathed on the outside of threaded drive rod 2201 and lift and are connected to for 26 bottom of electric installation, and second fastening block 2203 is arranged
In 2201 outside of threaded drive rod and separation is fixed on for 2 bottom of electric installation, and the pushing mechanism 23 includes fixed frame 2301, rolling
Driving wheel 2302, diamond shape motion bar 2303, vertical tooth row 2304, rectangle channel bar 2305, the fixed frame 2301 are welded in separation and supply
It is fixedly connected on 2 inner wall of electric installation and with diamond shape motion bar 2303, the scroll wheel 2302 is installed in 2303 bottom of diamond shape motion bar
Portion simultaneously connect the rolling connection of tooth row 2107 with second, and the diamond shape motion bar 2303 passes through scroll wheel 2302 and limiting device 24 is lived
Dynamic connection, the vertical tooth row 2304 are welded in 2303 outside of diamond shape motion bar and are connected with for electric installation 26, the rectangle
Channel bar 2305 is fixed on 2303 top of diamond shape motion bar and is connected with limiting device 24, and the limiting device 24 includes that limit is justified
Pin 2401, connecting rod 2402, wall bar 2403, set block 2404, limit inserted link 2405, the limit round pin 2401 run through connecting rod
2402 and on the rectangle channel bar 2305,2402 top of the connecting rod with the welding of 2404 bottom of set block and with rectangle channel bar 2305
It is connected, the left side of the wall bar 2403 is fixedly connected for 2 inner wall of electric installation with detaching, and the set block 2404 is sheathed on wall bar 2403
It is external and by connecting rod 2402 and 2403 mobile connection of wall bar, the limit inserted link 2405 be fixed on cover 2404 top of block and with
The limit connection of heat conversion device 25, the heat conversion device 25 include slot 2501, motion bar 2502, connecting spring 2503, too
Positive energy solar panel 2504, gag lever post 2505, hinge axis 2506, link 2507, the slot 2501 are embedded at motion bar 2502
Bottom is simultaneously fixedly connected to form integral structure, and the motion bar 2502 connects solar panel 2504 and in rear portion and passes through limit
Position inserted link 2405 is flexibly connected with solar panel 2504, the connecting spring 2503 be sheathed on outside gag lever post 2505 and with
It is connected for 26 top of electric installation, the solar panel 2504 is installed on for 26 top of electric installation simultaneously by link 2507
It is mutually parallel with for electric installation 26 by gag lever post 2505, the gag lever post 2505 is welded in 2504 bottom of solar panel simultaneously
It is connected with connecting spring 2503, the hinge axis 2506 is set on link 2507 and connects with 2504 hinge of solar panel
Connect, the link 2507 is installed on for 26 top of electric installation, it is described for electric installation 26 include battery block 2601, ball 2602,
Limit buckle 2603, accumulator 2604, live wire 2605, the battery block 2601 are fixed on 2202 top of lifting jacking block and and motor
2008 top of case is connected, and the ball 2602 is welded in 2601 both ends of battery block and is flexibly connected with vertical tooth row 2304, institute
It states limit buckle 2603 and is fixed on separation for limiting connection on 2 inner wall of electric installation and with live wire 2605, the accumulator 2604 is pacified
It is electrically connected loaded on 2008 top of motor housing and with live wire 2605, the live wire 2605 connects battery block 2601, accumulator
2604 on motor 2004 and being electrically connected.
The present invention provides a kind of anti-tampering unmanned plane, its working principle is that：Make internal control by remote control control fuselage 1
Device makes controller that triggering rod 2001 and the pressing connection starting switch of motor 2004, motor 2004 be pushed to drive 2006 turns of motor shaft
Dynamic, cone tooth 2007 is welded in 2006 outside of motor shaft and is connect with 2103 gear of transmission gear, transmission gear 2103 and the first skin
Belt wheel 2104 rotates synchronously, and separation is connected in symmetrical structure and for 2 inside of electric installation by driving belt 2105, gear connection
Bar 2101 is fixed on transmission gear 2103 and is connected to right side transmission gear 2103, and when transmission gear 2103 rotates, gear connects
Extension bar 2101 drives tooth row 2102 to be threadedly coupled with threaded drive rod 2201, so that threaded drive rod 2201 is rotated up and drives liter
Drop jacking block 2202, which is raised above, makes battery block 2601 be detached with 2008 top of motor housing the jack-up of battery block 2601, by battery block
2601 send to separation for the influence behaviour for preventing controller by battery block 2601 that spaces out with internal controller at the top of electric installation 2
Make failure, when driving belt 2105 and the second belt pulley 2106 are sequentially connected, be fixed on the second belt pulley 2106 second
Connection tooth row 2107 is moved synchronously and is rolled with scroll wheel 2302 and connected, and scroll wheel 2302 is carried out by the second connection tooth row 2107
Top drives 2402 synchronizing moving of connecting rod and covers block 2404 when moving left and right drives limit inserted link 2405 by connecting rod 2402
Solar panel 2504 is set to be mutually parallel with battery block 2601 with the limit connection of 2501 slot of slot, when diamond shape motion bar 2303
It is welded in the vertical tooth row 2304 in outside when mobile to centre and ball 2602 rolls connection auxiliary and rises, works as solar panel
2504 can be absorbed when strutting nature heat be converted into electric energy constantly be battery block 2601 power, so that unmanned plane is flown for a long time
Row, it is easy to use.
Diamond shape motion bar 2303 of the present invention is that four equivalent motion bars of shape size combine to be formed, deformable work
It is dynamic.
Problems solved by the invention is that normal controller and battery are closely located, due to magnetic field problem controller be easy by
The influence of battery causes to control failure, it has not been convenient to use and operate, the present invention is combined with each other by above-mentioned component, can pass through lift
High battery can avoid the solar panel at the top of while controller is influenced by battery and put outside battery at a distance from controller
Absorbable converting heat is that electric energy is continuously battery powered, provides sufficient electricity for unmanned plane navigation, boosts environmental awareness simultaneously
Take full advantage of natural resources.
The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention, for this field skill
For art personnel, it is clear that invention is not limited to the details of the above exemplary embodiments, and without departing substantially from the present invention spirit or
In the case of essential characteristic, the present invention can be realized in other specific forms.Therefore, in all respects, should all incite somebody to action
Embodiment regards exemplary as, and is non-limiting, the scope of the present invention by appended claims rather than on state
Bright restriction, it is intended that including all changes that come within the meaning and range of equivalency of the claims in the present invention
It is interior.Any reference signs in the claims should not be construed as limiting the involved claims.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiment being appreciated that.
Claims (8)
1. a kind of anti-tampering unmanned plane, structure includes fuselage (1), separation for electric installation (2), engine base (3), wing (4), paddle
(5), supporting rack (6), shower plate (7), medicine-chest (8), holder (9), camera (10), it is characterised in that：
The fuselage (1) is connected with engine base (3) and is set to top, and the separation is set to fuselage (1) inside simultaneously for electric installation (2)
Electrical connection, the engine base (3) are that round connects fuselage (1) in lower section, and the wing (4) is equally spaced and is welded in engine base
(3) it is flexibly connected outside and with paddle (5), the paddle (5) is installed in wing (4) top and is electrically connected with fuselage (1), described
Supporting rack (6) is installed in engine base (3) bottom and is connected in shower plate (7), and the shower plate (7) is cuboid and is fixed on branch
Support (6) bottom, the medicine-chest (8) are set to engine base (3) inside and are fixedly connected to form integral structure, and the holder (9) is even
Earthing of frame (3) bottom is fixedly connected in camera (10) and with camera (10), and the camera (10) is set to by holder (9)
Below engine base (3) and in the middle part of supporting rack (6)；
The separation includes power source transmission device (20), transmission mechanism (21), lifting gear (22), promotion for electric installation (2)
Mechanism (23), limiting device (24), heat conversion device (25), for electric installation (26), the power source transmission device (20) is set to
Separation is internal for electric installation (2) and presses connection with fuselage (1), and the transmission mechanism (21) is installed in for below electric installation (26)
And be flexibly connected with power source transmission device (20), the lifting gear (22) is set in the middle part of transmission mechanism (21) and passes through transmission
Mechanism (21) lifts connection with for electric installation (26), and the pushing mechanism (23) is set to for electric installation (26) both sides and and driver
Structure (21) is flexibly connected, and limiting device (24) the connection pushing mechanism (23) limits company in top and with heat conversion device (25)
It connects, the heat conversion device (25) is installed in for electric installation (26) top and is connect with limiting device (24) slot, the power supply
Device (26) is sheathed on lifting gear (22) outside and lifts connection.
2. a kind of anti-tampering unmanned plane according to claim 1, it is characterised in that：Power source transmission device (20) packet
Include triggering rod (2001), fixed block (2002), motor rack (2003), motor (2004), terminal box (2005), motor shaft
(2006), cone tooth (2007), motor housing (2008), the triggering rod (2001) by notch and fuselage (1) control connection and with
Motor (2004) pressing connection, the fixed block (2002) are sheathed on triggering rod (2001) outside and set on separation for electric installation
(2) interior bottom, the motor rack (2003) are welded in motor (2004) bottom and, the motor internal set on motor housing (2008)
(2004) it is installed on motor housing (2008) and is electrically connected with for electric installation (26), the terminal box (2005) is installed in motor
(2004) on and it is fixedly connected to form integral structure, the motor shaft (2006) is rotatablely connected with motor (2004) and set on biography
Motivation structure (21) both ends, the cone tooth (2007) are welded on the outside of motor shaft (2006) and are connect with transmission mechanism (21) gear,
It is internal for electric installation (2) and be fixedly connected and top is connected with for electric installation (26) that the motor housing (2008) is fixed on separation
It connects.
3. a kind of anti-tampering unmanned plane according to claim 1 or 2, it is characterised in that：The transmission mechanism (21) includes
Gear connecting rod (2101), tooth row (2102), transmission gear (2103), the first belt pulley (2104), driving belt (2105),
Two belt pulleys (2106), the second connection tooth row (2107), the gear connecting rod (2101) are set to transmission gear (2103) upper table
Face is simultaneously fixedly connected with tooth row (2102), and tooth row (2102) both ends are fixed with gear connecting rod (2101) and are connected by gear
Extension bar (2101) is threadedly coupled with lifting gear (22), and the transmission gear (2103) is fixed on separation for electric installation by axis
(2) it is connect on inner wall and with cone tooth (2007) gear, first belt pulley (2104) is fixed on the outside of transmission gear (2103)
And rotate synchronously, the driving belt (2105) connects the first belt pulley (2104) on the second belt pulley (2106) and the company of rotation
It connects, second belt pulley (2106) is symmetrically distributed in lifting gear (22) both sides and is fixed on motor housing (2008) and transmission
Belt (2105) be sequentially connected, it is described second connection tooth row (2107) connect the second belt pulley (2106) and rotate synchronously and with push away
Motivation structure (23) gear connects.
4. a kind of anti-tampering unmanned plane according to claim 1, it is characterised in that：The lifting gear (22) includes screw thread
Drive link (2201), lifting jacking block (2202), the second fastening block (2203), the threaded drive rod (2201) are run through for electric installation
(26) and with tooth row (2102) it is threadedly coupled, the lifting jacking block (2202) is sheathed on threaded drive rod (2201) outside and lifts
It is connected to for electric installation (26) bottom, second fastening block (2203) is sheathed on threaded drive rod (2201) outside and is fixed on
Separation is for electric installation (2) bottom.
5. a kind of anti-tampering unmanned plane according to claim 1, it is characterised in that：The pushing mechanism (23) includes fixing
Frame (2301), scroll wheel (2302), diamond shape motion bar (2303), vertical tooth row (2304), rectangle channel bar (2305), the fixation
Frame (2301), which is welded in, to be detached for being fixedly connected on electric installation (2) inner wall and with diamond shape motion bar (2303), the scroll wheel
(2302) it is installed in diamond shape motion bar (2303) bottom and connect tooth row (2107) with second and roll connection, the diamond shape motion bar
(2303) it is flexibly connected with limiting device (24) by scroll wheel (2302), the vertical tooth row (2304) is welded in diamond shape activity
It is connected on the outside of bar (2303) and with for electric installation (26), the rectangle channel bar (2305) is fixed on diamond shape motion bar (2303) top
Portion is simultaneously connected with limiting device (24).
6. a kind of anti-tampering unmanned plane according to claim 1 or 5, it is characterised in that：The limiting device (24) includes
Limit round pin (2401), connecting rod (2402), wall bar (2403), set block (2404), limit inserted link (2405), the limit round pin
(2401) run through connecting rod (2402) and be set on rectangle channel bar (2305), connecting rod (2402) top and set block (2404)
Bottom, which is welded, to be simultaneously connected with rectangle channel bar (2305), is fixed for electric installation (2) inner wall on the left of the wall bar (2403) with detaching
Connection, the set block (2404) are sheathed on wall bar (2403) outside and connect by the way that connecting rod (2402) and wall bar (2403) are mobile
It connects, the limit inserted link (2405), which is fixed on set block (2404) top and is limited with heat conversion device (25), to be connected.
7. a kind of anti-tampering unmanned plane according to claim 1, it is characterised in that：The heat conversion device (25) includes inserting
Slot (2501), motion bar (2502), connecting spring (2503), solar panel (2504), gag lever post (2505), hinge axis
(2506), link (2507), the slot (2501) are embedded at motion bar (2502) bottom and are fixedly connected to form integration
Structure, motion bar (2502) the connection solar panel (2504) is in rear portion and by limiting inserted link (2405) and solar energy
Solar panel (2504) is flexibly connected, the connecting spring (2503) be sheathed on gag lever post (2505) it is external and with for electric installation (26)
Top is connected, and the solar panel (2504) is installed on for electric installation (26) top and is passed through by link (2507)
Gag lever post (2505) is mutually parallel with for electric installation (26), and the gag lever post (2505) is welded in solar panel (2504) bottom
Portion is simultaneously connected with connecting spring (2503), and the hinge axis (2506) is set on link (2507) and and solar panel
(2504) hinge connection, the link (2507) are installed on for electric installation (26) top.
8. a kind of anti-tampering unmanned plane according to claim 1 or 2, it is characterised in that：It is described to include for electric installation (26)
Battery block (2601), ball (2602), limit buckle (2603), accumulator (2604), live wire (2605), the battery block
(2601) it is fixed at the top of lifting jacking block (2202) and is connected with motor housing (2008) top, the ball (2602) is welded in
Battery block (2601) both ends are simultaneously flexibly connected with vertical tooth row (2304), and the limit buckle (2603) is fixed on separation for electric installation
(2) limit on inner wall and with live wire (2605) and connect, the accumulator (2604) be installed at the top of motor housing (2008) and with
Live wire (2605) is electrically connected, and live wire (2605) the connection battery block (2601), accumulator (2604) are in motor (2004)
It goes up and is electrically connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810147472.8A CN108341063A (en) | 2018-02-12 | 2018-02-12 | A kind of anti-tampering unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810147472.8A CN108341063A (en) | 2018-02-12 | 2018-02-12 | A kind of anti-tampering unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108341063A true CN108341063A (en) | 2018-07-31 |
Family
ID=62959395
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810147472.8A Pending CN108341063A (en) | 2018-02-12 | 2018-02-12 | A kind of anti-tampering unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108341063A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112734168A (en) * | 2020-12-22 | 2021-04-30 | 国网浙江省电力有限公司温州供电公司 | Unmanned aerial vehicle-based overhead transmission line channel inspection system and hidden danger analysis method |
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| US9807996B1 (en) * | 2016-05-28 | 2017-11-07 | Simon Siu-Chi Yu | Bug eater |
| CN206766340U (en) * | 2017-06-07 | 2017-12-19 | 深圳市海旭飞科技有限公司 | A kind of large area pesticide spraying unmanned plane |
| CN107646818A (en) * | 2017-09-23 | 2018-02-02 | 佛山净潭机械科技有限公司 | A kind of chemical spraying device of afforestation |
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| US20170178618A1 (en) * | 2015-12-18 | 2017-06-22 | Amazon Technologies, Inc. | Carbon nanotube transducers on propeller blades for sound control |
| US9807996B1 (en) * | 2016-05-28 | 2017-11-07 | Simon Siu-Chi Yu | Bug eater |
| CN206569249U (en) * | 2016-12-08 | 2017-10-20 | 天津中翔腾航科技股份有限公司 | A kind of folding four rotor wing unmanned aerial vehicle |
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| CN112734168A (en) * | 2020-12-22 | 2021-04-30 | 国网浙江省电力有限公司温州供电公司 | Unmanned aerial vehicle-based overhead transmission line channel inspection system and hidden danger analysis method |
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Application publication date: 20180731 |
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