A kind of remotely pilotless machine seeding apparatus and its type of seeding
Technical field
The present invention relates to unmanned aerial vehicles sowing technical fields, and in particular to a kind of remotely pilotless machine seeding apparatus and its sowing side
Method.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft or fully or intermittently independently operated by car-mounted computer that presetting apparatus manipulates.
Compared with manned aircraft, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Nobody
Machine press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane
+ sector application is that unmanned plane has really just needed;At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief,
Observe wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field
Application, greatly expanded the purposes of unmanned plane in itself, developed country is also in actively extension sector application and development unmanned plane
Technology.
With the input subsidies that country increases agricultural, the equipment for plant protection of modernization is going into the hand of peasant.Plant protection
The appearance of machinery solves the deficiency of labour, improves the precision of production efficiency and agricultural.Plant protection is agricultural and forestry production
Important component.It is to ensure that one of important measures of agriculture and forestry high yield good harvest.In order to efficiently and effectively carry out plant protection,
Various control methods and positive effect should be played, implement the policy of " putting prevention first, integrated control ", disease, worm, crop smothering and its
Its harmful organism is eliminated before harm, it is not made to cause disaster.
Plant protection unmanned plane, as the term suggests it is the UAV for agriculture and forestry plant protection operation.
But in the prior art, the complete seed of unmanned aerial vehicles sowing is often eaten up by flying bird, leverages sowing effect, and
Some seeds can not be buried in the earth.
The content of the invention
For more than technical problem, the present invention provides a kind of remotely pilotless machine seeding apparatus and its type of seeding, Neng Goushi
Now to seed effectively to be injected in the soil that need to be sowed and dispersed flying bird nearby, prevent flying bird from being preyed on to seed.
The technical scheme is that:A kind of remotely pilotless machine seeding apparatus, mainly includes:Unmanned plane and remote controler, institute
Stating unmanned plane includes:Main duct, tail duct, unmanned plane antenna, photographic device, stent, bluetooth module, sensing receiver, GPRS
Module, stand-by power supply, PCL controllers, inverter, two-dimentional linkage controller, accumulator group, protective device, engine, pumping dress
Put, compression pump, kind storehouse, left duct, right duct, solar panel, air compression big gun, the main duct is located in unmanned plane
Portion, main duct include:It is main culvert propeller, it is main culvert motor, main culvert stent, it is described it is main culvert propeller totally four and circumferentially uniformly
It is installed on the main culvert motor, main culvert motor is installed on the main culvert stent, and main culvert stent is connected with unmanned plane;The tail
Duct is located at unmanned drive end unit, and tail duct includes:Tail contains stent, tail contains motor, tail contains shaft, tail contains propeller, and the tail is contained
Stent is installed on unmanned drive end unit, and the tail contains motor and is installed on tail culvert stent rear, and the tail contains shaft and is installed on tail culvert electricity
Machine rear, the tail contain propeller and totally three and are circumferentially uniformly installed on tail and contain in shaft;The unmanned plane antenna installation
At the top of unmanned plane at prow, the photographic device is installed on uav bottom at prow, and photographic device includes:Mirror
Head, video camera, left and right motor, connecting rod, upper and lower motor, the camera lens are installed on the video camera front end, and video camera is installed on institute
Left and right motor front end is stated, left and right motor is connected with the connecting rod bottom, and connecting rod top is connected with the motor front end up and down, up and down
Motor is installed on uav bottom at prow;Totally four, the stent is uniformly installed on uav bottom, the bluetooth mould
Block is installed on upper strata in unmanned plane, and at prow, the sensing receiver is installed on bluetooth module rear, the GPRS module
It is installed on sensing receiver, the stand-by power supply is installed on sensing receiver rear, and the PCL controllers are installed on standby electricity
Source rear, the inverter installation and PCL controllers rear, the accumulator group are installed on inverter rear, the two dimension connection
Movement controller is installed on above accumulator group, and the protective device is installed on unmanned plane inner top at tail, protective device
Including:Parachute system and electromagnetic valve two, the parachute system are installed on two lower section of electromagnetic valve, electromagnetic valve two
Unmanned plane inner top is installed at tail;The engine is located in unmanned plane in the middle part of lower floor, and the air extractor is located at
At tail, air extractor includes unmanned plane lower inner surface:Exhaust tube and filter screen, described exhaust tube one end and filter screen
Connection, the other end are connected with the compression pump, and filter screen is located at unmanned plane lower inner surface at tail;Compression pump is equipped with
Air inlet and gas outlet, the air inlet are installed on compression pump bottom-rear, and the gas outlet is installed on compression pump front center,
In lower floor in unmanned plane at prow, kind storehouse includes described kind of position in storehouse:Plants case, seed inlet, conveying crawler belt, electromagnetic valve two,
The plants case is located in kind of storehouse, and the seed inlet is installed on plants case front top and is connected with unmanned plane, the conveying crawler belt
Kind of an orlop portion is installed on, the electromagnetic valve two is installed on conveying crawler belt rear;The left duct is installed in unmanned plane left wing,
Left duct includes:It is left culvert propeller, it is left culvert motor, it is left culvert shaft, left culvert stent, it is described it is left culvert propeller totally three and uniformly
Be installed on it is described it is left culvert shaft on, it is left culvert shaft be installed on it is described it is left culvert motor above, it is left culvert motor be installed on it is described it is left contain branch
On frame and left culvert stent is connected with unmanned plane;The right duct is installed in unmanned plane right flank, and right duct includes:Right culvert spiral
Paddle, right culvert motor, right culvert shaft, right culvert stent, the right culvert propeller totally three and are uniformly installed on the right culvert shaft
On, it is right culvert shaft be installed on it is described it is right culvert motor above, it is right culvert motor be installed on it is described it is right culvert stent on and it is right culvert stent with
Unmanned plane connects;Totally two pieces of the solar panel, is respectively arranged on unmanned plane or so wing, the air compression big gun peace
It is connected between compression pump and kind storehouse and respectively with compression pump with kind storehouse, air compression big gun includes:Air tank, electromagnetic valve
3rd, kind of a mouth, transmitting tube are gone out, the air tank is installed below gas outlet, and the electromagnetic valve three is installed below air tank, institute
It states out kind of a mouth front end to be connected with plants case, rear is connected with the transmitting tube, and transmitting tube is installed on three lower section of electromagnetic valve;PCL is controlled
Device processed by data cable respectively with main duct, tail duct, photographic device, bluetooth module, sensing receiver, stand-by power supply, inversion
Device, engine, air extractor, compression pump, kind storehouse, left duct, right duct, air compression battery connect, and solar panel passes through
Conducting wire is connected with two-dimentional linkage controller, and two-dimentional linkage controller is connected by conducting wire with accumulator group, and accumulator group is by leading
Line is connected with inverter, engine by conducting wire respectively with main duct, tail duct, photographic device, air extractor, compression pump, kind
Storehouse, left duct, right duct, air compression battery connect, and sensing receiver connects respectively with unmanned plane antenna, video camera and GPRS module
It connects;Unmanned plane antenna is connected by wireless with the remote controler.
Further, the forward flight speed of the unmanned plane at work is 50-60m/min;After preventing excessive velocities
Sowing is spaced larger waste plantation space and speed shouts the smaller crop growth in sowing interval and receives influence mutually slowly excessively.
Further, the air compression big gun working frequency is 60 times/min, compresses big gun by air and seed is injected soil
In ground, 60 times/min just meets the growth distance between crops while ensure that seed successful growth probability.
Further, the protective device works automatically when decrease speed is more than 20m/s;Prevent the present apparatus from being sent out in high-altitude
It drops when outside business, not only ensure that lower section passerby's safety, more effectively prevent the damage of unmanned plane.
Further, the method for work of described device is:
A. the preparation stage:Operating personnel will fill it up with seed, Ran Houjian by the seed inlet set in described kind of storehouse in plants case
It looks into the unmanned plane and is connected with the remote controller signal and whether succeeded;
B. fly to job site:The first input service place in the remote controler of operating personnel, then presses institute on remote controler
That states reaches job site key mapping, and the unmanned plane controls the main duct, tail to contain according to the GPRS module and PCL controllers
Road, engine, left duct, to designated position, are then observed with the automatic flight of right duct work by observing the locating and displaying screen
Unmanned plane during flying to job site progress;
C. start to work:Operating personnel by the camera lens raise up key mapping, that camera lens declines key mapping, pan left key mapping, camera lens is right
Turn key position adjusts the viewing angle of the camera, and the building ring of the unmanned plane is observed by the image display screen
Border, then by the movement of the advance key mapping, retrogressing key mapping, left winged key mapping, right winged key mapping control unmanned plane, finally by institute
State the sowing work that air compression big gun work key mapping stops key mapping control unmanned plane with air compression big gun;
D. make a return voyage:After work, operating personnel assign instruction of making a return voyage by key mapping of making a return voyage described on the remote controler, then
Unmanned plane is observed by observing the locating and displaying screen to make a return voyage progress.
Compared with prior art, beneficial effects of the present invention are:
1st, the present invention, which efficiently solves seed in the prior art, can not be implanted into the technical barrier in soil, and compressing big gun by air will
Seed is injected in soil, and injects certain depth so as to ensure that seed successful growth probability.
2nd, the present invention is provided with protective device, prevents the present invention from dropping when accident occurs for high-altitude, not only ensure that lower section
Passerby's safety, more effectively prevents user to generate greater loss.
3rd, the present invention solve thes problems, such as that flying bird encroaches on the soil just sowed in the prior art, passes through air
The sound that big gun generates is compressed, the flying bird around soil is dispersed, adds land yield.
4th, structure novel of the present invention, cost is relatively low, and full-featured, and efficiently solving the part prior art can not solve
The problem of, and efficiency increases compared to similar-type products, is suitble to be widely popularized.
Description of the drawings
Fig. 1 is the unmanned plane outside drawing of the present invention;
Fig. 2 is the structure diagram of unmanned plane of the present invention;
Fig. 3 is the schematic diagram of controller of the present invention;
1- unmanned planes, 2- remote controlers, the main ducts of 3-, 4- tails duct, 5- unmanned planes antenna, 6- photographic devices, 7- stents, 8- bluetooths
Module, 9- sensing receivers, 10-GPRS modules, 11- stand-by power supplies, 12-PCL controllers, 13- inverters, 14- two dimension linkages
Controller, 15- accumulators group, 16- protective devices, 17- engines, 18- air extractors, 19- compression pumps, 20- kinds storehouse, 21- are left
The right duct of duct, 22-, 23- solar panels, 24- air compression big gun, 201- switches key mapping, 202- go to job site key
Position, 203- image display screens, 204- camera lenses raise up key mapping, 205- camera lenses decline key mapping, 206- pan lefts key mapping, 207- camera lenses
Right-hand rotation key mapping, 208- stand-by power supplies open key mapping, 209- air compresses big gun work key mapping, 210- air compression big gun stops key mapping,
211- protective devices open key mapping, 212- advances key mapping, 213- and retreat the left winged key mapping of key mapping, 214-, the right winged key mappings of 215-, 216-
Locating and displaying screen, 217- make a return voyage, and key mapping, 218- remote controlers antenna, 301- are main to contain the main culvert branch of the main culvert motor of propeller, 302-, 303-
Frame, 401- tails contain stent, 402- tails contain motor, 403- tails contain shaft, 404- tails contain propeller, 601- camera lenses, 602- video cameras,
603- or so motors, 604- connecting rods, 605- motor, 1601- parachute systems, 1602- electromagnetic valves one, 1801- pumpings up and down
Pipe, 1802- filter screens, 1901- air inlets, 1902- gas outlets, 2001- plants cases, 2002- seed inlets, 2003- conveying crawler belt,
2004- electromagnetic valves two, 2101- be left contain propeller, 2102- it is left contain motor, 2103- it is left contain shaft, 2104- it is left contain stent,
2201- is right to contain the right culvert motor of propeller, 2202-, the right culvert shafts of 2203-, the right culvert stents of 2204-, 2401- air tanks, 2402- electricity
Magnet valve door three, 2403- go out kind of a mouth, 2404- transmitting tubes.
Specific embodiment
In order to more fully explain the implementation of the present invention, a kind of following remotely pilotless machine seeding apparatus and its sowing side are provided
The embodiment of method.These embodiments are only to explain rather than limit the scope of the invention.Implement below by typical
The present invention is described further for example.
Embodiment 1:
As shown in Figure 1, a kind of remotely pilotless machine seeding apparatus, mainly includes:Unmanned plane 1 and remote controler 2, unmanned plane 1 include:It is main
It is duct 3, tail duct 4, unmanned plane antenna 5, photographic device 6, stent 7, bluetooth module 8, sensing receiver 9, GPRS module 10, standby
With power supply 11, PCL controllers 12, inverter 13, two-dimentional linkage controller 14, accumulator group 15, protective device 16, engine
17th, air extractor 18, compression pump 19, kind storehouse 20, left duct 21, right duct 22, solar panel 23, air compression big gun 24,
Main duct 3 is located at 3 middle part of unmanned plane, and main duct 3 includes:Main culvert propeller 301, main culvert motor 302, main culvert stent 303, main culvert
Propeller 301 totally four and be circumferentially uniformly installed on it is main culvert motor 302 on, it is main culvert motor 302 be installed on it is main culvert stent 303
On, main culvert stent 303 is connected with unmanned plane 1;Tail duct 4 is located at 1 afterbody of unmanned plane, and tail duct 4 includes:Tail contains stent 401, tail
Contain motor 402, tail culvert shaft 403, tail and contain propeller 404, tail contains stent 401 and is installed on 1 afterbody of unmanned plane, and tail contains motor 402
It is installed on tail and contains stent 401 rear, tail, which contains shaft 403 and is installed on tail, contains 402 rear of motor, and tail contains propeller 404, and totally three simultaneously
And it is circumferentially uniformly installed on tail and contains in shaft 403;Unmanned plane antenna 5 is installed on 1 top of unmanned plane at prow, camera shooting dress
It puts 6 and is installed on 1 bottom of unmanned plane at prow, photographic device 6 includes:Camera lens 601, video camera 602, left and right motor 603, company
Bar 604, upper and lower motor 605, camera lens 601 are installed on 602 front end of video camera, and video camera 602 is installed on 603 front end of left and right motor,
Left and right motor 603 is connected with 604 bottom of connecting rod, and 604 top of connecting rod is connected with upper and lower 605 front end of motor, and upper and lower motor 605 is installed
In 1 bottom of unmanned plane at prow;Totally four, stent 7, is uniformly installed on 1 bottom of unmanned plane, and bluetooth module 8 is installed on nobody
At prow, sensing receiver 9 is installed on 8 rear of bluetooth module on upper strata in machine 1, and GPRS module 10 is installed on sensing receiver
On 9, stand-by power supply 11 is installed on 9 rear of sensing receiver, and PCL controllers 12 are installed on 11 rear of stand-by power supply, inverter 13
Installation and 12 rear of PCL controllers, accumulator group 15 are installed on 13 rear of inverter, and two-dimentional linkage controller 14 is installed on electric power storage
15 top of pond group, protective device 16 are installed on 1 inner top of unmanned plane at tail, and protective device 16 includes:Parachute system
1601 are installed on 2 1602 lower section of electromagnetic valve with electromagnetic valve 2 1602, parachute system 1601, and electromagnetic valve 2 1602 is pacified
Loaded on 1 inner top of unmanned plane at tail;Engine 17 is located in unmanned plane 1 in the middle part of lower floor, and air extractor 18 is located at nobody
At tail, air extractor 18 includes 1 lower inner surface of machine:Exhaust tube 1801 and filter screen 1802,1801 one end of exhaust tube
It is connected with filter screen 1802, the other end is connected with compression pump 19, and filter screen 1802 is located at 1 lower inner surface of unmanned plane close to tail
Place;Compression pump 19 is equipped with air inlet 1901 and gas outlet 1902, and air inlet 1901 is installed on 19 bottom-rear of compression pump, outlet
Mouth 1902 is installed on 19 front center of compression pump, and kind storehouse 20 is located at lower floor in unmanned plane 1, and at prow, kind storehouse 20 includes:Kind
Case 2001, seed inlet 2002, conveying crawler belt 2003, electromagnetic valve 2 2004, plants case 2001 are located in kind of storehouse 20, seed inlet 2002
It is installed on 2001 front top of plants case and is connected with unmanned plane 1, conveying crawler belt 2003 is installed on 2001 bottom of kind of storehouse, solenoid valve
Door 2 2004 is installed on 2003 rear of conveying crawler belt;Left duct 21 is installed in 1 left wing of unmanned plane, and left duct 21 includes:Zuo Han
Propeller 2101, it is left culvert motor 2102, it is left culvert shaft 2103, it is left culvert stent 2104, it is left culvert propeller 2101 totally three and
Even to be installed in left culvert shaft 2103, left culvert shaft 2103 is installed on left 2102 top of culvert motor, and left culvert motor 2102 is installed on
On left culvert stent 2104 and left culvert stent 2104 is connected with unmanned plane 1;Right duct 21 is installed in 1 right flank of unmanned plane, right culvert
Road 22 includes:Right culvert propeller 2201, right culvert motor 2202, right culvert shaft 2203, right culvert stent 2204, right culvert propeller 2201
It totally three and is uniformly installed in right culvert shaft 2203, right culvert shaft 2203 is installed on right culvert motor 2202 top, right to contain electricity
Machine 2202 is installed on right culvert stent 2204 and right culvert stent 2204 is connected with unmanned plane 1;Totally two pieces of solar panel 23,
Be respectively arranged on 1 or so wing of unmanned plane, air compression big gun 24 be mounted on compression pump 19 and kind storehouse 20 between and respectively with
Compression pump 19 is connected with kind storehouse 20, and air compression big gun 24 includes:Air tank 2401, electromagnetic valve 3 2402 go out kind of mouth 2403, hair
Pipe 2404 is penetrated, air tank 2401 is installed on 1902 lower section of gas outlet, and electromagnetic valve 3 2402 is installed on 2401 lower section of air tank, goes out
2403 front end of kind mouth is connected with plants case 2001, and rear is connected with transmitting tube 2404, and transmitting tube 2404 is installed on electromagnetic valve three
2402 lower sections;PCL controllers 12 by data cable respectively with main duct 3, tail duct 4, photographic device 6, bluetooth module 8, sensing
Receiver 9, stand-by power supply 11, inverter 13, engine 17, air extractor 18, compression pump 19, kind storehouse 20, left duct 21, right culvert
Road 22, air compression big gun 24 connect, and solar panel 23 is connected by conducting wire with two-dimentional linkage controller 14, two dimension linkage control
Device 14 processed is connected by conducting wire with accumulator group 15, and accumulator group 15 is connected by conducting wire with inverter 13, and engine 17 passes through
Conducting wire respectively with main duct 3, tail duct 4, photographic device 6, air extractor 18, compression pump 19, kind storehouse 20, left duct 21, right culvert
Road 22, air compression big gun 24 connect, and sensing receiver 9 is connected respectively with unmanned plane antenna 5, video camera 6 with GPRS module 10;Nothing
Man-machine antenna 5 with remote controler 2 by being wirelessly connected.
Wherein, the forward flight speed of unmanned plane 1 at work is 60m/min;Prevent after excessive velocities sowing interval compared with
Waste plantation space is spaced smaller crop growth with the excessively slow rear sowing of speed and receives influence mutually greatly;Air compression big gun 24 works
Frequency is 60 times/min, compresses big gun 24 by air and injects seed in soil, while ensure that seed successful growth probability
60 times/min just meets the growth distance between crops;Protective device 16 is started building certainly when decrease speed is more than 20m/s
Make;It prevents the present apparatus from dropping when accident occurs for high-altitude, not only ensure that lower section passerby's safety, more effectively user is prevented to produce
Raw greater loss.
The method of work of the present apparatus is:
A. the preparation stage:Operating personnel will fill it up with seed by the seed inlet 2002 set in kind of storehouse 20 in plants case 2001, then
It checks that unmanned plane 1 is connected with 2 signal of remote controler whether to succeed;
B. fly to job site:The first input service place in remote controler 2 of operating personnel, then presses reaching on remote controler 2
To job site key mapping 202, unmanned plane 1 controls main duct 3, tail duct 4 according to GPRS module 10 and PCL controllers 12, starts
Machine 17, left duct 21 and right duct 22 work automatic flight to designated position, then observe nothing by observing locating and displaying screen 216
Man-machine 1 flies to the progress of job site;
C. start to work:Operating personnel by camera lens raise up key mapping 204, camera lens decline key mapping 205, pan left key mapping 206, mirror
Head right-hand rotation key mapping 207 adjusts the viewing angle of camera 6, and the building ring of unmanned plane 1 is observed by image display screen 203
Then border flies the movement of the control unmanned plane 1 of key mapping 215 by advance key mapping 212, retrogressing key mapping 213, left winged key mapping 214, the right side,
The sowing work of unmanned plane 1 is controlled with air compression big gun stopping key mapping 210 finally by air compression big gun work key mapping 209;
D. make a return voyage:After work, operating personnel assign instruction of making a return voyage by the key mapping 217 of making a return voyage on remote controler 2, then pass through
Observation locating and displaying screen 216 observes unmanned plane 1 and makes a return voyage progress.
Finally it should be noted that:The above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations;Although
The present invention is described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that:It still may be used
To modify to the technical solution recorded in previous embodiment or carry out equivalent substitution to which part technical characteristic;And
These modifications are replaced, and the essence of appropriate technical solution is not made to depart from the spirit and model of technical solution of the embodiment of the present invention
It encloses.