CN104614150B - Plant protection unmanned plane sprays Two phase flow field lab simulation test platform and method - Google Patents
Plant protection unmanned plane sprays Two phase flow field lab simulation test platform and method Download PDFInfo
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- CN104614150B CN104614150B CN201510051943.1A CN201510051943A CN104614150B CN 104614150 B CN104614150 B CN 104614150B CN 201510051943 A CN201510051943 A CN 201510051943A CN 104614150 B CN104614150 B CN 104614150B
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Abstract
The invention discloses a kind of plant protection unmanned plane sprinkling Two phase flow field lab simulation test platform and method, the analog testing platform, including console, analog machine and Pcnten-1 yne-4 detection and/or wind field detection equipment etc..The analog testing platform is used to simulate the low aerial work of plant protection unmanned plane, indoor dispenser experiment of the different type of machines unmanned plane in different work height, flying speed and different spray concentrations can be carried out, it is easy to research unmanned plane low latitude spray Two phase flow field and sprinkling distribution, optimize unmanned plane job parameter, be that unmanned plane plant protection operation specifies corresponding code.
Description
Technical field
The invention belongs to agriculture and forestry aviation machine technical field, and in particular to a kind of simulation test equipment and corresponding test
Method.
Background technology
In aerial sprays operation, the flying height and flying speed of plant protection unmanned plane be influence sprinkling quality it is important because
Element.Different type correspondence different work parameters, although field test is closer to actual conditions, influence mist droplet deposition distribution
Factor is uncontrollable in the wild.In the wild, change can cause the change of flight attitude at the time of wind speed and direction so that obtain
Obtain an accurate data extremely difficult, these uncertainties make to repeat there is sizable difference between testing.In order to determine
Different application method or different type of machines shower nozzles are to mist droplet deposition drift performance impact, it is necessary to design a kind of applicable laboratory test
Method.
The content of the invention
It is an object of the invention to propose that a kind of general plant protection unmanned plane sprays Two phase flow field lab simulation test platform,
Corresponding analog detection method is provided simultaneously, is that research plant protection unmanned plane pesticide spraying gas-liquid two-phase flow field and sprinkling distribution are provided
Means of testing, to enable aviation plant protection scientific development.
The technical scheme that the present invention is provided is：
A kind of plant protection unmanned plane sprays Two phase flow field lab simulation test platform, it is characterised in that including console, simulation
Equipment and Pcnten-1 yne-4 detection and/or wind field detection equipment；
The analog machine provided with the skyborne beam guideway of frame, moved along beam guideway guide rail electric car, be suspended in and lead
Elevating mechanism, simulation of wind and spraying system and control guide rail electric car, elevating mechanism, simulation of wind and spray below rail electric car
The servo-control system of mist system operation, the servo-control system is connected by wired or wireless mode and console communication
Connect；
The elevating mechanism includes expansion link and is suspended on the loading stand of expansion link bottom, the simulation of wind and spray
Mist system is arranged in the loading stand；
Simulation of wind and the simulation of wind module of spraying system include rotor and rotor motor, and the rotor is installed
On a hollow rotating shaft, below loading stand；Driven through the rotor in loading stand, with loading stand hollow rotating shaft upper end
Dynamic motor connection；
The spray module of simulation of wind and spraying system includes medicine-chest, liquid pump system, spray boom, shower nozzle and a hollow pipe
Set, the medicine-chest, liquid pump system are fixed in the loading stand, and the upper end of the hollow pipe sleeve is fixed with loading stand to be connected
Connect, pipe sleeve bottom is from the hollow rotating shaft central cavity through stretching out, and spray boom is fixedly connected on hollow pipe sleeve bottom, liquid pump system
Output pipe from hollow pipe sleeve through being connected with spray boom, decoction is spilt from the shower nozzle on spray boom.
Further technical scheme also includes：
Bearing block of the upper surface of the loading stand provided with the fixed hollow rotating shaft, the bearing block include pedestal with
And the rolling bearing in pedestal, hollow rotating shaft passes through in the middle of the rolling bearing, is connected with the bearing inner race, hollow turn
Axle enters action edge by the power output shaft of gear and the rotor motor from the upper end that the bearing stretches out and transmitted, covering
The gear cap of gear is fixed on the pedestal of the bearing block, and the upper end of the hollow pipe sleeve is then fixed on the gear cap
On.
The blade of the rotor is fixed on the side of hollow rotating shaft by mounting seat, and the mounting seat includes one and installs bottom
Plate, hollow rotating shaft is in mounting plane of the corresponding position provided with connection mounting base；At least two are provided with the mounting base
Concentric long arc-shaped holes, and provided with the stop screw or bolt pair being adapted to long arc-shaped holes, will by stop screw or bolt pair
The mounting plane locking of mounting base and hollow rotating shaft.In use, the angle windward of rotor blade can be adjusted by being rotatablely installed seat
Spend (propeller pitch angle).
The bottom of the hollow rotating shaft is installed with a rectangle pipe sleeve, and Rotor mount is fixedly connected on the rectangular tube
On the mounting plane for covering the week side of boss.
The joint face of the mounting base and hollow rotating shaft is provided with a central shaft, and mounting plane is provided with the insertion center
The centre bore of axle, the center of circle of the long arc-shaped holes falls on the axle center of the central shaft.
The lower section of the loading stand is also provided with the rolling bearing of a fixation hollow rotating shaft, and hollow rotating shaft is in the middle of the bearing
Pass through, be connected with the bearing inner race, the bearing is fixed on below loading stand by bearing sleeve.
The expansion link is preferred to use the scissor type telescopic mechanism of electric cylinder driving, there is higher stability and carrying energy
Power.
The shower nozzle is preferred to use rotating sprinkler.
A kind of single rotor wing unmanned aerial vehicle for platform as described above sprays Two phase flow field analog detection method, and its feature exists
In comprising the following steps：
One) loading stand is fallen to electric in analog machine servo-control system by console, unmanned plane to be measured is installed
Rotor, adjusts spacing, the inclination angle of shower nozzle, debugs spray module；
Two) relevant position arrangement Pcnten-1 yne-4 detection indoors and/or wind field detection equipment；
Three) loading stand is risen to specified altitude assignment by console；
Four) rotor motor is started by console, rotor wing rotation is reached the rotating speed specified；
Five) drive rail electric car to travel in orbit by console, after electric car reaches pre-set velocity, start spraying mould
Block, makes shower nozzle complete sprinkling in the wind field that rotor is formed；
Six) information of the detection of finishing analysis Pcnten-1 yne-4 and/or wind field detection equipment collection or display, completes simulation and surveys
Examination.
In the unmanned plane that current agriculture and forestry are used, single rotor wing unmanned aerial vehicle quality is big, rotating speed is high, directly using list rotor nobody
Empirical risk is than larger indoors for machine, so devising above-mentioned platform carries out lab simulation, and multi-rotor unmanned aerial vehicle quality is small, directly
Connect and many rotor small-sized plant protection unmanned planes are fixed in loading stand, you can carry out the biphase gas and liquid flow of small-sized multi-rotor unmanned aerial vehicle
Field detection.
A kind of multi-rotor unmanned aerial vehicle for platform as described above sprays Two phase flow field analog detection method, and its feature exists
In comprising the following steps：
One) loading stand is fallen, hollow stem sleeve pipe, spray boom are removed to electric in servo-control system by console, will
Multi-rotor unmanned aerial vehicle to be measured is fixedly connected on below loading stand, adjusts spacing, the inclination angle of multi-rotor unmanned aerial vehicle shower nozzle, debugging
Multi-rotor unmanned aerial vehicle spraying system；
Two) relevant position arrangement Pcnten-1 yne-4 detection indoors and/or wind field detection equipment；
Three) loading stand is risen to specified altitude assignment by console；
Four) unmanned plane is started by the remote-control handle of multi-rotor unmanned aerial vehicle, its rotor is reached predetermined rotating speed；
Five) drive rail electric car to travel in orbit by console, after electric car reaches pre-set velocity, pass through remote control hand
The spraying system that handle starts multi-rotor unmanned aerial vehicle is sprayed；
Six) information of the detection of finishing analysis Pcnten-1 yne-4 and/or wind field detection equipment collection or display, completes simulation and surveys
Examination.
Beneficial effects of the present invention：
When plant protection unmanned plane is sprayed insecticide, directly the vortex wind field work that Ji produces downward spiral will be revolved by plant protection unmanned plane
With the flying height of helicopter is low (typically in below 10m) in the actual spraying operation of agricultural chemicals, and downward wind field is to pesticide spraying
Influential effect is big.Analog testing platform of the present invention be used for simulate the low aerial work of plant protection unmanned plane, can carry out different type of machines nobody
Machine is easy to research unmanned plane low latitude spray in the indoor dispenser experiment of different work height, flying speed and different spray concentrations
Two phase flow field and sprinkling distribution, optimize unmanned plane job parameter, are that unmanned plane plant protection operation specifies corresponding code.And due to mould
In fixed position height, flying speed when proposing for work, metastable wind field can be formed, in repeating to test,
Stabilization, believable test data can be obtained.
Brief description of the drawings
Fig. 1 is the overall structure diagram of platform of the present invention；
Fig. 2 illustrates for the stereochemical structure of the rail electric car of the single rotor simulation of wind of the present invention, elevating mechanism, rotor and spray boom
Figure；
Fig. 3 is Fig. 2 main structure diagram；
Fig. 4 is Fig. 2 side structure schematic view；
Fig. 5 is Fig. 2 overlooking the structure diagram；
Fig. 6 is simulation of wind of the present invention and the dimensional structure diagram one of spraying system；
Fig. 7 is Fig. 6 main structure diagram；
Fig. 8 is Fig. 6 overlooking the structure diagram；
Fig. 9 is Fig. 8 A-A profile structure diagrams；
Figure 10 is Fig. 9 partial enlargement structural representation；
Figure 11 is simulation of wind of the present invention and the dimensional structure diagram two of spraying system；
Figure 12 is Figure 11 partial enlargement structural representations；
Figure 13 is present invention looks up structural representation of the Rotor mount on mounting platform；
Figure 14 is mounting seat and the dimensional structure diagram of rectangle pipe sleeve；
Figure 15 is the structural representation of many rotor simulation of wind embodiments of the invention.
Embodiment
In order to further find out the technical purpose and technical scheme of the present invention, below in conjunction with the accompanying drawings with specific embodiment to this
Invention is described further.
As shown in Figures 1 to 10, a kind of plant protection unmanned plane sprinkling Two phase flow field lab simulation test platform, including console
4th, analog machine and Pcnten-1 yne-4 detection and wind field detection equipment etc..
The console 4 is arranged on the position of the convenient manipulation of experiment indoor occupant provided with display and input unit, and pacifies in advance
Equipped with corresponding operation software.
The analog machine provided with beam guideway 3, guide rail electric car 1, elevating mechanism 2, simulation of wind and spraying system and
The servo-control system for controlling guide rail electric car 1, elevating mechanism 2, simulation of wind and spraying system 5 to run, the SERVO CONTROL system
System is communicated to connect on guide rail electric car 1 or elevating mechanism 2 by wired or wireless mode with console 4, receives control
Signal and feedback data.
The beam guideway 3 uses I-shaped guide rail, is erected at laboratory in the air.Guide rail electric car 1 is watched using exchange
Motor 1-4 is taken as power source, is slowed down by gear train 1-3 and imparts power to wheel side gear band motor car wheel 1-1 rollings.
The elevating mechanism 2 includes being fixed on stationary platen 2-1 below the car body 1-2 of guide rail electric car 1, installs simulation of wind
With the loading stand 2-3 of the grade device of spraying system 5, and be connected platen 2-1 and loading stand 2-3 scissor type telescopic bar
2-2。
Simulation of wind and the simulation of wind module of spraying system 5 include a pair list rotor 5-1 and rotor motor 5-
9.Single rotor 5-1 is arranged at loading stand 2-3 lower section, and rotor blade is fixed under hollow rotating shaft 5-13 by mounting seat
On the rectangle pipe sleeve 5-20 in portion.The rectangle pipe sleeve 5-20 is enclosed on hollow rotating shaft and is welded and fixed, and its outside is provided with fixed peace
Fill the mounting plane of seat.The mounting seat includes mounting base a 5-17, the mounting base 5-17 provided with two centers pair
The long arc-shaped holes 5-18 of title, as shown in figure 12, and is provided with and the long arc-shaped holes 5-18 stop screws being adapted to or bolt pair 5-19, square
Shape pipe sleeve 5-20 correspondence long arc-shaped holes 5-18 position is provided with circular screwhole or identical long arc-shaped holes；Mounting base 5-17 and square
The medial surface of shape pipe sleeve 5-20 contacts is provided with a rotary middle spindle, and rectangle pipe sleeve 5-20 mounting planes are provided with the insertion rotation
The centre bore of central shaft, the symmetrical centre of the long arc-shaped holes 5-18 falls on the axle center of the rotary middle spindle；Mounting base
5-17 lateral surface is provided with the support of fixed blades.
When rotor is installed, mounting seat and rectangle pipe sleeve 5-20 relative angle (angle that i.e. blade is installed) are adjusted, will
Tightened through long arc-shaped holes 5-18 with the rectangle pipe sleeve 5-20 stop screws being connected or bolt pair 5-19, so as to lock mounting base
5-17 and rectangle pipe sleeve 5-20.
Hollow rotating shaft 5-13 upper ends pass through loading stand 2-3, are fixed on by bearing block 5-12 on platen, the bearing block
5-12 includes pedestal and the rolling bearing in pedestal, and the hollow rotating shaft 5-13 is passed through in the middle of the rolling bearing,
It is connected with the bearing inner race, hollow rotating shaft 5-13 passes through gear 5-8, gear 5-11 and the rotation from the upper end that the bearing stretches out
Wing motor 5-9 power output shaft enters action edge transmission.Cover gear 5-8, gear 5-11 gear cap 5-10 is fixed
On the pedestal of the bearing block 5-12.The lower section of the loading stand 2-3 is also stuck in the angular contact on hollow rotating shaft provided with one
Ball bearing 5-15, hollow rotating shaft 5-13 are passed through in the middle of the bearing, are connected with the bearing inner race, the bearing passes through a bearing sleeve
5-14 is fixed on below loading stand.
The spray module of simulation of wind and spraying system 5 includes medicine-chest 5-2, liquid pump system, spray boom 5-4, some rotary
The hollow pipe sleeve 5-16 of shower nozzle 5-5 and one.The medicine-chest 5-2, liquid pump system are fixed on the loading stand 2-3, and described
Hollow pipe sleeve 5-16 upper end is fixed on the gear cap 5-10 by flange arrangement, and pipe sleeve bottom is from the hollow rotating shaft
5-13 central cavities are through (not contacted with hollow rotating shaft) is stretched out, and two spray boom 5-4 are symmetrically fixedly connected under hollow pipe sleeve 5-16
The left and right sides in portion, the output pipe and rotary nozzle circuit of liquid pump system etc. are passed through from hollow pipe sleeve 5-16, liquid pump
The output pipe of system is connected with spray boom 5-4, decoction is spilt from the shower nozzle 5-5 on spray boom 5-4.The liquid pump system
Including vane pump 5-6, blade pump motor 5-7 and the pressure regulator valve 5-3 being arranged on medicine-chest 5-2 and vane pump 5-6 connecting lines.
A kind of single rotor wing unmanned aerial vehicle for above-mentioned platform sprays Two phase flow field analog detection method, comprises the following steps：
One) start the servo-control system of analog machine by console 4, fall loading stand 2-3 to minimum point, install
Unmanned plane rotor to be measured is to hollow rotating shaft 5-13 connecting portion, and medicine-chest 5-2 additions are given at adjustment shower nozzle 5-5 spacing, inclination angle
Certain density decoction, by console 4 debug shower nozzle 5-5 etc. whether normal operation；
Two) after spray module normal operation, the Pcnten-1 yne-4 test such as relevant position arrangement water sensitive paper, anemobiagraph indoors is used
The equipment arrived；
Three) control interface of operating console 4, rises loading stand 2-3 (or simulation of wind and spraying system) high to specifying
Degree；
Four) rotor motor 5-9 is started, driving rotor 5-1 rotates the rotating speed for reaching and specifying；
Five) drive rail electric car 1 to travel in orbit by console 4, amplifier regulation electricity is controlled by software interface
The travel speed of car, after electric car reaches pre-set velocity, starts spray module, makes shower nozzle 5-5 in the wind field that rotor 5-1 is formed
Complete sprinkling；
Six) data message of the collection of finishing analysis Pcnten-1 yne-4 detection equipment or display, completes simulation and tests, using not
Same tester, can carry out the 1. plant protection unmanned plane wind field test under indoor and outside weather conditions；2. sprinkling system is sprayed
Spill drop in the air and ground spray is distributed, deposition, drift performance are tested；3. two-phase flow sprinkler performance test etc..
A kind of multi-rotor unmanned aerial vehicle for platform as described above sprays Two phase flow field analog detection method, and its feature exists
In comprising the following steps：
One) loading stand 2-3 is fallen to electric in servo-control system by console 4, by hollow stem sleeve pipe 5-16, spray
Bar 5-4 is removed, and multi-rotor unmanned aerial vehicle 6 to be measured is bolted or the mode of nylon rope binding is fixedly connected on rectangle
Pipe sleeve 5-20 lower section, adjusts spacing, the inclination angle of the shower nozzle of multi-rotor unmanned aerial vehicle 6, debugs the spraying system of multi-rotor unmanned aerial vehicle 6；
Two) relevant position arrangement Pcnten-1 yne-4 detection indoors and/or wind field detection equipment；
Three) loading stand 2-3 is risen to specified altitude assignment by console 4；
Four) unmanned plane is started by the remote-control handle of multi-rotor unmanned aerial vehicle 6, its rotor is reached predetermined rotating speed；
Five) drive rail electric car 1 to travel in orbit by console 4, after electric car reaches pre-set velocity, pass through remote control
The spraying system that handle starts multi-rotor unmanned aerial vehicle 6 is sprayed；
Six) information of the detection of finishing analysis Pcnten-1 yne-4 and/or wind field detection equipment collection or display, completes simulation and phase
Close test.
General principle, principal character and the advantages of the present invention of the present invention has been shown and described above.The technology of the industry
Personnel are it should be appreciated that the present invention is not limited to the above embodiments, and the simply explanation described in above-described embodiment and specification is originally
The principle of invention, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible.The present invention
Claimed scope is by appended claims, specification and its equivalent thereof.
Claims (10)
1. a kind of plant protection unmanned plane sprays Two phase flow field lab simulation test platform, it is characterised in that including console (4), mould
Propose the detection of standby and Pcnten-1 yne-4 and/or wind field detection equipment；
The analog machine is provided with the skyborne beam guideway of frame (3), the guide rail electric car (1) along beam guideway (3) movement, suspention
Elevating mechanism (2), simulation of wind and spraying system (5) and control guide rail electric car (1) below guide rail electric car (1), lifting
The servo-control system of mechanism (2), simulation of wind and spraying system (5) operation, the servo-control system passes through wired or nothing
The mode of line is communicated to connect with console (4)；
The elevating mechanism (2) includes expansion link (2-2) and is suspended on the loading stand (2-3) of expansion link (2-2) bottom, institute
State simulation of wind and spraying system (5) is arranged in the loading stand (2-3)；
Simulation of wind and the simulation of wind module of spraying system (5) include rotor (5-1) and rotor motor (5-9), institute
Rotor (5-1) is stated on a hollow rotating shaft (5-13), below loading stand (2-3)；Hollow rotating shaft (5-13) upper end
Through loading stand (2-3), it is connected with the rotor motor (5-9) in loading stand (2-3)；
The spray module of simulation of wind and spraying system (5) includes medicine-chest (5-2), liquid pump system, spray boom (5-4), shower nozzle (5-5)
And a hollow pipe sleeve (5-16), the medicine-chest (5-2), liquid pump system are fixed in the loading stand (2-3), described hollow
The upper end of pipe sleeve (5-16) is fixedly connected with loading stand (2-3), and pipe sleeve bottom is empty in the middle part of the hollow rotating shaft (5-13)
Chamber is through stretching out, and spray boom (5-4) is fixedly connected on hollow pipe sleeve (5-16) bottom, and the output pipe of liquid pump system is from hollow pipe sleeve
Through being connected with spray boom (5-4) in (5-16), decoction is set to be sprayed from the shower nozzle (5-5) on spray boom (5-4).
2. a kind of plant protection unmanned plane sprinkling Two phase flow field lab simulation test platform according to claim 1, its feature exists
In the upper surface of the loading stand (2-3) is provided with the bearing block (5-12) of fixation hollow rotating shaft (5-13), the bearing block
(5-12) includes pedestal and the rolling bearing in pedestal, and the hollow rotating shaft (5-13) is worn in the middle of the rolling bearing
Cross, be connected with the bearing inner race, hollow rotating shaft (5-13) is driven from the upper end that the bearing stretches out by gear and the rotor
The power output shaft of motor (5-9) enters action edge transmission, and the gear cap (5-10) of covering gear is fixed on the bearing block (5-
12) on pedestal, and the upper end of the hollow pipe sleeve (5-16) is then fixed in the gear cap (5-10).
3. its feature of a kind of plant protection unmanned plane sprinkling Two phase flow field lab simulation test platform according to claim 2 exists
In the lower section of the loading stand (2-3) is also provided with the rolling bearing in a fixation hollow rotating shaft (5-13), hollow rotating shaft (5-
13) pass through, be connected with the bearing inner race, the bearing is fixed on loading stand by a bearing sleeve (5-14) in the middle of the bearing
Lower section.
4. a kind of plant protection unmanned plane sprinkling Two phase flow field lab simulation test platform according to claim 1, its feature exists
In the blade of rotor (5-1) is fixed on hollow rotating shaft (5-13) side, the mounting seat, including an installation by mounting seat
Bottom plate (5-17), hollow rotating shaft (5-13) is in mounting plane of the corresponding position provided with connection mounting base (5-17)；The peace
At least two concentric long arc-shaped holes (5-18) are provided with dress bottom plate (5-17), and provided with the limit being adapted to long arc-shaped holes (5-18)
Position screw or bolt pair (5-19), by stop screw or bolt pair (5-19) by the peace of mounting base (5-17) and hollow rotating shaft
Fill plane locking.
5. a kind of plant protection unmanned plane sprinkling Two phase flow field lab simulation test platform according to claim 4, its feature exists
In the bottom of the hollow rotating shaft (5-13) is installed with a rectangle pipe sleeve (5-20), and Rotor mount is fixedly connected on institute
On the mounting plane for stating rectangle pipe sleeve (5-20) the week side of boss.
6. a kind of plant protection unmanned plane sprinkling Two phase flow field lab simulation test platform according to claim 4 or 5, its feature
It is, the joint face of the mounting base (5-17) and hollow rotating shaft (5-13) is provided with a central shaft, and mounting plane is provided with slotting
Enter the centre bore of the central shaft, the center of circle of the long arc-shaped holes (5-18) falls on the axle center of the central shaft.
7. a kind of plant protection unmanned plane sprinkling Two phase flow field lab simulation test according to any claim in claim 1-5 is flat
Platform, it is characterised in that the expansion link (2-2) is the scissor type telescopic mechanism driven using electric cylinder.
8. a kind of plant protection unmanned plane sprinkling Two phase flow field lab simulation test according to any claim in claim 1-5 is flat
Platform, it is characterised in that the shower nozzle is rotating sprinkler.
9. a kind of single rotor wing unmanned aerial vehicle sprinkling Two phase flow field simulation for being used for the platform as described in any claim in claim 1-5 is surveyed
Method for testing, it is characterised in that comprise the following steps：
One) loading stand (2-3) is fallen to electric in servo-control system by console (4), unmanned plane rotation to be measured is installed
The wing, spray module is debugged at the spacing of adjustment shower nozzle (5-5), inclination angle；
Two) relevant position arrangement Pcnten-1 yne-4 detection indoors and/or wind field detection equipment；
Three) loading stand (2-3) is risen to specified altitude assignment by console (4)；
Four) rotor motor (5-9) is started by console (4), rotor (5-1) is rotated up to the rotating speed specified；
Five) drive rail electric car (1) to travel in orbit by console (4), after electric car reaches pre-set velocity, start spraying
Module, makes shower nozzle (5-5) complete sprinkling in the wind field that rotor (5-1) is formed；
Six) information of the detection of finishing analysis Pcnten-1 yne-4 and/or wind field detection equipment collection or display, completes simulation and tests.
10. a kind of multi-rotor unmanned aerial vehicle sprinkling Two phase flow field simulation for being used for the platform as described in any claim in claim 1-5
Method of testing, it is characterised in that comprise the following steps：
One) loading stand (2-3) is fallen to electric in servo-control system by console (4), by hollow bushing (5-16), spray
Bar (5-4) is removed, and multi-rotor unmanned aerial vehicle (6) to be measured is fixedly connected on below loading stand (2-3), adjust many rotors nobody
The spacing of machine (6) shower nozzle, inclination angle, debug multi-rotor unmanned aerial vehicle (6) spraying system；
Two) relevant position arrangement Pcnten-1 yne-4 detection indoors and/or wind field detection equipment；
Three) loading stand (2-3) is risen to specified altitude assignment by console (4)；
Four) unmanned plane is started by the remote-control handle of multi-rotor unmanned aerial vehicle (6), its rotor is reached predetermined rotating speed；
Five) drive rail electric car (1) to travel in orbit by console (4), after electric car reaches pre-set velocity, pass through remote control
The spraying system that handle starts multi-rotor unmanned aerial vehicle (6) is sprayed；
Six) information of the detection of finishing analysis Pcnten-1 yne-4 and/or wind field detection equipment collection or display, completes simulation and tests.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201510051943.1A CN104614150B (en) | 2015-01-30 | 2015-01-30 | Plant protection unmanned plane sprays Two phase flow field lab simulation test platform and method |
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| CN201510051943.1A CN104614150B (en) | 2015-01-30 | 2015-01-30 | Plant protection unmanned plane sprays Two phase flow field lab simulation test platform and method |
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| CN204495540U (en) * | 2015-01-30 | 2015-07-22 | 农业部南京农业机械化研究所 | Plant protection unmanned plane sprays Two phase flow field lab simulation test platform |
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