CN108934661A - A kind of device for administering acid rain using aircraft - Google Patents

A kind of device for administering acid rain using aircraft Download PDF

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Publication number
CN108934661A
CN108934661A CN201810756310.4A CN201810756310A CN108934661A CN 108934661 A CN108934661 A CN 108934661A CN 201810756310 A CN201810756310 A CN 201810756310A CN 108934661 A CN108934661 A CN 108934661A
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China
Prior art keywords
powder
bolt
opened
placement
hole
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Granted
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CN201810756310.4A
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Chinese (zh)
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CN108934661B (en
Inventor
崔艳
董芳
董梓润
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Chaoyang Chuangyida Technology Co ltd
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Shanghai Yan Ge Mechanical And Electrical Technology Co Ltd
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    • A—HUMAN NECESSITIES
    • A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
    • A01G—HORTICULTURE; CULTIVATION OF VEGETABLES, FLOWERS, RICE, FRUIT, VINES, HOPS OR SEAWEED; FORESTRY; WATERING
    • A01G15/00—Devices or methods for influencing weather conditions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
    • B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
    • B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
    • C—CHEMISTRY; METALLURGY
    • C02—TREATMENT OF WATER, WASTE WATER, SEWAGE, OR SLUDGE
    • C02F—TREATMENT OF WATER, WASTE WATER, SEWAGE, OR SLUDGE
    • C02F1/00—Treatment of water, waste water, or sewage
    • C—CHEMISTRY; METALLURGY
    • C02—TREATMENT OF WATER, WASTE WATER, SEWAGE, OR SLUDGE
    • C02F—TREATMENT OF WATER, WASTE WATER, SEWAGE, OR SLUDGE
    • C02F2103/00—Nature of the water, waste water, sewage or sludge to be treated
    • C02F2103/001—Runoff or storm water
    • C—CHEMISTRY; METALLURGY
    • C02—TREATMENT OF WATER, WASTE WATER, SEWAGE, OR SLUDGE
    • C02F—TREATMENT OF WATER, WASTE WATER, SEWAGE, OR SLUDGE
    • C02F2201/00—Apparatus for treatment of water, waste water or sewage
    • C02F2201/008—Mobile apparatus and plants, e.g. mounted on a vehicle
    • C—CHEMISTRY; METALLURGY
    • C02—TREATMENT OF WATER, WASTE WATER, SEWAGE, OR SLUDGE
    • C02F—TREATMENT OF WATER, WASTE WATER, SEWAGE, OR SLUDGE
    • C02F2209/00—Controlling or monitoring parameters in water treatment
    • C02F2209/005—Processes using a programmable logic controller [PLC]

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  • Life Sciences & Earth Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Water Supply & Treatment (AREA)
  • Hydrology & Water Resources (AREA)
  • Environmental & Geological Engineering (AREA)
  • Pest Control & Pesticides (AREA)
  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Atmospheric Sciences (AREA)
  • Environmental Sciences (AREA)
  • Catching Or Destruction (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

本发明公开了一种利用飞机治理酸雨的装置，包括机身，所述利用飞机治理酸雨的装置由粉末存储装置、粉末处理装置、粉末喷洒装置、控制装置共同组成，所述粉末存储装置由粉末存储箱体、进粉口一、盖子、出粉口一、步进电机、治理粉共同组成，所述粉末处理装置由粉末处理箱体、进粉口二、挡板结构、旋转电机、刀片、风扇共同组成，所述粉末喷洒装置由出粉口二、抽风机、喷头共同组成，所述控制装置PLC控制器、按钮开关共同组成。本发明的有益效果是，结构简单，实用性强。

The invention discloses a device for controlling acid rain by using an aircraft, which includes a fuselage. The device for controlling acid rain by using an aircraft is composed of a powder storage device, a powder processing device, a powder spraying device and a control device. The powder storage device is composed of powder The storage box, powder inlet 1, cover, powder outlet 1, stepping motor, and treatment powder are composed together. The powder processing device is composed of powder processing box, powder inlet 2, baffle structure, rotating motor, blade, The fan is composed together, the powder spraying device is composed of the powder outlet 2, the exhaust fan, and the nozzle, and the control device is composed of a PLC controller and a button switch. The invention has the advantages of simple structure and strong practicability.

Description

A kind of device for administering acid rain using aircraft
Technical field
The present invention relates to water treatment field, especially a kind of device that acid rain is administered using aircraft.
Background technique
Acid rain falls in farmland and can impact to crops, and people again eat these grains, and the time has been grown also can be slow Slowly deleterious effect is generated to the body of people, in order to solve this problem, because the invention utilizes the device of aircraft improvement acid rain, The invention will be administered powder using aircraft and is sprayed onto the air, achieve the effect that administer acid rain with reacting for water using powder is administered, PLC control The auto recycling of device realization device processed, stepper motor push one every time and guarantee to cure reason powder, and fan uniformly dispels powder is administered, subtracts It is few as administer powder it is too many caused by waste, exhaust fan is uniformly siphoned away powder is administered, and passes through spray head and rainwater carries out haptoreaction.
Summary of the invention
The purpose of the present invention is to solve the above problems, devise a kind of device that acid rain is administered using aircraft.
Realize above-mentioned purpose the technical scheme is that, a kind of device for administering acid rain using aircraft, including fuselage, institute It states and administers the device of acid rain by passing through the fixed powder storage unit of bolt arrangement one with body bottom surface, being located at powder using aircraft Storage device side and the powder processing being fixedly connected with body bottom surface by bolt arrangement two are located at powder processing Following powder flusher, the control device being fixedly connected in fuselage and with fuselage collectively constitute, the powder storing Device by be fixedly connected with body bottom surface by bolt arrangement one powder storing cabinet, be opened in powder storing top of the box into Powder mouth one, the meal outlet one for being opened in powder storing body side, is opened in powder at the lid being connect by pin shaft structure with powder inlet one Stepper motor putting hole of the end storage body side far from meal outlet one, the stepper motor being inlaid in stepper motor putting hole, Be inlaid in powder storing cabinet and collectively constituted with the packs of improvement powder that thin paper wraps up, the powder processing by with machine It is powder-processed cabinet that body underrun bolt arrangement two is fixedly connected, the powder inlet two for being opened in powder-processed body side, embedding Baffle arrangement in powder inlet two, is inlaid in rotating electric machine at the rotating electric machine placing groove for being opened in powder-processed top of the box In placing groove and rotating electric machine that round end is downward, the blade being connect by bearing with rotating electric machine round end, it is opened at powder The fan placing groove for managing top of the box, the fan being inlaid in fan placing groove collectively constitute, and the powder flusher is by opening The meal outlet two that is connected to fuselage in the powder-processed bottom of box, the exhaust fan being connect by helicitic texture one with meal outlet two, It is collectively constituted with exhaust fan by the spray head that helicitic texture two is connect, the control device is by being opened in the cockpit in fuselage PLC controller placing groove on control panel, the PLC for being inlaid in PLC controller placing groove and being electrically connected with control panel Controller, open button switch placing groove on the control panel, be inlaid in button switch placing groove in and with control panel electrical property The button switch of connection collectively constitutes.
The bolt arrangement one by be opened in the bolt putting hole of powder storing tank floor, attack in bolt putting hole and with The screw thread of bolt cooperation, be opened in the bolt hole that body bottom surface and bolt putting hole match collectively constitute, the spiral shell attacked in bolt hole Bolt between line, connection bolt putting hole and bolt hole collectively constitutes.
The bolt arrangement two by be opened in the bolt putting hole of powder-processed tank floor, attack in bolt putting hole and with The screw thread of bolt cooperation, be opened in the bolt hole that body bottom surface and bolt putting hole match collectively constitute, the spiral shell attacked in bolt hole Bolt between line, connection bolt putting hole and bolt hole collectively constitutes.
The baffle arrangement is by the baffle placing groove being opened in powder inlet two, the baffle being inlaid in baffle placing groove, company Delay switch structure between logical baffle placing groove and baffle collectively constitutes.
Delay switch structure by be fixedly connected with delay switch close to baffle one end electromagnet one, be opened in baffle close to prolonging Two placing groove of electromagnet of the one end Shi Kaiguan, the electromagnet two being inlaid in two placing groove of electromagnet collectively constitute.
The meal outlet one is inserted with powder inlet two by smooth circular pipe communicated, the smooth round tube and meal outlet one One end be higher than one end for inserting with powder inlet two.
The blade is overlapped with the center line of powder inlet two.
The pin shaft structure is by being opened in the pin shaft fixation hole of powder inlet one and cap contacts one end, being opened in lid and powder inlet The pin shaft putting hole of one contact one end, the pin shaft being connected between pin shaft fixation hole and pin shaft putting hole collectively constitute, the screw thread Structure one is in contact one end by attacking in meal outlet two external screw thread of the one end that is in contact with exhaust fan, attacking in exhaust fan with meal outlet two Internal screw thread collectively constitute, the helicitic texture two is by attacking in spray head the internal screw thread of the one end that is in contact with exhaust fan, attacking in exhausting Be in contact with the spray head external screw thread of one end of machine collectively constitutes.
It is provided with alarm placing groove in the powder storing cabinet, is embedded with alarm, institute in the alarm placing groove It states alarm and stepper motor is electrically connected.
The PLC controller input terminal is electrically connected with button switch, the PLC controller and stepper motor electrically connect It connects, the PLC controller and rotating electric machine are electrically connected, and the PLC controller and fan are electrically connected, the PLC controller It is electrically connected with exhaust fan, the PLC controller and delay switch are electrically connected, and the PLC controller electrically connects with alarm It connects.
Using the device for administering acid rain using aircraft of technical solution of the present invention production, powder will be administered using aircraft and will be sprayed To aerial, achieve the effect that improvement acid rain, the automatic cycle of PLC controller realization device make with react for water using powder is administered Push one every time with, stepper motor and guarantee to cure reason powder, fan is uniformly dispelled powder is administered, reduce as administer powder it is too many caused by wave Take, exhaust fan is uniformly siphoned away powder is administered, and carries out haptoreaction by spray head and rainwater.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the device of the present invention that acid rain is administered using aircraft；
Fig. 2 is one structural schematic diagram of bolt arrangement of the device of the present invention that acid rain is administered using aircraft；
Fig. 3 is two structural schematic diagram of bolt arrangement of the device of the present invention that acid rain is administered using aircraft；
Fig. 4 is the structural schematic diagram of the baffle arrangement of the device of the present invention that acid rain is administered using aircraft；
Fig. 5 is the structural schematic diagram of the pin shaft structure of the device of the present invention that acid rain is administered using aircraft；
Fig. 6 is one structural schematic diagram of helicitic texture of the device of the present invention that acid rain is administered using aircraft；
Fig. 7 is two structural schematic diagram of helicitic texture of the device of the present invention that acid rain is administered using aircraft；
Fig. 8 is the control panel structural schematic diagram of the device of the present invention that acid rain is administered using aircraft；
In figure, 1, fuselage；2, bolt arrangement one；3, bolt arrangement two；4, powder storing cabinet；5, powder inlet one；6, it sells Axle construction；7, lid；8, meal outlet one；9, PLC controller input terminal；10, stepper motor putting hole；11, stepper motor；12, Administer powder；13, powder-processed cabinet；14, powder inlet two；15, baffle arrangement；16, rotating electric machine placing groove；17, rotating electric machine； 18, bearing；19, blade；20, fan placing groove；21, fan；22, meal outlet two；23, helicitic texture one；24, exhaust fan；25, Helicitic texture two；26, spray head；27, cockpit；28, control panel；29, PLC controller placing groove；30, PLC controller；31, Button switch placing groove；32, button switch；33, bolt putting hole；34, bolt；35, screw thread；36, bolt hole；37, baffle is put Set slot；38, baffle；39, delay switch structure；40, delay switch；41, electromagnet one；42, two placing groove of electromagnet；43, electric Magnet two；44, round tube；45, pin shaft fixation hole；46, pin shaft putting hole；47, pin shaft；48, external screw thread；49, internal screw thread；50, it reports Alert device placing groove；51, alarm.
Specific embodiment
The present invention is specifically described with reference to the accompanying drawing, as shown in figures 1-8, a kind of dress for administering acid rain using aircraft Set, including fuselage 1, which is characterized in that it is described using aircraft administer acid rain device by with 1 underrun bolt arrangement one of fuselage 2 fixed powder storage units are fixedly connected positioned at powder storage unit side and with 1 underrun bolt arrangement 23 of fuselage Powder processing, the powder flusher below powder processing, be located in fuselage 1 and with fuselage 1 is fixed connects The control device connect collectively constitutes, and the powder storage unit is by the powder that is fixedly connected with 1 underrun bolt arrangement 1 of fuselage End storage cabinet 4, the powder inlet 1 for being opened in 4 top of powder storing cabinet pass through the lid that pin shaft structure 6 is connect with powder inlet 1 Son 7, is opened in stepping of 4 side of powder storing cabinet far from meal outlet 1 at the meal outlet 1 for being opened in 4 side of powder storing cabinet Motor putting hole 10, is inlaid in powder storing cabinet 4 and uses thin paper the stepper motor 11 being inlaid in stepper motor putting hole 10 The packs of improvement powder 12 of package collectively constitute, and the powder processing with 1 underrun bolt arrangement 23 of fuselage by consolidating Surely the powder-processed cabinet 13 that connects, is inlaid in powder inlet 2 14 powder inlet 2 14 for being opened in 13 side of powder-processed cabinet Baffle arrangement 15, be opened in the top of powder-processed cabinet 13 rotating electric machine placing groove 16, be inlaid in rotating electric machine placing groove 16 Interior and downward round end rotating electric machine 17, is opened in powder at the blade 19 being connect by bearing 18 with 17 round end of rotating electric machine The fan placing groove 20 at 13 top of processing cabinet, the fan 21 being inlaid in fan placing groove 20 collectively constitute, the powder spray Device is spilt by being opened in meal outlet 2 22 that 13 bottom of powder-processed cabinet is connected to fuselage 1, passing through screw thread knot with meal outlet 2 22 The exhaust fan 24 of the connection of structure 1 is collectively constituted with exhaust fan 24 by the spray head 26 that helicitic texture 2 25 is connect, the control Device by the control panel 28 in the cockpit 27 that is opened in fuselage 1 PLC controller placing groove 29, be inlaid in PLC control The PLC controller 30 being electrically connected in device placing groove 29 and with control panel 28, the button switch being opened on control panel 28 are put The button switch 32 being electrically connected in setting slot 31, being inlaid in button switch placing groove 31 and with control panel 28 collectively constitutes；Institute Bolt arrangement 1 is stated by being opened in the bolt putting hole 33 of 4 bottom surface of powder storing cabinet, attacking in bolt putting hole 33 and and bolt The screw thread 35 of 34 cooperations is opened in the bolt hole 36 that 1 bottom surface of fuselage and bolt putting hole 33 match and collectively constitutes, attacks in bolt hole 36 Bolt 34 between interior screw thread 35, connection bolt putting hole 33 and bolt hole 36 collectively constitutes；The bolt arrangement 23 is by opening 13 bottom surface of powder-processed cabinet bolt putting hole 33, attack in bolt putting hole 33 and cooperate with bolt 34 screw thread 35, It is opened in 1 bottom surface of fuselage and collectively constitutes, the screw thread 35 attacked in bolt hole 36, is connected to the bolt hole 36 that bolt putting hole 33 matches Bolt 34 between bolt putting hole 33 and bolt hole 36 collectively constitutes；The baffle arrangement 15 is by being opened in powder inlet 2 14 Delay between baffle placing groove 37, the baffle 38 being inlaid in baffle placing groove 37, connection baffle placing groove 37 and baffle 38 Construction of switch 39 collectively constitutes；Delay switch structure 39 is by the electromagnet that is fixedly connected with delay switch 40 close to 38 one end of baffle One 41, be opened in baffle 38 close to 40 one end of delay switch two placing groove 42 of electromagnet, be inlaid in two placing groove 42 of electromagnet Electromagnet 2 43 collectively constitute；The meal outlet 1 is connected to powder inlet 2 14 by smooth round tube 44, described smooth One end that round tube 44 and meal outlet 1 insert is higher than the one end inserted with powder inlet 2 14；The blade 19 and powder inlet 2 14 Center line be overlapped；The pin shaft structure 6 contacts the pin shaft fixation hole 45 of one end by being opened in powder inlet 1 and lid 7, is opened in lid Son 7 contacts the pin shaft putting hole 46 of one end, the pin shaft being connected between pin shaft fixation hole 45 and pin shaft putting hole 46 with powder inlet 1 47 collectively constitute, and the helicitic texture 1 is by attacking in meal outlet 2 22 external screw thread 48 of the one end that is in contact with exhaust fan 24, attacking It is collectively constituted in be in contact with meal outlet 2 22 internal screw thread 49 of one end of exhaust fan 24, the helicitic texture two is by attacking in spray head 26 Be in contact with exhaust fan 24 one end internal screw thread 49, attack in exhaust fan 24 48 common groups of external screw thread of the one end that is in contact with spray head 26 At；, it is provided with alarm placing groove 50 in the powder storing cabinet 4, is embedded with alarm 51 in the alarm placing groove 50, The alarm 51 is electrically connected with stepper motor 11；The PLC controller input terminal 9 and the electric connection of button switch 32, institute It states PLC controller 30 and stepper motor 11 is electrically connected, the PLC controller 30 is electrically connected with rotating electric machine 17, the PLC Controller 30 and fan 21 are electrically connected, and the PLC controller 30 is electrically connected with exhaust fan 24, the PLC controller 30 with Delay switch 40 is electrically connected, and the PLC controller 30 is electrically connected with alarm 51.
The characteristics of the present embodiment is to administer the device of acid rain by consolidating with body bottom surface by bolt arrangement one using aircraft Fixed powder storage unit passes through the powder that bolt arrangement two is fixedly connected positioned at powder storage unit side and with body bottom surface Processing unit, the powder flusher below powder processing, the control being fixedly connected in fuselage and with fuselage Device collectively constitutes, powder storage unit by be fixedly connected with body bottom surface by bolt arrangement one powder storing cabinet, open In the powder inlet one of powder storing top of the box, the lid being connect by pin shaft structure with powder inlet one, it is opened in powder storing case The meal outlet one of body side surface is opened in stepper motor putting hole of the powder storing body side far from meal outlet one, is inlaid in stepping Stepper motor in motor putting hole is inlaid in common group of packs of improvement powder wrapped up in powder storing cabinet with thin paper At, powder processing by be fixedly connected with body bottom surface by bolt arrangement two powder-processed cabinet, be opened in powder-processed The powder inlet two of body side, the baffle arrangement being inlaid in powder inlet two, the rotating electric machine for being opened in powder-processed top of the box Placing groove is inlaid in rotating electric machine placing groove and rotating electric machine that round end is downward, with rotating electric machine round end passes through bearing The blade of connection, the fan placing groove for being opened in powder-processed top of the box, the fan being inlaid in fan placing groove collectively constitute, Powder flusher is by being opened in meal outlet two that the powder-processed bottom of box is connected to fuselage, passing through helicitic texture with meal outlet two The exhaust fan of one connection is collectively constituted with exhaust fan by the spray head that helicitic texture two is connect, and control device is by being opened in fuselage Cockpit in control panel on PLC controller placing groove, be inlaid in PLC controller placing groove and with control panel electricity Property connection PLC controller, open button switch placing groove on the control panel, be inlaid in button switch placing groove in and with control The button switch that panel processed is electrically connected collectively constitutes, and will administer powder using aircraft and be sprayed onto the air, and utilize improvement powder and water Reaction achievees the effect that improvement acid rain, the auto recycling of PLC controller realization device, stepper motor push one every time and guarantees to cure Manage powder, fan by administer powder uniformly dispel, reduce as administer powder it is too many caused by waste, exhaust fan by administer powder uniformly inhale It walks, haptoreaction is carried out by spray head and rainwater.
In the present embodiment, press button switch, PLC controller obtain it is electric, by the program finished in PLC controller into Row automation control, stepper motor start-up operation stepper motor wrap first in the Bao Baozhili powder in powder storing cabinet It is pushed into round tube, is slid into powder-processed cabinet in the improvement powder that acts on of gravity along round tube, delay switch is in stepping electricity Start timing after motor-driven work, by calculating the time administered powder and reach powder inlet two, to set the time of delay switch, setting Time is more slightly longer than the time for administering powder arrival powder inlet two, after delay switch movement, two power loss of electromagnet one and electromagnet, and electromagnetism Iron one is separated with electromagnet two, flapper closure, and rotating electric machine starts to act after a period of work in stepper motor, electric rotating Machine stops rotating after delay switch movement, and fan is started to work after delay switch movement, drive of the blade in rotating electric machine Under, the thin paper wrapped up outside powder will be administered and scratched, fan is dispelled powder is administered, and the improvement powder dispelled is aspirated through spray head by exhaust fan It sprays out, improvement powder and the rainwater in air sprayed out reacts, and plays the function of administering acid rain, calculates completion The time that primary sprinkling needs, the time of stepper motor operation is controlled by PLC controller, after stepper motor all stretches out, Alarm sounds, and presses button switch, and device is out of service, and staff opens the lid in powder storing cabinet a packet Improvement powder be put into powder storing cabinet, then press button switch, restart device.
Above-mentioned technical proposal only embodies the optimal technical scheme of technical solution of the present invention, those skilled in the art The principle of the present invention is embodied to some variations that some of them part may be made, belongs to the scope of protection of the present invention it It is interior.

Claims (10)

1.一种利用飞机治理酸雨的装置，包括机身(1)，其特征在于，所述利用飞机治理酸雨的装置由与机身(1)底面通过螺栓结构一(2)固定的粉末存储装置、位于粉末存储装置侧面且与机身(1)底面通过螺栓结构二(3)固定连接的粉末处理装置、位于粉末处理装置下面的粉末喷洒装置、位于机身(1)内且与机身(1)固定连接的控制装置共同组成，所述粉末存储装置由与机身(1)底面通过螺栓结构一(2)固定连接的粉末存储箱体(4)、开在粉末存储箱体(4)顶部的进粉口一(5)、与进粉口一(5)通过销轴结构(6)连接的盖子(7)、开在粉末存储箱体(4)侧面的出粉口一(8)、开在粉末存储箱体(4)侧面远离出粉口一(8)的步进电机放置孔(10)、嵌装在步进电机放置孔(10)内的步进电机(11)、嵌装在粉末存储箱体(4)内用薄纸包裹的一包包的治理粉(12)共同组成，所述粉末处理装置由与机身(1)底面通过螺栓结构二(3)固定连接的粉末处理箱体(13)、开在粉末处理箱体(13)侧面的进粉口二(14)、嵌装在进粉口二(14)内的挡板结构(15)、开在粉末处理箱体(13)顶部的旋转电机放置槽(16)、嵌装在旋转电机放置槽(16)内且旋转端向下的旋转电机(17)、与旋转电机(17)旋转端通过轴承(18)连接的刀片(19)、开在粉末处理箱体(13)顶部的风扇放置槽(20)、嵌装在风扇放置槽(20)内的风扇(21)共同组成，所述粉末喷洒装置由开在粉末处理箱体(13)底部与机身(1)连通的出粉口二(22)、与出粉口二(22)通过螺纹结构一(23)连接的抽风机(24)、与抽风机(24)通过螺纹结构二(25)连接的喷头(26)共同组成，所述控制装置由开在机身(1)内的驾驶舱(27)里的控制面板(28)上的PLC控制器放置槽(29)、嵌装在PLC控制器放置槽(29)内且与控制面板(28)电性连接的PLC控制器(30)、开在控制面板(28)上的按钮开关放置槽(31)、嵌装在按钮开关放置槽(31)内且与控制面板(28)电性连接的按钮开关(32)共同组成。1. a device utilizing aircraft to control acid rain, comprising a fuselage (1), characterized in that, the device utilizing an aircraft to control acid rain is fixed by a powder storage device with the fuselage (1) bottom surface by bolt structure one (2) , a powder processing device located on the side of the powder storage device and fixedly connected to the bottom surface of the fuselage (1) through bolt structure 2 (3), a powder spraying device located below the powder processing device, located in the fuselage (1) and connected to the fuselage ( 1) The control devices that are fixedly connected are composed together, and the powder storage device is composed of a powder storage box (4) fixedly connected to the bottom surface of the fuselage (1) through a bolt structure (2), and a powder storage box (4) opened on the powder storage box (4) Powder inlet 1 (5) on the top, cover (7) connected to powder inlet 1 (5) through a pin structure (6), powder outlet 1 (8) opened on the side of the powder storage box (4) , the stepper motor placement hole (10) opened on the side of the powder storage box (4) away from the powder outlet one (8), the stepper motor (11) embedded in the stepper motor placement hole (10), the embedded Packed in a powder storage box (4) and wrapped in a bag of treatment powder (12) with thin paper, the powder treatment device is fixedly connected to the bottom surface of the fuselage (1) through a bolt structure two (3). The powder processing box (13), the powder inlet two (14) opened on the side of the powder treatment box (13), the baffle structure (15) embedded in the powder inlet two (14), opened in the powder treatment The rotary motor placement slot (16) on the top of the box (13), the rotary motor (17) embedded in the rotary motor placement slot (16) with the rotary end downward, and the rotary motor (17) rotary end through the bearing (18 ) connected to the blade (19), the fan placement slot (20) opened on the top of the powder processing box (13), and the fan (21) embedded in the fan placement slot (20) are composed together, and the powder spraying device consists of Open the powder outlet two (22) connected to the fuselage (1) at the bottom of the powder processing box (13), the exhaust fan (24) connected with the powder outlet two (22) through the thread structure one (23), and the Blower fan (24) is jointly formed by the nozzle (26) that thread structure two (25) connects, and described control device is opened by the PLC on the control panel (28) in the cockpit (27) in fuselage (1) The controller placement slot (29), the PLC controller (30) embedded in the PLC controller placement slot (29) and electrically connected to the control panel (28), the button switch placed on the control panel (28) The groove (31) and the button switch (32) embedded in the button switch placement groove (31) and electrically connected with the control panel (28) are jointly composed. 2.根据权利要求1所述的一种利用飞机治理酸雨的装置，其特征在于，所述螺栓结构一(2)由开在粉末存储箱体(4)底面的螺栓放置孔(33)、攻在螺栓放置孔(33)内且与螺栓(34)配合的螺纹(35)、开在机身(1)底面与螺栓放置孔(33)相配的螺栓孔(36)共同组成、攻在螺栓孔(36)内的螺纹(35)、连通螺栓放置孔(33)和螺栓孔(36)之间的螺栓(34)共同组成。2. a kind of device utilizing aircraft to control acid rain according to claim 1, is characterized in that, described bolt structure one (2) is made of the bolt placement hole (33) that is opened in powder storage box (4) bottom surface, taps In the bolt placement hole (33) and the screw thread (35) that cooperates with the bolt (34), the bolt hole (36) that is opened on the bottom surface of the fuselage (1) and the bolt placement hole (33) matches to form together, tap the bolt hole The screw thread (35) in (36), the bolt (34) between the connecting bolt placement hole (33) and the bolt hole (36) is jointly formed. 3.根据权利要求1所述的一种利用飞机治理酸雨的装置，其特征在于，所述螺栓结构二(3)由开在粉末处理箱体(13)底面的螺栓放置孔(33)、攻在螺栓放置孔(33)内且与螺栓(34)配合的螺纹(35)、开在机身(1)底面与螺栓放置孔(33)相配的螺栓孔(36)共同组成、攻在螺栓孔(36)内的螺纹(35)、连通螺栓放置孔(33)和螺栓孔(36)之间的螺栓(34)共同组成。3. a kind of device that utilizes aircraft to control acid rain according to claim 1, is characterized in that, described bolt structure two (3) is made of the bolt placement hole (33) that is opened on the powder treatment casing (13) bottom surface, taps In the bolt placement hole (33) and the screw thread (35) that cooperates with the bolt (34), the bolt hole (36) that is opened on the bottom surface of the fuselage (1) and the bolt placement hole (33) matches to form together, tap the bolt hole The screw thread (35) in (36), the bolt (34) between the connecting bolt placement hole (33) and the bolt hole (36) is jointly formed. 4.根据权利要求1所述的一种利用飞机治理酸雨的装置，其特征在于，所述挡板结构(15)由开在进粉口二(14)内的挡板放置槽(37)、嵌装在挡板放置槽(37)内的挡板(38)、连通挡板放置槽(37)和挡板(38)之间的延时开关结构(39)共同组成。4. a kind of device utilizing aircraft to control acid rain according to claim 1, is characterized in that, described baffle plate structure (15) is made of the baffle plate placement groove (37) that opens in powder inlet two (14), The baffle plate (38) embedded in the baffle plate placement groove (37), and the delay switch structure (39) between the baffle plate placement groove (37) and the baffle plate (38) are jointly formed. 5.根据权利要求4所述的一种利用飞机治理酸雨的装置，其特征在于，延时开关结构(39)由与延时开关(40)靠近挡板(38)一端固定连接的电磁铁一(41)、开在挡板(38)靠近延时开关(40)一端的电磁铁二放置槽(42)、嵌装在电磁铁二放置槽(42)内的电磁铁二(43)共同组成。5. a kind of device utilizing aircraft to control acid rain according to claim 4, is characterized in that, delay switch structure (39) is by the electromagnet that is fixedly connected with delay switch (40) near baffle plate (38) one end (41), the electromagnet two placement groove (42) that is opened in baffle plate (38) near delay switch (40) one end, the electromagnet two (43) embedded in the electromagnet second placement groove (42) are formed jointly . 6.根据权利要求1所述的一种利用飞机治理酸雨的装置，其特征在于，所述出粉口一(8)与进粉口二(14)通过光滑的圆管(44)连通，所述光滑的圆管(44)与出粉口一(8)插装的一端高于与进粉口二(14)插装的一端。6. a kind of device utilizing aircraft to control acid rain according to claim 1, is characterized in that, described powder outlet one (8) is communicated with powder inlet two (14) by smooth round pipe (44), so The end of the smooth circular pipe (44) and powder outlet one (8) plugged in is higher than the end plugged in with powder inlet two (14). 7.根据权利要求1所述的一种利用飞机治理酸雨的装置，其特征在于，所述刀片(19)与进粉口二(14)的中心线重合。7. A kind of device utilizing airplane to control acid rain according to claim 1, is characterized in that, described blade (19) coincides with the centerline of powder inlet two (14). 8.根据权利要求1所述的一种利用飞机治理酸雨的装置，其特征在于，所述销轴结构(6)由开在进粉口一(5)与盖子(7)接触一端的销轴固定孔(45)、开在盖子(7)与进粉口一(5)接触一端的销轴放置孔(46)、连通销轴固定孔(45)与销轴放置孔(46)之间的销轴(47)共同组成，所述螺纹结构一(23)由攻在出粉口二(22)与抽风机(24)相接触一端的外螺纹(48)、攻在抽风机(24)与出粉口二(22)相接触一端的内螺纹(49)共同组成，所述螺纹结构二由攻在喷头(26)与抽风机(24)相接触一端的内螺纹(49)、攻在抽风机(24)与喷头(26)相接触一端的外螺纹(48)共同组成。8. A kind of device utilizing aircraft to control acid rain according to claim 1, characterized in that, said pin structure (6) consists of a pin that is opened at one end of powder inlet one (5) and cover (7) contact Fixing hole (45), the pin placement hole (46) that is opened at cover (7) and powder inlet one (5) contact end, communicates between the pin fixing hole (45) and the pin placement hole (46) Bearing pin (47) forms jointly, and described thread structure one (23) is tapped at the external thread (48) of one end that powder outlet two (22) contacts with exhaust fan (24), taps at exhaust fan (24) and exhaust fan (24) and The internal thread (49) at the contacting end of the powder outlet two (22) is jointly formed. Machine (24) forms jointly with the external thread (48) of one end that shower nozzle (26) contacts. 9.根据权利要求1所述的一种利用飞机治理酸雨的装置，其特征在于，所述粉末存储箱体(4)内开有报警器放置槽(50)，所述报警器放置槽(50)内嵌装有报警器(51)，所述报警器(51)与步进电机(11)电性连接。9. A kind of device utilizing aircraft to control acid rain according to claim 1, characterized in that, an alarm placement groove (50) is arranged in the powder storage box (4), and the alarm placement groove (50) ) is embedded with an alarm (51), and the alarm (51) is electrically connected with the stepper motor (11). 10.根据权利要求1所述的一种利用飞机治理酸雨的装置，其特征在于，所述PLC控制器输入端(9)与按钮开关(32)电性连接、所述PLC控制器(30)与步进电机(11)电性连接，所述PLC控制器(30)与旋转电机(17)电性连接，所述PLC控制器(30)与风扇(21)电性连接，所述PLC控制器(30)与抽风机(24)电性连接，所述PLC控制器(30)与延时开关(40)电性连接，所述PLC控制器(30)与报警器(51)电性连接。10. a kind of device utilizing aircraft to control acid rain according to claim 1, is characterized in that, described PLC controller input terminal (9) is electrically connected with button switch (32), and described PLC controller (30) It is electrically connected with the stepper motor (11), the PLC controller (30) is electrically connected with the rotating motor (17), the PLC controller (30) is electrically connected with the fan (21), and the PLC control The device (30) is electrically connected with the exhaust fan (24), the PLC controller (30) is electrically connected with the delay switch (40), and the PLC controller (30) is electrically connected with the alarm (51) .
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