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

Abstract

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 device for controlling acid rain by using aircraft

technical field

The invention relates to the field of water treatment, in particular to a device for controlling acid rain by using aircraft.

Background technique

Acid rain falling on the farmland will affect the crops. If people eat these grains, it will gradually have a bad effect on the human body after a long time. In order to solve this problem, we invented the method of using airplanes to control acid rain The invention uses an airplane to spray the treatment powder into the air, and uses the reaction between the treatment powder and water to achieve the effect of controlling acid rain. The PLC controller realizes the automatic recycling of the device. The stepping motor pushes a pack of treatment powder each time, and the fan will control the acid rain. The powder is evenly blown away to reduce the waste caused by too much treatment powder. The exhaust fan sucks the treatment powder evenly, and reacts with the rainwater through the nozzle.

Contents of the invention

The purpose of the present invention is in order to solve the problems referred to above, has designed a kind of device utilizing aircraft to control acid rain.

Achieving the above-mentioned purpose The technical scheme of the present invention is, a kind of device that utilizes aircraft to control acid rain, comprises fuselage, and described device that utilizes aircraft to control acid rain consists of a powder storage device that is fixed to the bottom surface of the fuselage through a bolt structure, and is located in the powder storage device. The powder processing device on the side and fixedly connected to the bottom surface of the fuselage through bolt structure two, the powder spraying device located under the powder processing device, and the control device located in the fuselage and fixedly connected to the fuselage are composed of the powder storage device. The bottom surface of the fuselage is fixedly connected to the powder storage box through the bolt structure, the powder inlet opened on the top of the powder storage box, the cover connected to the powder inlet through the pin shaft structure, and the outlet opened on the side of the powder storage box. Powder port 1, a stepper motor placement hole opened on the side of the powder storage box away from powder outlet 1, a stepper motor embedded in the stepper motor placement hole, a stepper motor embedded in the powder storage box wrapped with tissue paper The treatment powder of the bag is composed together. The powder processing device is composed of a powder processing box fixedly connected to the bottom surface of the fuselage through a bolt structure 2, a powder inlet 2 opened on the side of the powder processing box, and embedded in the powder inlet 2. The internal baffle structure, the rotating motor placement slot opened on the top of the powder processing box, the rotating motor embedded in the rotating motor placement slot with the rotating end facing down, the blade connected to the rotating end of the rotating motor through bearings, and the The fan placement slot on the top of the processing box and the fan embedded in the fan placement slot are composed together. The powder spraying device is composed of the powder outlet 2 opened at the bottom of the powder processing box and communicated with the fuselage, and the powder outlet 2 passes through. The exhaust fan connected with thread structure 1 and the nozzle connected with the exhaust fan through thread structure 2 are jointly composed. The control device is composed of a PLC controller placement slot on the control panel in the cockpit in the fuselage, embedded in the PLC The controller is placed in the slot and is electrically connected to the control panel. The PLC controller is composed of the button switch slot opened on the control panel and the button switch embedded in the button switch slot and electrically connected to the control panel.

The bolt structure is composed of a bolt placement hole opened on the bottom surface of the powder storage box, a screw thread tapped in the bolt placement hole and matched with the bolt, a bolt hole opened on the bottom surface of the fuselage to match the bolt placement hole, and tapped on the bolt placement hole. Threads in holes, connecting bolt placement holes, and bolts between bolt holes.

The second bolt structure consists of bolt placement holes opened on the bottom surface of the powder processing box, threads tapped in the bolt placement holes and matched with the bolts, bolt holes opened on the bottom surface of the fuselage to match the bolt placement holes, and tapped on the bolt placement holes. Threads in holes, connecting bolt placement holes, and bolts between bolt holes.

The baffle structure is composed of a baffle placement groove opened in the second powder inlet, a baffle embedded in the baffle placement groove, and a delay switch structure connecting the baffle placement groove and the baffle.

The delay switch structure is composed of the electromagnet one fixedly connected to the end of the delay switch near the baffle, the electromagnet two placement slot opened on the end of the baffle near the delay switch, and the electromagnet two embedded in the electromagnet two placement slot. composition.

The first powder outlet is connected to the second powder inlet through a smooth round tube, and the end of the smooth round tube inserted into the first powder outlet is higher than the end inserted into the second powder inlet.

The blade coincides with the centerline of the second powder inlet.

The pin structure consists of a pin fixing hole opened at the end of the powder inlet that is in contact with the cover, a pin placement hole opened at the end of the cover that is in contact with the powder inlet, and a connection between the pin fixing hole and the pin placement hole. The pin shafts are formed together, the thread structure one is composed of the external thread tapped at the end of the powder outlet two in contact with the exhaust fan, and the internal thread tapped at the end of the exhaust fan and the powder outlet two contacted together, the thread structure The second is composed of tapping the internal thread at the end where the nozzle and the exhaust fan are in contact, and tapping the external thread at the end where the exhaust fan is in contact with the nozzle.

An alarm placement groove is opened in the powder storage box, and an alarm is embedded in the alarm placement groove, and the alarm is electrically connected to the stepping motor.

The input end of the PLC controller is electrically connected to the button switch, the PLC controller is electrically connected to the stepping motor, the PLC controller is electrically connected to the rotating motor, and the PLC controller is electrically connected to the fan. The PLC controller is electrically connected to the exhaust fan, the PLC controller is electrically connected to the delay switch, and the PLC controller is electrically connected to the alarm.

Utilize the device that utilizes aircraft to control acid rain that the technical scheme of the present invention is made, utilize aircraft to spray control powder into the air, utilize the reaction of control powder and water to achieve the effect of controlling acid rain, PLC controller realizes automatic recycling of the device, stepping motor Each time a pack of treatment powder is pushed, the fan will evenly disperse the treatment powder, reducing the waste caused by too much treatment powder.

Description of drawings

Fig. 1 is the structural representation of the device utilizing aircraft to control acid rain according to the present invention;

Fig. 2 is a bolt structure-structural schematic diagram of the device utilizing aircraft to control acid rain according to the present invention;

Fig. 3 is the bolt structure two structural representations of the device utilizing aircraft to control acid rain according to the present invention;

Fig. 4 is the structural representation of the baffle structure of the device utilizing aircraft to control acid rain according to the present invention;

Fig. 5 is the structural representation of the pin shaft structure of the device utilizing aircraft to control acid rain according to the present invention;

Fig. 6 is the thread structure-structural schematic diagram of the device utilizing aircraft to control acid rain according to the present invention;

Fig. 7 is the screw thread structure two structural representations of the device utilizing aircraft to control acid rain according to the present invention;

Fig. 8 is the structural representation of the control panel of the device utilizing aircraft to control acid rain according to the present invention;

In the figure, 1. Fuselage; 2. Bolt structure 1; 3. Bolt structure 2; 4. Powder storage box; 5. Powder inlet 1; 6. Pin structure; 7. Cover; 8. Powder outlet 1 ;9, PLC controller input end; 10, stepping motor placement hole; 11, stepping motor; 12, treatment powder; 13, powder processing box; 14, powder inlet two; 17. Rotating motor; 18. Bearing; 19. Blade; 20. Fan placement slot; 21. Fan; 22. Two powder outlets; 23. Thread structure one; 24. Exhaust fan; 25. Thread structure Two; 26. Nozzle; 27. Cockpit; 28. Control panel; 29. PLC controller placement slot; 30. PLC controller; 31. Button switch placement slot; 32. Button switch; 33. Bolt placement hole; 34. Bolt; 35, thread; 36, bolt hole; 37, baffle plate placement slot; 38, baffle plate; 39, delay switch structure; 40, delay switch; 41, electromagnet one; 42, electromagnet two placement slot; 43. Electromagnet 2; 44. Round tube; 45. Pin shaft fixing hole; 46. Pin shaft placement hole; 47. Pin shaft; 48. External thread; 49. Internal thread; 50. Alarm placement slot; 51. Alarm device.

Detailed ways

Below in conjunction with accompanying drawing, the present invention is specifically described, as shown in Figure 1-8, a kind of device that utilizes aircraft to control acid rain, comprises fuselage 1, it is characterized in that, described device that utilizes aircraft to control acid rain is formed with fuselage 1 bottom surface The powder storage device fixed by bolt structure one 2, the powder processing device located on the side of the powder storage device and fixedly connected to the bottom surface of the fuselage 1 by bolt structure two 3, the powder spraying device located below the powder processing device, located in the fuselage 1 and The control device fixedly connected with the fuselage 1 is jointly composed of a powder storage box 4 fixedly connected with the bottom surface of the fuselage 1 through a bolt structure 2, and a powder inlet 1 opened on the top of the powder storage box 4. 5. The cover connected to the powder inlet 5 through the pin structure 6 7, the powder outlet 8 opened on the side of the powder storage box 4, the step away from the powder outlet 8 opened on the side of the powder storage box 4 The motor placement hole 10, the stepping motor 11 embedded in the stepping motor placement hole 10, and the packs of treatment powder 12 embedded in the powder storage box 4 wrapped with tissue paper are composed together. The powder processing device The powder processing box 13 fixedly connected to the bottom surface of the fuselage 1 through the bolt structure 2 3, the powder inlet 14 opened on the side of the powder processing box 13, the baffle structure 15 embedded in the powder inlet 14, The rotary motor placement slot 16 opened on the top of the powder processing box 13, the rotary motor 17 embedded in the rotary motor placement slot 16 with the rotating end downward, the blade 19 connected to the rotary end of the rotary motor 17 through a bearing 18, and the The fan placement slot 20 on the top of the powder processing box 13 and the fan 21 embedded in the fan placement slot 20 are composed together. 22. The exhaust fan 24 connected with the powder outlet 22 through the thread structure 1 23, and the nozzle 26 connected with the exhaust fan 24 through the thread structure 2 25 are composed together, and the control device is composed of the cockpit 27 opened in the fuselage 1 The PLC controller placement slot 29 on the control panel 28 in the interior, the PLC controller 30 embedded in the PLC controller placement slot 29 and electrically connected with the control panel 28, the button switch placement slot 31 opened on the control panel 28 , the button switch 32 that is embedded in the button switch placement groove 31 and is electrically connected with the control panel 28 is jointly composed; The thread 35 in the hole 33 and matched with the bolt 34, the bolt hole 36 that is opened on the bottom surface of the fuselage 1 and matches the bolt placement hole 33 are jointly formed, the thread 35 tapped in the bolt hole 36, and the bolt placement hole 33 and the bolt hole 36 are connected. The bolts 34 between them are jointly formed; the bolt structure 2 consists of a bolt placement hole 33 opened on the bottom surface of the powder processing box 13, a screw thread 35 tapped in the bolt placement hole 33 and matched with the bolt 34, and opened on the fuselage 1 Bolt holes 36 matching the bottom surface and bolt placement holes 33 are jointly formed, threaded threads 35 tapped in the bolt holes 36, bolts 34 connected between the bolt placement holes 33 and the bolt holes 36 are jointly formed; The baffle plate structure 15 consists of a baffle plate placement groove 37 opened in the powder inlet 2 14, a baffle plate 38 embedded in the baffle plate placement groove 37, and an extension between the baffle plate placement groove 37 and the baffle plate 38. Time switch structure 39 forms jointly; Time delay switch structure 39 is by the electromagnet one 41 that is fixedly connected with time delay switch 40 near baffle plate 38 one ends, opens in baffle plate 38 and is close to the electromagnet two placement slots 42 of time delay switch 40 one ends, The electromagnet 2 43 embedded in the electromagnet 2 placement groove 42 is jointly composed; the powder outlet 1 8 is connected with the powder inlet 2 14 through a smooth round tube 44, and the smooth round tube 44 is connected with the powder outlet One end of one 8 plug-in is higher than one end inserted with powder inlet two 14; The blade 19 coincides with the center line of powder inlet two 14; 7, the pin shaft fixing hole 45 at one end of the contact, the pin shaft placement hole 46 at the end where the cover 7 contacts the powder inlet-5, and the pin shaft 47 connected between the pin shaft fixing hole 45 and the pin shaft placement hole 46 are jointly formed. Described thread structure one 23 is made up of the external thread 48 that is tapped at the end that powder outlet two 22 contacts with exhaust fan 24, and the internal thread 49 that taps at the end that exhaust fan 24 contacts with powder outlet two 22 is jointly formed, and described screw thread The second structure is composed of an internal thread 49 tapped at the end where the nozzle 26 is in contact with the exhaust fan 24, and an external thread 48 tapped at the end where the exhaust fan 24 is in contact with the nozzle 26; the powder storage box 4 is equipped with an alarm Place the slot 50, the alarm placement slot 50 is embedded with an alarm 51, the alarm 51 is electrically connected with the stepper motor 11; the input terminal 9 of the PLC controller is electrically connected with the button switch 32, the The PLC controller 30 is electrically connected to the stepper motor 11, the PLC controller 30 is electrically connected to the rotating motor 17, the PLC controller 30 is electrically connected to the fan 21, and the PLC controller 30 is electrically connected to the exhaust fan. 24, the PLC controller 30 is electrically connected to the delay switch 40, and the PLC controller 30 is electrically connected to the alarm 51.

The feature of this embodiment is that the device for controlling acid rain by aircraft consists of a powder storage device fixed to the bottom surface of the fuselage through a bolt structure, a powder processing device located on the side of the powder storage device and fixedly connected to the bottom surface of the fuselage through a second bolt structure, and located at the bottom of the fuselage. The powder spraying device under the powder processing device and the control device located in the fuselage and fixedly connected with the fuselage are composed together. The powder inlet 1 on the top of the body, the cover connected to the powder inlet 1 through a pin structure, the powder outlet 1 on the side of the powder storage box, and the stepping motor opened on the side of the powder storage box away from the powder outlet 1 The placement hole, the stepping motor embedded in the stepping motor placement hole, and a bag of treatment powder embedded in the powder storage box wrapped in tissue paper are composed together. Fixedly connected powder processing box, powder inlet 2 opened on the side of the powder processing box, baffle structure embedded in powder inlet 2, rotating motor placement slot opened on the top of the powder processing box, embedded in The rotating motor is placed in the slot of the rotating motor and the rotating end is downward, the blade is connected with the rotating end of the rotating motor through a bearing, the fan slot is opened on the top of the powder processing box, and the fan embedded in the fan slot is composed together. The spraying device is composed of the powder outlet 2 opened at the bottom of the powder processing box and communicated with the fuselage, the exhaust fan connected with the powder outlet 2 through the thread structure 1, and the nozzle connected with the exhaust fan through the thread structure 2. The control device consists of The PLC controller placement slot on the control panel in the cockpit of the fuselage, the PLC controller embedded in the PLC controller placement slot and electrically connected to the control panel, and the push button switch on the control panel are placed The tank is composed of a button switch embedded in the button switch slot and electrically connected to the control panel. The aircraft is used to spray the treatment powder into the air, and the reaction between the treatment powder and water is used to achieve the effect of acid rain control. The PLC controller realizes the device The stepper motor pushes a pack of treatment powder each time, and the fan blows the treatment powder evenly to reduce the waste caused by too much treatment powder. The exhaust fan sucks the treatment powder away evenly, and reacts with rainwater through the nozzle .

In this embodiment, when the button switch is pressed, the PLC controller is powered on, and the program programmed in the PLC controller is automatically controlled, and the stepping motor starts to work. Push the first bag into the round tube, and under the action of gravity, the treated powder slides into the powder processing box along the round tube. time to set the delay switch time. The set time is slightly longer than the time for the treatment powder to reach the powder inlet 2. The two irons are separated, the baffle is closed, the rotating motor starts to move after the stepping motor works for a period of time, the rotating motor stops rotating after the delay switch action, the fan starts to work after the delay switch action, and the blade is driven by the rotating motor , cut the thin paper wrapped around the treatment powder, the fan blows the treatment powder away, the exhaust fan inhales the blown treatment powder and sprays it out through the nozzle, and the sprayed treatment powder reacts with the rain in the air to control acid rain function, calculate the time needed to complete a spraying, and control the running time of the stepping motor through the PLC controller. When the stepping motor is fully extended, the alarm will sound, press the button switch, the device will stop running, and the staff will open the powder. The lid in the storage box puts the bag of treatment powder into the powder storage box, and then presses the button switch to restart the device.

The above-mentioned technical solutions only reflect the preferred technical solutions of the technical solutions of the present invention, and some changes that those skilled in the art may make to certain parts reflect the principles of the present invention and fall within the protection scope of the present invention.

Claims (10)

1. a kind of device for administering acid rain using aircraft, including fuselage (1), which is characterized in that described to administer acid rain using aircraft Device by the powder storage unit fixed with fuselage (1) underrun bolt arrangement one (2), be located at powder storage unit side And be fixedly connected with fuselage (1) underrun bolt arrangement two (3) powder processing, below powder processing Powder flusher, control device interior positioned at fuselage (1) and being fixedly connected with fuselage (1) collectively constitute, the powder storing Device by be fixedly connected with fuselage (1) underrun bolt arrangement one (2) powder storing cabinet (4), be opened in powder storing case Powder inlet one (5) at the top of body (4), is opened in powder storing at the lid (7) being connect by pin shaft structure (6) with powder inlet one (5) The meal outlet one (8) of cabinet (4) side is opened in stepper motor placement of powder storing cabinet (4) side far from meal outlet one (8) Hole (10), is inlaid in powder storing cabinet (4) interior thin paper at the stepper motor (11) being inlaid in stepper motor putting hole (10) Package packs of improvement powder (12) collectively constitute, the powder processing by with fuselage (1) underrun bolt arrangement Powder-processed cabinet (13) that two (3) are fixedly connected, is inlaid in the powder inlet two (14) for being opened in powder-processed cabinet (13) side It is baffle arrangement (15) in powder inlet two (14), the rotating electric machine placing groove (16) being opened at the top of powder-processed cabinet (13), embedding Pass through axis mounted in the rotating electric machine (17) that rotating electric machine placing groove (16) is interior and round end is downward, with rotating electric machine (17) round end The blade (19) for holding (18) connection, the fan placing groove (20) being opened at the top of powder-processed cabinet (13) are inlaid in fan placement Fan (21) in slot (20) collectively constitutes, and the powder flusher is by being opened in powder-processed cabinet (13) bottom and fuselage (1) meal outlet two (22) that is connected to passes through the exhaust fan (24) that connect of helicitic texture one (23) and exhausting with meal outlet two (22) Machine (24) is collectively constituted by the spray head (26) that helicitic texture two (25) connects, and the control device is by being opened in fuselage (1) PLC controller placing groove (29) on the inner control panel (28) of cockpit (27) is inlaid in PLC controller placing groove (29) And the PLC controller (30) being electrically connected with control panel (28), the button switch placing groove being opened on control panel (28) (31), common group of the button switch (32) for being inlaid in button switch placing groove (31) and being electrically connected with control panel (28) At.

2. a kind of device for administering acid rain using aircraft according to claim 1, which is characterized in that the bolt arrangement one (2) by be opened in the bolt putting hole (33) of powder storing cabinet (4) bottom surface, attack in the bolt putting hole (33) and with bolt (34) The screw thread (35) of cooperation is opened in the bolt hole (36) that fuselage (1) bottom surface and bolt putting hole (33) match and collectively constitutes, attacks in spiral shell Screw thread (35), connection bolt putting hole (33) in keyhole (36) and the bolt (34) between bolt hole (36) collectively constitute.

3. a kind of device for administering acid rain using aircraft according to claim 1, which is characterized in that the bolt arrangement two (3) by being opened in the bolt putting hole (33) of powder-processed cabinet (13) bottom surface, attacking and and bolt interior in bolt putting hole (33) (34) screw thread (35) that cooperates is opened in the bolt hole (36) that fuselage (1) bottom surface matches with bolt putting hole (33) and collectively constitutes, attacks Common group of the bolt (34) between screw thread (35), connection bolt putting hole (33) and the bolt hole (36) in bolt hole (36) At.

4. a kind of device for administering acid rain using aircraft according to claim 1, which is characterized in that the baffle arrangement (15) by the baffle placing groove (37) being opened in powder inlet two (14), the baffle (38) being inlaid in baffle placing groove (37), company Delay switch structure (39) between logical baffle placing groove (37) and baffle (38) collectively constitutes.

5. a kind of device for administering acid rain using aircraft according to claim 4, which is characterized in that delay switch structure (39) by be fixedly connected with delay switch (40) close to baffle (38) one end electromagnet one (41), be opened in baffle (38) close to prolonging Two placing groove of electromagnet (42) of Shi Kaiguan (40) one end, the electromagnet two (43) being inlaid in two placing groove of electromagnet (42) are altogether With composition.

6. a kind of device for administering acid rain using aircraft according to claim 1, which is characterized in that the meal outlet one (8) it is connected to powder inlet two (14) by smooth round tube (44), the smooth round tube (44) and meal outlet one (8) inserting One end is higher than the one end inserted with powder inlet two (14).

7. it is according to claim 1 it is a kind of using aircraft administer acid rain device, which is characterized in that the blade (19) with The center line of powder inlet two (14) is overlapped.

8. a kind of device for administering acid rain using aircraft according to claim 1, which is characterized in that the pin shaft structure (6) by being opened in the pin shaft fixation hole (45) of powder inlet one (5) and lid (7) contact one end, being opened in lid (7) and powder inlet one (5) pin shaft (47) between the pin shaft putting hole (46), connection pin shaft fixation hole (45) and pin shaft putting hole (46) of one end is contacted It collectively constitutes, the helicitic texture one (23) is by attacking in meal outlet two (22) external screw thread of the one end that is in contact with exhaust fan (24) (48), the internal screw thread (49) for attacking in exhaust fan (24) one end that is in contact with meal outlet two (22) collectively constitutes, the helicitic texture Two by attacking in spray head (26) internal screw thread (49) of the one end that is in contact with exhaust fan (24), attacking in exhaust fan (24) and spray head (26) phase The external screw thread (48) of contact one end collectively constitutes.

9. a kind of device for administering acid rain using aircraft according to claim 1, which is characterized in that the powder storing case It is provided with alarm placing groove (50) in body (4), is embedded with alarm (51) in the alarm placing groove (50), the alarm (51) it is electrically connected with stepper motor (11).

10. a kind of device for administering acid rain using aircraft according to claim 1, which is characterized in that the PLC controller Input terminal (9) and button switch (32) are electrically connected, the PLC controller (30) and stepper motor (11) are electrically connected, described PLC controller (30) and rotating electric machine (17) are electrically connected, and the PLC controller (30) and fan (21) are electrically connected, described PLC controller (30) and exhaust fan (24) are electrically connected, and the PLC controller (30) and delay switch (40) are electrically connected, institute PLC controller (30) and alarm (51) are stated to be electrically connected.