CN211996152U

CN211996152U - Unmanned aerial vehicle for artificial rainfall

Info

Publication number: CN211996152U
Application number: CN202020515381.8U
Authority: CN
Inventors: 张俊成
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-04-09
Filing date: 2020-04-09
Publication date: 2020-11-24
Anticipated expiration: 2030-04-09

Abstract

The utility model discloses an unmanned aerial vehicle for artificial rainfall, including shell case and unmanned aerial vehicle body, all fixedly connected with cartridge magazine is all around the lower surface of shell case, both sides all fixedly connected with shell storage bin between the cartridge magazine, the middle part upper end of shell storage bin is connected with the lower surface of shell case fixedly, the shell is filled in the shell storage bin, shell storage bin and the inside of upper cartridge magazine communicate; every go up the equal fixed mounting in inside bottom of magazine and have the promotion cylinder, the upper end fixedly connected with backing plate of promotion cylinder, go up the upper end of magazine and seted up out the magazine, the utility model discloses a set up the magazine all around in cannon ball bottom of the case portion and set up electromagnetism gun barrel, propulsion cylinder and go up the magazine respectively in cannon ball incasement portion both sides, can carry out the sabot transmission when carrying out artificial rainfall incessantly for artificial rainfall operation can be in the quick completion of short time, and operating time is many, reduces the cost of operation.

Description

Unmanned aerial vehicle for artificial rainfall

Technical Field

The utility model relates to an unmanned aerial vehicle application technology field, concretely relates to an unmanned aerial vehicle for artificial rainfall.

Background

Unmanned planes (unmanned planes for short) can perform aerial photography, resource investigation, patrol, disaster relief material delivery and other projects, and the demand of the unmanned planes in social life is higher and higher. With the popularization of aircraft attitude control systems and aerospace technologies, unmanned aircraft of various sizes gradually enter the civil market, and particularly in the freight logistics industry, unmanned aircraft are gradually utilized to transport goods.

The unmanned aerial vehicle is also applied to the work of artificial rainfall, the cost of the artificial rainfall can be effectively reduced, and the patent with the publication number of CN208026130U discloses the unmanned aerial vehicle for the artificial rainfall, which comprises an aircraft body, a to-be-loaded cartridge case, a cartridge case, an adjusting platform and an electromagnetic gun barrel, wherein the cartridge case is fixedly connected to the bottom of the aircraft body, a cartridge placing structure and a cartridge lifting structure for placing cartridges are arranged in the cartridge case, the to-be-loaded cartridge case and the adjusting platform are fixedly connected to the top of the aircraft body, the adjusting platform can adjust the transmitting direction of the electromagnetic gun barrel up and down, the cartridge lifting structure conveys the cartridges into the to-be-loaded cartridge case, and a pushing device is arranged on the to-be-loaded cartridge case and used for pushing the cartridges in the to-be-loaded cartridge case into the electromagnetic gun barrel; and the electromagnetic gun barrel is also provided with a balancing device for balancing the impact force when the cannonball is launched.

When the device is used for artificial rainfall work, the interval time for launching the shells is long, continuous launching cannot be carried out, and the weight inside the shell box of the device is uneven, so that the device is unstable in the flight operation process and influences the normal operation of artificial rainfall.

There is therefore a need to design a drone for artificial rainfall to solve the problems set forth in the background above.

SUMMERY OF THE UTILITY MODEL

The utility model aims at overcoming the current device that prior art exists and carrying out artificial rainfall during operation, it is longer to carry out the transmission interval of shell, can not carry out continuous transmission, and the device's bullet incasement portion has weight inhomogeneous, in-process unstability at the flight operation, influence artificial rainfall's normal operation problem, an unmanned aerial vehicle for artificial rainfall is provided, this an unmanned aerial vehicle for artificial rainfall has and can not carry out the sabot transmission intermittently when carrying out artificial rainfall, make artificial rainfall operation can be quick completion in the short time, the activity duration is many, the effect of the cost of operation has been reduced.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle for artificial rainfall comprises a shell box and an unmanned aerial vehicle body, wherein upper magazine bins are fixedly connected to the periphery of the lower surface of the shell box, shell storage bins are fixedly connected between the upper magazine bins on two sides, the upper ends of the middle parts of the shell storage bins are fixedly connected with the lower surface of the shell box, shells are filled in the shell storage bins, and the shell storage bins are communicated with the inner parts of the upper magazine bins;

a lifting cylinder is fixedly mounted at the inner bottom end of each upper magazine, a base plate is fixedly connected to the upper end of each lifting cylinder, an ejection slot is formed in the upper end of each upper magazine, and the ejection slot is communicated with the interior of a gun magazine;

the middle part fixedly connected with division board of shell case, the both sides at division board both ends all are provided with propulsion cylinder, every the inner wall fixed connection of propulsion cylinder and shell case, and every the first push pedal of the equal fixedly connected with of one end of propulsion cylinder, the mounting groove has all been seted up to the middle part both sides of division board, both sides the equal fixed mounting in inside of mounting groove has the promotion cylinder, both sides the equal fixedly connected with second push pedal of one end of promotion cylinder.

Preferably, the loading groove has all been seted up to the inside lower surface both sides of unmanned aerial vehicle body, the loading groove is located both sides the middle part position of propulsion cylinder, both sides one side in loading groove all is provided with the bullet case, go up the inside fixed surface of bullet case and unmanned aerial vehicle body and be connected, both sides go up the equal fixedly connected with electromagnetism barrel of one end of bullet case, both sides the outside that the unmanned aerial vehicle body extends to the unmanned aerial vehicle body is run through to the one end of electromagnetism barrel.

Preferably, the two sides of the upper ejection box are fixedly connected with limiting plates, and two ends of each limiting plate are flush with one side of the ejection grooves on the two sides.

Preferably, the shell storage bin is obliquely arranged, and an included angle between the shell storage bin and the upper shell bin is 60 degrees.

Preferably, the equal fixedly connected with second connecting strip in upper surface both sides of shell case, the equal fixedly connected with first connecting strip in lower extreme both sides of unmanned aerial vehicle body, through fixing bolt fixed connection between first connecting strip and the second connecting strip.

Preferably, the lift cylinder has a rising length equal to the length of the inside of the upper magazine.

Compared with the prior art, the utility model provides an unmanned aerial vehicle for artificial rainfall possesses following beneficial effect:

1. the utility model discloses a set up the magazine all around at the shell case bottom and set up electromagnetism gun barrel, propulsion cylinder and bullet loading case respectively in shell case inside both sides, can carry out the bullet filling transmission intermittently not when carrying out artificial rainfall, make artificial rainfall operation can be in the quick completion of short time, the operating time is many, has reduced the cost of operation;

2. the utility model can keep the weight inside the cannonball box balanced by symmetrically arranging the upper magazine, the electromagnetic cannon barrel, the propulsion cylinder and the upper ammunition box, and avoid the uncontrolled flight direction caused by unbalanced weight inside the cannonball box when the unmanned aerial vehicle operates, so that the device can keep stable operation when artificial rainfall is carried out;

3. the electromagnetic gun tubes are arranged on two sides of the utility model, when the artificial rainfall operation is carried out, the launching reaction force of the device is balanced by launching the shells at the same time, and the influence of recoil on the device is eliminated;

the part that does not relate to in the device all is the same with prior art or can adopt prior art to realize, the utility model has the advantages of being scientific and reasonable in structure, convenience safe in utilization provides very big help for people.

Drawings

Fig. 1 is a schematic view of a front view structure provided by the present invention;

fig. 2 is a schematic view of a front view cross-sectional structure provided by the present invention;

fig. 3 is a schematic top view cross-sectional structure of the projectile box according to the present invention;

fig. 4 is an enlarged schematic structural diagram of a point a in fig. 3 according to the present invention.

Description of the reference numerals

The cartridge case 1, unmanned aerial vehicle body 2, go up magazine 3, the magazine is stored to the shell 4, first connecting strip 5, second connecting strip 6, fixing bolt 7, electromagnetism barrel 8, go up magazine 9, propulsion cylinder 10, promote cylinder 11, backing plate 12, shell 13, play bullet groove 14, limiting plate 15, dress bullet groove 16, division board 17, first push pedal 18, mounting groove 19, promote cylinder 20, second push pedal 21.

Detailed Description

The following detailed description of the embodiments of the present invention will be made with reference to the accompanying drawings. It is to be understood that the description of the embodiments herein is for purposes of illustration and explanation only and is not intended to limit the invention.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be a fixed connection, a detachable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Please refer to fig. 1-4, the utility model provides an unmanned aerial vehicle technical scheme for artificial rainfall: an unmanned aerial vehicle for artificial rainfall comprises a cartridge case 1 and an unmanned aerial vehicle body 2, wherein the periphery of the lower surface of the cartridge case 1 is fixedly connected with an upper cartridge chamber 3, a shell storage chamber 4 is fixedly connected between the upper cartridge chambers 3 on two sides, the upper end of the middle part of the shell storage chamber 4 is fixedly connected with the lower surface of the cartridge case 1, shells 13 are filled in the shell storage chamber 4, and the shell storage chamber 4 is communicated with the interior of the upper cartridge chamber 3; the cannonball storage bin 4 is used for filling cannonballs 13 into the upper magazine 3, the bottom end of the inner part of each upper magazine 3 is fixedly provided with a lifting cylinder 11, the upper end of each lifting cylinder 11 is fixedly connected with a backing plate 12, the upper end of each upper magazine 3 is provided with an ejection slot 14, and the ejection slots 14 are communicated with the inner part of the cannonball box 1; the cannonball 13 is lifted through the lifting cylinder 11 and the backing plate 12, the cannonball box 1 is arranged in the ejection slot 14, the middle part of the cannonball box 1 is fixedly connected with the separation plate 17, the two sides of the two ends of the separation plate 17 are provided with the propulsion cylinders 10, each propulsion cylinder 10 is fixedly connected with the inner wall of the cannonball box 1, one end of each propulsion cylinder 10 is fixedly connected with the first push plate 18, the cannonball 13 in the cannonball box 1 is pushed through the propulsion cylinders 10 and the first push plates 18, the mounting grooves 19 are formed in the two sides of the middle part of the separation plate 17, the propulsion cylinders 20 are fixedly mounted in the mounting grooves 19 in the two sides, the second push plates 21 are fixedly connected with the ends of the propulsion cylinders 20 in the two sides, and the cannonball 13 is pushed into the upper ammunition box 9 through the propulsion cylinders 20 and the second push plates 21.

In the utility model, preferably, both sides of the inner lower surface of the unmanned aerial vehicle body 2 are provided with the ammunition loading grooves 16, the ammunition loading grooves 16 are positioned at the middle position of the two-side propulsion cylinders 10, the cannonball 13 is limited through the ammunition loading grooves 16 to avoid the cannonball sliding, one side of each of the two-side ammunition loading grooves 16 is provided with the ammunition feeding box 9, the ammunition feeding box 9 is fixedly connected with the inner lower surface of the unmanned aerial vehicle body 2, one end of each of the two-side ammunition feeding boxes 9 is fixedly connected with the electromagnetic gun tube 8, the cannonball 13 is launched through the electromagnetic gun tube 8, one end of each of the two-side electromagnetic gun tubes 8 penetrates through the unmanned aerial vehicle body 2 and extends to the outer side of the unmanned aerial vehicle body 2, both sides of each of the ammunition feeding box 9 are fixedly connected with the limiting plates 15, both ends of the limiting, and the contained angle that storehouse 4 and last magazine 3 were stored to the shell is 60, store 4 slopes in storehouse through the shell and set up the inside that is favorable to the shell to store 4 inside shells 13 of storehouse and enter into last magazine 3, the equal fixedly connected with second connecting strip 6 in upper surface both sides of shell case 1, the equal fixedly connected with first connecting strip 5 in lower extreme both sides of unmanned aerial vehicle body 2, through fixing bolt 7 fixed connection between first connecting strip 5 and the second connecting strip 6, the rising length that promotes cylinder 11 is the same with the inside length in last magazine 3.

The utility model discloses a theory of operation and use flow: when in use, the shell 13 enters the upper magazine 3 from the inside of the shell storage bin 4, the shell 13 entering the upper magazine 3 is facilitated by the inclined arrangement of the shell storage bin 4, the shell 13 entering the upper magazine 3 is lifted by the lifting cylinder 11 and the backing plate 12 and enters the shell box 1 through the shell outlet groove 14, the shell 13 inside the shell box 1 pushes the shell 13 inside the shell box 1 through the pushing cylinder 10 and the first push plate 18, so that the shell 13 enters the shell loading groove 16, the shell 13 inside the shell loading groove 16 is pushed into the upper magazine 9 through the pushing cylinder 20 and the second push plate 21, the shell 13 is shot through the electromagnetic gun tube 8, the electromagnetic gun tube 8 is arranged on both sides, when the shell 13 is shot, recoil force is generated at the same time for balancing, the device can not incline, and the artificial rainfall can be carried out smoothly.

The preferred embodiments of the present invention have been described in detail above, but the present invention is not limited thereto. In the technical idea scope of the present invention, it can be right to the technical solution of the present invention perform multiple simple modifications, including each technical feature combined in any other suitable manner, these simple modifications and combinations should be regarded as the disclosed content of the present invention, and all belong to the protection scope of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle for artificial rainfall, includes shell case (1) and unmanned aerial vehicle body (2), its characterized in that: the periphery of the lower surface of the artillery shell case (1) is fixedly connected with upper magazine bins (3), shell storage bins (4) are fixedly connected between the upper magazine bins (3) on two sides, the upper ends of the middle parts of the shell storage bins (4) are fixedly connected with the lower surface of the artillery shell case (1), shells (13) are filled in the shell storage bins (4), and the shell storage bins (4) are communicated with the inner parts of the upper magazine bins (3);

a lifting cylinder (11) is fixedly mounted at the bottom end of the interior of each upper magazine (3), a backing plate (12) is fixedly connected to the upper end of each lifting cylinder (11), an ejection slot (14) is formed in the upper end of each upper magazine (3), and the ejection slot (14) is communicated with the interior of the gun magazine (1);

the middle part fixedly connected with division board (17) of shell case (1), the both sides at division board (17) both ends all are provided with propulsion cylinder (10), every propulsion cylinder (10) and the inner wall fixed connection of shell case (1), and every the first push pedal of the equal fixedly connected with of one end (18) of propulsion cylinder (10), mounting groove (19), both sides have all been seted up to the middle part both sides of division board (17) the equal fixed mounting in inside of mounting groove (19) has propulsion cylinder (20), both sides the equal fixedly connected with second push pedal (21) of one end of propulsion cylinder (20).

2. The unmanned aerial vehicle for artificial rainfall according to claim 1, wherein both sides of the inner lower surface of the unmanned aerial vehicle body (2) are provided with an ammunition loading groove (16), the ammunition loading groove (16) is located at the middle position of the propulsion cylinder (10) at both sides, one side of the ammunition loading groove (16) at both sides is provided with an ammunition feeding box (9), the ammunition feeding box (9) is fixedly connected with the inner lower surface of the unmanned aerial vehicle body (2), one end of the ammunition feeding box (9) at both sides is fixedly connected with an electromagnetic gun barrel (8), and one end of the electromagnetic gun barrel (8) at both sides extends through the unmanned aerial vehicle body (2) to the outer side of the unmanned aerial vehicle body (2).

3. Unmanned aerial vehicle for artificial rainfall according to claim 2, wherein limiting plates (15) are fixedly connected to both sides of the upper bouncing box (9), and both ends of the limiting plates (15) are flush with one side of the bouncing grooves (14) on both sides.

4. Unmanned aerial vehicle for artificial rainfall as claimed in claim 1 wherein the projectile storage bins (4) are all arranged obliquely and the angle between the projectile storage bins (4) and the upper magazine (3) is 60 °.

5. The unmanned aerial vehicle for artificial rainfall according to claim 1, wherein the projectile box (1) is fixedly connected with second connecting strips (6) on two sides of the upper surface, the unmanned aerial vehicle body (2) is fixedly connected with first connecting strips (5) on two sides of the lower end, and the first connecting strips (5) and the second connecting strips (6) are fixedly connected through fixing bolts (7).

6. Unmanned aerial vehicle for artificial rainfall according to claim 1 wherein the lift cylinder (11) has a raised length that is the same as the length inside the upper magazine (3).